Joel James Posted February 11, 2012 Report Share Posted February 11, 2012 (edited) Population: 83,000,000 [size="6"][b]Relations[/b][/size] [center][color="#0000FF"][b]Blue[/b] = Major Allies[/color] [color="#800080"][b]Purple[/b] = Minor allies[/color] [color="#00FF00"][b]Green[/b] = Friendly[/color] [color="#FF8C00"][b]Orange[/b] = Threat[/color] [color="#FF0000"][b]Red[/b] = Enemy[/color] [b][color="#0000FF"]African Union[/color][/b] - [color="#0000FF"]Being a nation in Africa, Atlantis was the 9th of 14 nations to be inducted into the African Unity pact. the pact has been recently upgraded to an Mutual Defense Pact with a supremacy clause, and renamed the African Union. This Union, unlike the ones in Europe and Asia, encompass all nations in Africa and represents Africa as a whole. The African Union currently has 7 member nations. [u][b]Current Members[/b][/u] [b]1.[/b] People's Republic of Africa [b]2.[/b] Aeon [b]4.[/b] Arctica [b]5.[/b] Haven [b]9.[/b] Atlantis [b]12.[/b] KwaZulu [b][u]Nations that left the African Union[/u][/b] [b]3.[/b] Tanzania Federation - Fallen Nation [b]6.[/b] Imperial Imazighen - Fallen Nation [b]7.[/b] Legion - Withdrawn by Legion popular vote [b]8.[/b] The Imperium - Fallen Nation [b]10.[/b] Levantia - Fallen Nation [b]11.[/b] Evonian - Fallen Nation [b]13.[/b] Zimbabwe - Fallen Nation [b]14.[/b] Lunar Republic - Withdrawn[/color] [s][b]Republic of Gallifrey[/b] - Treaty with this nation in the form of aid, trade, and intel sharing. This is the South American ally of Atlantis. Allying with this nation was preferred due to its ties with the Athenian Federation. [/s] [b](Fallen Nation)[/b] [color="#800080"][b]Athenian Federation[/b] - The Athenian Federation is the only non-African nation to have land holdings in Continental Africa. This nation has not shown any aggression to Africa. Also, this nation is considered friendly by extension of Tanzania's treaty with the nation. Recently, the nation of Atlantis signed a trade and non-aggression pact with this nation. This nation is the European ally of Atlantis.[/color][/center] [color="#FF0000"][b]Yaza Hajin[/b] - This is the remnants of a terrorist group left over from the days of Najambia. The citizens of the Hidden Kingdom worked hard to eliminate the Yaza Hajin, and many believed they were gone for good. Evidently, they were proven wrong when a Yaza Hajin member tried to assassinate the king[/color] [color="#FF8C00"][b]Umbrella Commonwealth[/b] - There is no diplomatic connection with this country.[/color] [size="6"][b]Army[/b][/size] 1st Army Corp 50000 soldiers 500 tanks 500 Main Hell Guns 500 S-400 Triumfs 500 Strykers 2nd Army Corp 50000 soldiers 500 tanks 500 Main Hell Guns 500 S-400 Triumfs 500 Strykers 3rd Army Corp 50000 soldiers 500 tanks 500 Main Hell Guns 500 S-400 Triumfs 500 Strykers 4th Army Corp 50000 soldiers 500 tanks 500 Main Hell Guns 500 S-400 Triumfs 500 Strykers 5th Army Corp 50000 soldiers 500 tanks 500 Main Hell Guns 500 S-400 Triumfs 500 Strykers 6th Army Corp 50000 soldiers 500 tanks 500 Main Hell Guns 500 S-400 Triumfs 500 Strykers 7th Army Corp 50000 soldiers 500 tanks 500 Main Hell Guns 500 S-400 Triumfs 500 Strykers 8th Army Corp 50,000 soldiers 500 tanks 500 Main Hell Guns 500 S-400 Triumfs 500 Strykers 9th Army Corp 50000 Soldiers 500 tanks 500 Main Hell Guns 500 S-400 Triumfs 500 Strykers 10th Army Corp 50000 soldiers 500 tanks 500 Main Hell Guns 500 S-400 Triumfs 500 Strykers 11th Army Corp 25344 soldiers 254 tanks 254 Main Hell Guns 254 S-400 Triumfs 254 Strykers Team 777 4,900 soldiers Team 777 Elite 100 soldiers Island 1500 soldiers 15 tanks 15 Main Hell Guns 15 S-400 Triumfs 15 Strykers Firebase Andy 1000 soldiers 10 tanks 10 Main Hell Guns 10 S-400 Triumfs 10 Strykers African Union Security Force 50000 soldiers 500 tanks 500 Main Hell Huns 500 S-400 Triumfs 500 Strykers [b]Reserves[/b] 4943 tanks 4943 Main Hell Guns 4943 S-400 Triumfs 4943 Strykers The Main Tanks are as follows: 50% are the AZ7 Protector Mk. II. It is the MANPADS variant 50% are the AZ7 Protector Mk. II. It is the Mortar Variant The Reserves are as follows: 50% are M-1 Abrams Tanks 50% are the Leopard 2A6 Kampfpanzer [size="6"][b]Navy[/b][/size] [b][size="3"]Northern Fleet[/size][/b] 45 Patrol Boats 6 Corvettes 2 Landing Ships 1 Battleship 1 Cruiser 6 Frigates 4 Destroyers 6 Submarines (5 attack, 1 missile) 2 Aircraft Carriers [b][size="3"]Southern Fleet[/size][/b] 45 Patrol Boats 3 Corvettes 2 Landing Ships 1 Battleship 1 Cruiser 6 Frigates 5 Destroyers 6 submarines (4 attack, 2 missile) 3 Aircraft Carriers [b]Island [/b] 90 Patrol Boats [b]Reserves[/b] 180 Patrol Boats 9 Corvettes 4 Landing Ships 2 Battleships 2 Cruisers 12 Frigates 9 Destroyers 12 Submarines (9 attack, 3 missile) 5 Aircraft Carriers [size="6"][b]Air Force[/b][/size] 100 AWACS 100 UAVs First Fighter Division Squad 1: 12 Sukhoi Su-37 Squad 2: 12 Sukhoi Su-37 Squad 3: 12 Sukhoi Su-37 Squad 4: 12 Sukhoi Su-37 Squad 5: 12 Sukhoi Su-37 Squad 6: 12 Sukhoi Su-37 Squad 7: 12 Sukhoi Su-37 Squad 8: 12 Sukhoi Su-37 Squad 9: 12 Sukhoi Su-37 Squad 10: 12 Sukhoi Su-37 Second Fighter Division Squad 11: 12 Sukhoi Su-37 Squad 12: 12 Sukhoi Su-37 Squad 13: 12 Sukhoi Su-37 Squad 14: 12 Sukhoi Su-37 Squad 15: 12 Sukhoi Su-37 Squad 16: 12 Sukhoi Su-37 Squad 17: 12 Sukhoi Su-37 Squad 18: 12 Sukhoi Su-37 Squad 19: 12 XF-32 Grey Widows Squad 20: 12 XF-32 Grey Widows Third Fighter Division Squad 21: 12 XF-32 Grey Widows Squad 22: 12 XF-32 Grey Widows Squad 23: 12 XF-32 Grey Widows Squad 24: 12 XF-32 Grey Widows Squad 25: 12 XF-32 Grey Widows Squad 26: 12 XF-32 Grey Widows Squad 27: 12 XF-32 Grey Widows Squad 28: 12 XF-32 Grey Widows Squad 29: 12 XF-32 Grey Widows Squad 30: 12 XF-32 Grey Widows Fourth Fighter Division Squad 31: 12 XF-32 Grey Widows Squad 32: 12 XF-32 Grey Widows Squad 33: 12 XF-32 Grey Widows Squad 34: 12 XF-32 Grey Widows Squad 35: 12 XF-32 Grey Widows Squad 36: 12 XF-32 Grey Widows Squad 37: 12 XF-32 Grey Widows Squad 38: 12 XF-32 Grey Widows Squad 39: 12 F/A-0 Brown Widows Squad 40: 12 F/A-0 Brown Widows Fifth Fighter Division Squad 41: 12 F/A-0 Brown Widows Squad 42: 12 F/A-0 Brown Widows Squad 43: 12 F/A-0 Brown Widows Squad 44: 12 F/A-0 Brown Widows Squad 45: 12 F/A-0 Brown Widows Squad 46: 12 F/A-0 Brown Widows Squad 47: 12 F/A-0 Brown Widows Squad 48: 12 F/A-0 Brown Widows Squad 49: 12 F/A-0 Brown Widows Squad 50: 12 F/A-0 Brown Widows Sixth Fighter Division Squad 51: 12 F/A-0 Brown Widows Squad 52: 12 F/A-0 Brown Widows Squad 53: 12 F/A-0 Brown Widows First Bomber Division Squad 54: 12 B-2 Lancers Squad 55: 12 B-2 Lancers Squad 56: 12 B-2 Lancers Squad 57: 12 B-2 Lancers Squad 58: 12 B-2 Lancers Squad 59: 12 B-2 Lancers Squad 60: 12 B-2 Lancers Squad 61: 12 B-2 Lancers Squad 62: 12 B-2 Lancers Squad 63: 12 B-2 Lancers Second Bomber Division Squad 64: 12 B-2 Lancers Squad 65: 12 B-2 Lancers Squad 66: 12 B-2 Lancers Squad 67: 12 B-2 Lancers Squad 68: 12 B-2 Lancers First Stealth Bomber Division Squad 69: 12 B-2 Stealth Bombers Squad 70: 12 B-2 Stealth Bombers Squad 71: 12 B-2 Stealth Bombers Squad 72: 12 B-2 Stealth Bombers Squad 73: 12 B-2 Stealth Bombers Squad 74: 12 B-2 Stealth Bombers Squad 75: 12 B-2 Stealth Bombers 840 Helicopters 840 C-130s 150 Predator B Drones 50 Predator C Drones [b]Reserves[/b] 980 Sukhoi Su-37 204 F/A-0 Brown Widows 240 XF-32 Grey Widows 330 B-2 Lancers 144 B-2 Spirit Stealth Bombers [size="4"][b]Missiles[/b][/size] 5000 Neptune hypersonic Air to Land Missiles mid-range variant 5000 Neptune hypersonic Air to Sea Missiles mid-range variant 5000 Neptune hypersonic Sea to Sea Missiles mid-range variant 5000 Neptune hypersonic Sea to Land Missiles mid-range variant 5000 Neptune hypersonic Land to Sea Missiles mid-range variant 5000 Neptune hypersonic Land to Land Missiles mid-range variant 5000 Neptune hypersonic Air to Land Missiles short-range variant 5000 Neptune hypersonic Air to Sea Missiles short-range variant 5000 Neptune hypersonic Sea to Sea Missiles short-range variant 5000 Neptune hypersonic Sea to Land Missiles short-range variant 5000 Neptune hypersonic Land to Sea Missiles short-range variant 5000 Neptune hypersonic Land to Land Missiles short-range variant 500 Neptune supersonic Air to Land Missiles mid-range variant 500 Neptune supersonic Air to Sea Missiles mid-range variant 500 Neptune supersonic Sea to Sea Missiles mid-range variant 500 Neptune supersonic Sea to Land Missiles mid-range variant 500 Neptune supersonic Land to Sea Missiles mid-range variant 500 Neptune supersonic Land to Land Missiles mid-range variant 100 Neptune I ICBM 10 Ricin missiles 7 500kt Nuclear Missiles (Range: 10,000 miles) Air Defense Network 1. Tor Missile Defense System 2. Buk-M2 Missile Defense System 3. S-300V 4. S-400 5. GMD Missile 6. S-450 Edited June 23, 2012 by Joel James Quote Link to comment Share on other sites More sharing options...
Joel James Posted February 11, 2012 Author Report Share Posted February 11, 2012 (edited) [center][size="7"][b]Various Specs[/b][/size][/center] [size="3"][b]F-35 Lightning IIs[/b][/size] Crew: 1 Length: 51.4 ft (15.67 m) Wingspan: 35 ft[N 5] (10.7 m) Height: 14.2 ft[N 6] (4.33 m) Wing area: 460 ft²[153] (42.7 m²) Empty weight: 29,300 lb (13,300 kg) Loaded weight: 49,540 lb[114][N 7][316] (22,470 kg) Max. takeoff weight: 70,000 lb[N 8] (31,800 kg) Powerplant: 1 × Pratt & Whitney F135 afterburning turbofan Dry thrust: 28,000 lbf[317][N 9] (125 kN) Thrust with afterburner: 43,000 lbf[317][318] (191 kN) Internal fuel capacity: 18,480 lb (8,382 kg)[N 10] Performance Maximum speed: Mach 1.6+[148] (1,200 mph, 1,930 km/h) Tested to Mach 1.61. Range: 1,200 nmi (2,220 km) on internal fuel Combat radius: over 590 nmi[N 11] (1,090 km) on internal fuel Service ceiling: 60,000 ft[321] (18,288 m) Rate of climb: classified (not publicly available) Wing loading: 91.4 lb/ft² (446 kg/m²) Thrust/weight: **With full fuel: 0.87 With 50% fuel: 1.07 g-Limits: 9 g[N 12] Armament Guns: 1 × General Dynamics GAU-22/A Equalizer 25 mm (0.984 in) 4-barreled gatling cannon, internally mounted with 180 rounds[N 13][148] Hardpoints: 6 × external pylons on wings with a capacity of 15,000 lb (6,800 kg)[148][153] and 2 internal bays with 2 pylons each for a total weapons payload of 18,000 lb (8,100 kg)[115] and provisions to carry combinations of: Missiles: ** Air-to-air missiles: AIM-120 AMRAAM AIM-9X Sidewinder IRIS-T MBDA Meteor (Pending further funding) Air-to-surface missiles: AGM-154 JSOW AGM-158 JASSM Brimstone missile Joint Air-to-Ground Missile SOM Anti-ship missiles: JSM Bombs: ***Mark 84, Mark 83 and Mark 82 GP bombs Mk.20 Rockeye II cluster bomb Wind Corrected Munitions Dispenser capable Paveway-series laser-guided bombs Small Diameter Bomb (SDB) JDAM-series B61 nuclear bomb Avionics Northrop Grumman Electronic Systems AN/APG-81 AESA radar Northrop Grumman Electronic Systems AN/AAQ-37 Distributed Aperture System (DAS) missile warning system BAE Systems AN/ASQ-239 (Barracuda) electronic warfare system Harris Corporation Multifunction Advanced Data Link (MADL) communication system [size="3"][b]F-22 Raptors[/b][/size] General characteristics Crew: 1 Length: 62 ft 1 in (18.90 m) Wingspan: 44 ft 6 in (13.56 m) Height: 16 ft 8 in (5.08 m) Wing area: 840 ft² (78.04 m²) Airfoil: NACA 64A?05.92 root, NACA 64A?04.29 tip Empty weight: 43,430 lb (19,700 kg) Loaded weight: 64,460 lb (29,300 kg[N 5]) Max. takeoff weight: 83,500 lb (38,000 kg) Powerplant: 2 × Pratt & Whitney F119-PW-100 Pitch Thrust vectoring turbofans Dry thrust: 23,500 lb[266] (104 kN) each Thrust with afterburner: 35,000+ lb[6][266] (156+ kN) each Fuel capacity: 18,000 lb (8,200 kg) internally, or 26,000 lb (11,900 kg) with two external fuel tanks Performance Maximum speed: At altitude: Mach 2.25 (1,500 mph, 2,410 km/h) [estimated] Supercruise: Mach 1.82 (1,220 mph, 1,963 km/h)[130] Range: >1,600 nmi (1,840 mi, 2,960 km) with 2 external fuel tanks Combat radius: 410 nmi (with 100 nmi in supercruise) (471 mi, 759 km) Ferry range: 2,000 mi (1,738 nmi, 3,219 km) Service ceiling: 65,000 ft (19,812 m) Wing loading: 77 lb/ft² (375 kg/m²) Thrust/weight: 1.09 (1.26 with loaded weight & 50% fuel) Maximum design g-load: -3.0/+9.0 g USAF poster overview of key features and armament Armament Guns: 1× 20 mm (0.787 in) M61A2 Vulcan 6-barreled gatling cannon in starboard wing root, 480 rounds Air to air loadout: 6× AIM-120 AMRAAM 2× AIM-9 Sidewinder Air to ground loadout: 2× AIM-120 AMRAAM and 2× AIM-9 Sidewinder for self-protection, and one of the following: 2× 1,000 lb (450 kg) JDAM or 8× 250 lb (110 kg) GBU-39 Small Diameter Bombs Hardpoints: 4× under-wing pylon stations can be fitted to carry 600 US gallon drop tanks or weapons, each with a capacity of 5,000 lb (2,268 kg). Avionics RWR (Radar warning receiver): 250 nmi (463 km) or more Radar: 125–150 miles (200–240 km) against 1 m2 (11 sq ft) targets (estimated range) Chemring MJU-39/40 flares for protection against IR missiles. [size="3"][b]B-2 Lancers[/b][/size] Crew: 4 (aircraft commander, copilot, offensive systems officer and defensive systems officer) Payload: 125,000 lb (56,700 kg) ; internal and external ordnance combined Length: 146 ft (44.5 m) Wingspan: Extended: 137 ft (41.8 m) Swept: 79 ft (24.1 m) Height: 34 ft (10.4 m) Wing area: 1,950 ft² (181.2 m²) Airfoil: NA69-190-2 Empty weight: 192,000 lb (87,100 kg) Loaded weight: 326,000 lb (148,000 kg) Max. takeoff weight: 477,000 lb (216,400 kg) Powerplant: 4 × General Electric F101-GE-102 augmented turbofans Dry thrust: 14,600 lbf (64.9 kN) each Thrust with afterburner: 30,780 lbf (136.92 kN) each Fuel capacity, optional: 10,000 U.S. gal (38,000 L) fuel tank for 1–3 internal weapons bays each Performance Maximum speed: At altitude: Mach 1.25 (721 knots, 830 mph, 1,340 km/h at 50,000 ft/15,000 m altitude) At low level: Mach 0.92 (700 mph, 1,130 km/h at 200–500 ft/60-150 m altitude) Range: 6,478 nmi (7,456 mi, 11,998 km) Combat radius: 2,993 nmi (3,445 mi, 5,543 km) Service ceiling: 60,000 ft (18,000 m) Wing loading: 167 lb/ft² (816 kg/m²) Thrust/weight: 0.38 Armament Hardpoints: six external hardpoints for 50,000 lb (22,700 kg) of ordnance (use for weapons currently restricted by START I treaty[72]) and three internal bomb bays for 75,000 lb (34,000 kg) of ordnance. Bombs: 84× Mk-82 Air inflatable retarder (AIR) general purpose (GP) bombs[154] 81× Mk-82 low drag general purpose (LDGP) bombs[155] 84× Mk-62 Quickstrike sea mines[156] 24× Mk-65 naval mines[157] 30× CBU-87/89/CBU-97 Cluster Bomb Units (CBU)[N 2] 30× CBU-103/104/105 Wind Corrected Munitions Dispenser (WCMD) CBUs 24× GBU-31 JDAM GPS guided bombs (Mk-84 GP or BLU-109 warhead)[N 3] 15× GBU-38 JDAM GPS guided bombs (Mk-82 GP warhead)[N 4] 24× Mk-84 general purpose bombs 12× AGM-154 Joint Standoff Weapon (JSOW) 96× or 144× GBU-39 Small Diameter Bomb GPS guided bombs[N 5] (not fielded on B-1 yet) 24× AGM-158 Joint Air to Surface Standoff Munitions (JASSM) 24× B61 nuclear variable-yield gravity bombs[157] (no longer carried) 24x B83 nuclear gravity bombs[157] (no longer carried) Avionics 1× AN/APQ-164 forward-looking offensive passive phased-array radar 1× AN/ALQ-161 radar warning and defensive jamming equipment 1× AN/ASQ-184 defensive management system 1× Lockheed Martin Sniper XR targeting pod (optional)[158][159] [size="3"][b]B-2 Spirit Stealth Bomber[/b][/size] Payload: 70,000 Lbs. Flight ceiling: 100,000 Ft. Classification: Stealth Crew: 2 RADAR jamming system: DRFM Missile evasion system: FLARE [size="3"][b]Corvette[/b][/size] Speed: 45 mph 2 76mm guns 2 40mm guns 3 BrahMos missiles 12 MK48 Advanced Capability (ADCAP) Heavyweight Torpedo 10 RAMS Draft: 17.4 ft Displacement - 2,000 tons Range 8,000 miles [size="3"][b]Landing Ships[/b][/size] Displacement: 8,500 tons Length: 522 ft Beam: 70 ft Draft: 17.4 ft Propulsion: 6 ALCO diesels (3 per shaft) 16,000 shaft horsepower; 800 hp GE bow thruster. 2 Hydraulically Controlled Variable Pitch Reversible Props and 1 Variable Pitch Bow Thruster 3 ALCO/GE Generators (750 kW, 1201 A each) Speed: 33 knots Troops: 400 [size="3"][b]Cruisers[/b][/size] Displacement: 9,800 tons Length: 567 ft Beam: 55 ft Draught: 34 ft Propulsion: 4 × General Electric LM2500 gas turbine engines, 80,000 shaft horsepower (60,000 kW) 2 × controllable-reversible pitch propellers 2 × rudders Speed: 32.5 knots Range: 3300 nmi at 30 knots Troops: 400 Sensors and Processing Systems: AN/SPY-1A/B multi-function radar AN/SPS-49 air search radar AN/SPG-62 fire control radar AN/SPS-73 surface search radar AN/SPQ-9 gun fire control radar AN/SQQ-89(V)3 Sonar suite, consisting of AN/SQS-53B/C/D active sonar AN/SQR-19 TACTAS passive sonar AN/SQQ-28 light airborne multi-purpose system AN/SLQ-32 Electronic Warfare Suite Electronic Warefare: Mark 36 SRBOC AN/SLQ-25 Nixie Armament: 2 × 61 cell Mk 41 vertical launch systems 122 × Mix of RIM-66M-5 Standard SM-2MR Block IIIB, RIM-156A SM-2ER Block IV, RIM-161 SM-3, RIM-162A ESSM, RIM-174A Standard ERAM, BGM-109 Tomahawk, or RUM-139A VL-ASROC 8 × RGM-84 Harpoon missiles 2 × Mk 45 Mod 2 5 in / 54 cal lightweight gun 2 × 25 mm Mk 38 gun 2–4 × .50 cal (12.7 mm) gun 2 × Phalanx CIWS Block 1B 2 × Mk 32 12.75 in (324 mm) triple torpedo Armor: Limited Kevlar splinter protection in critical areas Aircraft: 2 × Sikorsky SH-60B or MH-60R Seahawk LAMPS III helicopters. [size="3"][b]Battleships[/b][/size] Displacement: 45,000 tons 52,000 tons 57,000 tons Length: 861¼ ft 890 ft Beam: 108 ft Draft: 36 ft Installed power: 212,000 shp Propulsion: 4 screws;[1] GE geared turbines;[1] 8 B&W boilers Speed: 31 knots Range: 14,890 miles 11,700 miles (18,820 km) @ 20 knots (23 mph; 37 km/h)[2] Complement: ~2,700 officers and men (WWII, Korea)[1] ~1,800 officers and men (1980s)[1] Electronic warfare and decoys: 1980s: AN/SLQ-32(V)[4] AN/SLQ-25 Nixie[4] Mark 36 SRBOC[4] Armament: 9 × 16-inch / 50 cal. Mark 7 guns 12 × 5-inch/38 cal. Mark 12 guns 32 × BGM-109 Tomahawk 16 × RGM-84 Harpoon 3 x BrahMos Missiles 4 × 20 mm (78 inch).Phalanx CIWS[1][4] Armor: Belt: 12.1 in (310 mm),[5] Bulkheads: 11.3 in (290 mm),[5] Barbettes: 11.6 to 17.3 in (295 to 439 mm),[5] Turrets: 19.7 in (500 mm),[5] Decks: 7.5 in (190 mm)[5] Aircraft carried: World War II: 3 × Vought OS2U Kingfisher/Curtiss SC Seahawk Korea/Vietnam: 3 × helicopters Cold War/Gulf War: 5 × RQ-2 Pioneer Unmanned aerial vehicle[6] [size="3"][b]Destroyers[/b][/size] Displacement: 8,000 tons Length: 152.4 m (500 ft 0 in) Beam: 21.2 m (69 ft 7 in) Draught: 7.4 m (24 ft 3 in) Propulsion: 2 shafts Integrated electric propulsion(IEP); 2× Rolls-Royce WR-21 gas turbines, 21.5 MW (28,800 shp) each 2× Wärtsilä 12V200 diesel generators, 2 MW (2,700 shp) each[2] 2× Converteam electric motors, 20 MW (27,000 shp) each Speed: In excess of 29 kn (54 km/h; 33 mph)[3] Range: 7,000 nautical miles (13,000 km) at 18 kn (33 km/h) Complement: 190 (accommodation for up to 235) Sensors and Processing systems: SAMPSON multi-function air tracking radar (Type 1045) S1850M 3-D air surveillance radar (Type 1046) 2× Raytheon I-band Radar (Type 1047) 1× Raytheon E/F-band Radar (Type 1048)[4] Ultra Electronics Series 2500 Electro-Optical Gun Control System (EOGCS)[5] Ultra Electronics SML Technologies radar tracking system Ultra Electronics/EDO MFS-7000 sonar Electronic warfare and decoys: UAT16 Surface ship torpedo defence (SSTD) Armament: Anti-air missiles; Sea Viper air defence system. 48 cell SYLVER A50 VLS, for a combination of 48; Aster 15 missiles (range 2-30 km) Aster 30 missiles (range 3-120 km) BrahMos Missiles - 5 (290 km) CIWS system Guns; 1× BAE 4.5 inch Mk8 Mod. 1 gun 2× 30 mm guns 2× Phalanx CIWS 2× Miniguns 6× General-purpose machine guns 2× Quad Boeing AGM-84 Harpoon launchers (8 anti-ship missiles) BGM-109 Tomahawk land attack cruise missiles Aircraft carried: 1-2×Lynx HMA8, armed with; 4× Sea Skua anti ship missiles, or 2× anti submarine torpedoes Aviation facilities: Large flight deck Enclosed hangar [size="3"][b]S-400 Triumf (40N6)[/b][/size] Propellant solid propellant rocket motor Operational range 400 kilometres (250 mi) Flight ceiling 185 km[2] Boost time cold launch ejection system Speed Mach 12.0 Guidance system inertial guidance with radio command corrections Steering system gas dynamic flight control system [size="3"][b]Main Hell Gun[/b][/size] Weight 1,858 kg (4,100 lb) Length 8.8 m (28 ft 10 in) Barrel length 37 calibers[1] Width 1.78 m (5 ft 10 in) Height 2.13 m (7 ft) Crew 6 (normal), 4 (reduced) Calibre 105 mm (4.1 in) Breech vertical sliding block with electric firing mechanism Recoil hydropneumatic Carriage box trail, firing with wheels on the ground or platform Elevation -5.625° (-100 mils) to 70.3125° (1,250 mils) Traverse 360° (6,400 mils) on its platform and top traverse 5.625° (100 mils) left or right Rate of fire 6-8 rounds per minute Muzzle velocity maximum 708 m/s (2,320 ft/s) Maximum range 17,200 m (18,800 yd) (20.6 km (22,500 yd) extended range using base bleed) Sights optical dial sight on reciprocating mount or inertial using 3 ring laser gyros [size="3"][b]M-1 Abrams Tank[/b][/size] Weight 67.6 tons Length Gun forward: 32.04 ft Hull length: 26.02 ft Width 12 ft Height 8 ft Crew 4 (commander, gunner, loader, driver) Armor Chobham, RH armor, Depleted Uranium strike plates, Kevlar mesh Hull & turret - 350 mm vs APFSDS, 700 mm vs HEAT Main Armament 105 mm L52 M68 rifled cannon 120 mm L44 M256 smoothbore cannon with 42 rounds Secondary Armament 1 x .50-caliber (12.7 mm) M2HB heavy machine gun with 900 rounds 2 x 7.62 mm (.308) M240 machine guns with 8,800 rounds (1 pintle-mounted, 1 coaxial) Engine Honeywell AGT1500C multi-fuel turbine engine 1,500 shp (1,120 kW) Power/weight 24.5 hp/metric ton (18.27 kW/t) Transmission Allison DDA X-1100-3B Suspension Torsion bar Ground clearance 0.48 m (1 ft 7 in) Fuel capacity 500 gallons Operational Range: 426 km (265 mi) Speed : Road 67.6 km/h (42.0 mph) Off-road: 48.28 km/h (30.00 mph) [size="3"][b]Leopard 2A6 Kampfpanzer[/b][/size] Weight 62.3 tonnes Length 9.97 m Width 3.75 m Height 3.0 m Crew 4 Armour 3rd generation composite; including high-hardness steel, tungsten and plastic filler with ceramic component. Main Armament 1 x 120 mm Rheinmetall L55 smoothbore gun 42 rounds Secondary armament 2 x 7.62 mm MG3A1 4,750 rounds Engine MTU MB 873 Ka-501 liquid-cooled V-12 Twin-turbo diesel engine 1,500 PS (1,479 hp, 1,103 kW) at 2600 rpm Power/weight 24.1 PS/t (17.7 kW/t) Transmission Renk HSWL 354 Suspension Torsion-bar suspension Fuel capacity 1,200 liters Operational range 550 km (340 mi) (internal fuel) Speed 72 km/h (45 mph) [size="3"][b]AZ7 Protector-Mk. II [/b] [/size] Systems Crew: 3 (Commander, Driver, Gunner) Autoloader: AAZL795 Autoloader Computer: AvecNord AZK4 Advanced Electronics Management System Operating System: Linux Defender 6 'Freelancer' Communications: Thialfi II Advanced BattComm Network Dimensions Height: 2.5m Length: 7.90m Length (w/ gun): 9.5m Width: 4.05m Weight: 76.5 tonnes (+2.7 tonnes w/ slat armor additions) Propulsion Engine: AZE2462 Multi-Fuel LPG and Water Injection F-8 Hyperbar Diesel Engine [2200 HP] Engine Fuel Storage: 2500 Liter Insulated Fuel Storage Compartment APU: 2x AZE3025 Brushless DC Electric Engine, 1x AZE2258 Compact Gas Turbine 9x Lithium-Ion Manganese spinel cathode Battery (2016) Power/Weight: 29.93 hp/metric ton Transmission: Continuously Variable Transmission (Hydraulic Mechanical Transmission) Performance Suspension: Hydropneumatic Active Suspension Ground Clearance: 0.5m (Adjustable) Range: 725 to 815 km Max Onroad Speed: 84 kmph Max Reverse Onroad Speed: 84 kmph Max Offroad Speed: 65 kmph Max Reverse Offroad Speed: 65 kmph Fording Depth: 1.15 m [4.2 m w/ proper equipment] Protection Armor: Wyvelt-Orvald Advanced Composite Armor, RHA steel alloys, titanium ceramic composites, titanium alloy, depleted uranium, Draakskild/Weinik-Draakskild ERA/NERA, Slat Armor (optional) Anti-spall: Cenodyne Advanced Spall Liner Countermeasures: Invictus APS [Cato-3 Soft-kill Protection Suite; Langskild Hard-kill Protection Suite; Kobalt Hard-kill Protection Suite], AvecNord 'Ermit' CBRN Protection System Armament AZ1127 135mm L52 LP ETC EM-Rifled Smoothbore (2020) Right Coaxial Armament: AZ932 45 mm Autocannon Left Coaxial Armament: 7.62 mm pintle-mount machine gun Secondary Armaments: .50 caliber swing-mount heavy automated machinegun, 4x lateral mounted grenade launchers Tertiary Armaments: Rear-mounted mortar launcher, Rear-mounted laser-guided MANPADS [size="3"][b]Stryker[/b][/size] Weight ICV: 16.47 tons MGS: 18.77 tons Length 6.95 m Width 2.72 m Height 2.64 m Crew Varies. Usually 2. Passengers Varies Armor 7.62 mm/14.5 mm resistant Main armament M2 .50 cal. machine gun or MK19 40 mm grenade launcher mounted in a PROTECTOR M151 remote weapon station (RWS) (ICV) Secondary armament .50-cal M2 MG and M240 7.62 mm MG (MGS) Engine Caterpillar C8 260 kW (350 hp) Power/weight ICV: 20.0 kW/t Suspension 8×8 wheeled Operational range 400 miles Speed 70 mph [b]Upgrades[/b] Semi-Active Suspension Shallow V-Shaped Structure on hull [size="3"][b]Atlantis Attack Submarine [/b][/size] Class and type: Astute-class submarine Displacement: 7400 tonnes submerged Length: 97 m (323 ft) Beam: 11.3 m (37 ft) Draught: 10 m (33 ft) Propulsion: Rolls-Royce PWR2 reactor (with full submarine life core), MTU 600 kilowatt diesel generators Speed: 29+ knots (54 km/h) submerged Range: Only limited by food and maintenance requirements Complement: 98 officers and men normally, capacity of 109 Sensors and processing systems: Thales Sonar 2076 Atlas DESO 25 echosounder 2 x Thales CM010 optronic masts Raytheon Successor IFF Armament: 6 x 21-inch (533 mm) torpedo tubes with stowage for up to 38 weapons; Tomahawk Block IV land-attack cruise missiles Spearfish wire-guided heavyweight torpedoes [size="3"][b]Atlantis Missile Submarines[/b][/size] Type: Ballistic missile submarine Displacement: 14,720 t (14,488 long tons) surfaced 24,000 t (23,621 long tons) submerged Length: 170 m (557 ft 9 in) Beam: 13.5 m (44 ft 3 in) Draught: 10 m (32 ft 10 in) Propulsion: 1 × ОК-650В nuclear reactor 1 × AEU steam turbine 1 × shaft and propeller (pump-jet) Speed: Submerged: 29 knots (33 mph; 54 km/h)[2] Surfaced: 15 knots (17 mph; 28 km/h) Range: Unlimited except by food stores Test depth: planned 450m Complement: 55 officers, 52 enlisted Armament: 16(Project 955), 20(955U Borei II) × RSM-56 Bulava SLBMs with 6-10 MIRVed warheads[3] 6 × 533 mm torpedo tubes RPK-2 Viyuga cruise missiles 1 nuclear Missile (capacity) [size="3"][b]Patrol Boats[/b][/size] Displacement: 331 tons Length: 179 ft (55 m) Beam: 25 ft (7.6 m) Draught: 7.5 ft (2.3 m) Installed power: 2 CAT Marine SSDG Propulsion: 4 Paxman Valenta Diesel Engines Speed: 40 knots Boats and landing craft carried: USCG Over the Horizon Crew: 2 officers, 3 chiefs, 25 enlisted Armament: (USN) 2 × Mk38 chain guns 2 × Mk19 grenade launchers 2 × .50 (12.7 mm) machine guns 6 × Stinger missiles [size="3"][b]Atlantis Aircraft Carrier[/b][/size] Displacement: 100,000 tons (standard load) Overall: Length: 350 m Beam: 96 m Waterline: Length: 325 m Beam: 48 m Draft: 12 m Speed: 30+ kn (18 kn - operative) Range: unlimited Supply endurance: 45 days Propulsion: 4 x OK-900 nuclear reactors (600 MWt each) Armament Edit 4 x 72 S-500F Red Star combat system VLS (S-500D or E missiles) 4 x Palash CIWS/CADS complexes (32 9M337Sosna-R hypersonic CADS missiles) 4 x RBU-12000 Udav-1M counter-torpedo, anti-frogman and mobile minefield system (4 x 60 projectiles) [img]http://i1133.photobucket.com/albums/m586/JoelJames1/AricraftCarrier.gif[/img] [size="3"][b]Battle Suit[/b][/size] The suit will weigh a total of 25 pounds. Its many features include compartments for emergency morphine and salt, a knife and emergency light. Built into the forearms are a small recording device, a pepper-spray gun and a detachable transponder that can be swallowed in case of trouble. In the helmet, there's a solar-powered fresh-air system and a drinking tube attached to a canteen in the small of the back. A laser pointer mounted in the middle of the forehead is ready to point to snipers, while LED lights frame the face. The whole suit is made from high-impact plastic lined with ceramic bullet protection over ballistic foam. This armoe can stave off bullets, explosives, knives, and clubs. The armor protects everything on the body except for fingertips, and is lightly armored on all major joints. There is a satellite up link to the suit. [size="3"][b]F/A-0 Brown Widow[/b][/size] General Characteristics & Performance Crew: 1 Powerplant: 1 x Ragnarok F119-PW-100 Pitch Thrust Vectoring Turbofans 23,500 lbf of thrust (Supercruise) +35,000 lbf of thrust (With Afterburner) Max Speed: Mach 2+ (Supercruise) Mach 2+ (With Afterburners) Ferry Range: 3800 km (With twin external fuel tanks) Combat Radius: 2000 km Maximum Design g-Load: 9 g 1. The F/A-0 "BROWN WIDOW" is a 5th generation Strike Fighter developed by MILITARY AVIATION COMPLEX (MILAC) in collaboration AIR MILITANT COMMAND (AMC) to act as an Advanced Tactical Strike Asset (ATSA) program. As a DUAL ROLED aircraft, it is capable of delivering a vast array of air-to-air and air-to-ground munitions. It's secondary role as an air-to-ground system makes the aircraft a rapidly deployable delivery platform, from which munitions can be used for AIR INTERDICTION, TACTICAL ground attack and CLOSE AIR SUPPORT. However, utilizing both a tailless all-aspect broadband stealth airframe, an IR-Shielded thrust-vectoring engine, a hybrid control/close-coupled canard system and a vast array of technologies and weapons shared with the MILAC F-23 BLACK WIDOW, this plane also serves as a potent threat to any enemy air assets as a light duty fighter aircraft. 2.The "BROWN WIDOW" is aptly named after the spider species (following in the tradition of MILAC naming conventions), which is typically a somewhat smaller spider whose venom is twice as potent as the infamous black widow, but is normally confined to the area around the bite. This fits the aircraft well, as it carries a larger assortment of weapons, but it's smaller design leaves less room for fuel and hence limiting it's operational range to closer assignments (leaving longer range air-dominance roles to the F-23 BLACK WIDOW and priority interdiction sorties to the A-1 KRIEG). 3. Additionally, the aircraft is designed to be cheap and easier to fix by utilizing many of the same systems and technologies present within it's cousin, the F-23 BLACK WIDOW. This decision drastically reduces the cost of both planes by means of mass production of parts and results in a cheaper long-term maintenance plan for both aircraft. This serves as a deviation from the norm of contemporary MILAC built aircraft - the BROWN WIDOW is the first aircraft designed from conceptual stages to be primarily a full capability export aircraft, with production rights solely given to allied states. 4. THIS AIRCRAFT IS DESIGNED TO IMPLEMENT THE STANAG AND FULL INTEGRATION OF AFRICAN UNITY PACT COMBINED FORCES COMMAND (COMFOR) INTO A COHESIVE PAN-AFRICAN MILTARY FORCE. IT IS A PRIMARY MULTI-ROLE FIGHTER WITH EMPHASIS ON USAGE IN NORTH AND EAST MILITARY AIR OFFENSIVE ROLES AND A DEFENSIVE ROLE ACROSS THE AFRICAN CONTINENT. COCKPIT 1. The Cockpit of the MILAC F/A-0 features a roomy "glass-cockpit" design. Commands can be entered manually or via an integrated "user dependent" Adacel DVI (Direct Voice Input) system which accepts commands from the pilot verbally. The plane also contains a full-panel-width "cockpit panoramic display" to display warnings, RADAR systems, sensor-fuzed identification, targeting and tracking information and other relevant stimuli. The on-board computer can accesses an INTERNAL REFERENCE SYSTEM (IRS), which provides color and shape coordinated information on an enemy aircraft type and provides CURRENT battlefield knowledge of the maximum enemy RADAR detection range (yellow line) and missile range (red line). Overlapping enemy RADAR and missile regions are combined to avoid user clutter and the pilot is informed via a HELMET MOUNTED DISPLAY SYSTEM (HDMS) when they have fallen into either. Pilots can also use touch screen commands to share information with other pilots, by clicking on particular targets, or setting way-points at their command allowing for a fluid flow of information from one pilot to the group during a conversation (priority being given to the group leader). 2. All planes will utilize a HELMET MOUNTED DISPLAY SYSTEM (HMDS) to display enemy aircraft with missile systems cued to lock on by simply looking in the direction of the desired target if desired via combination of HIGH OFF-BORESIGHT weapons (HOBS). Alternative methods that can be sent to the FIRE CONTROL SYSTEM (FCS) including "manual" or "automatic" target selection. The aircraft contains a HEADS UP DISPLAY (HUD) system as a back up, relying primarily on the HMDS to convey information to the pilot. 3. All aircraft are equipped with a MARTIN-BAKER US16E ejection seat. Furthermore, control of the aircraft utilizes a right hand stick controller and a left throttle control. FIRE CONTROL SYSTEM (FCS) XN7 AND NETWORKING 1. The FCS XN7 fire control system is designed to maximize the effectiveness of the BROWN WIDOW. The aircraft is designed to acquire and track up to fifty targets air, land and sea on the COCKPIT DISPLAY PANEL and HMDS, and fire up to ten weapons simultaneously. Target acquisition is performed utilizing a combination of continuous radio-frequency and Infra-red tracking systems via SAIRST. Autonomous tracking for standoff weapons and further enemy information can be acquired via an onboard ELECTRO-OPTICAL TRACKING SYSTEM (EOTS) (OOC: Stealthy version of this) and IIDU based sensors. In combination, this array of sensors integrates with the FCS to provide full HIGH OFF-BORESIGHT weapon (HOBS) capabilities to all weapons - making aircraft orientation unimportant. The combined might of this multi-spectrum sensory information is realized as a sensor-fused advancement of the contemporary Target Acquisition System Software (TASS) utilized in the BLACK WIDOW, a marked improvement incorporating both legacy Nodic as well as modern Aeon advancements into a single cohesive package. 2. These systems are designed to work with a local "Group AEWACs", local group networks or space based networks via a MULTIFUNCTION ADVANCED DATA LINK (MADL), which transmits data between the planes and various military networks without compromising stealth features of the plane. The application of a satellite based WIDE AREA NETWORK (WAN), which can transmit data at 548 megabits per second and receive at gigabit speeds, allows for pilots to have full battlefield combat situational awareness and at the same time allows them to focus in on a smaller region to handle threats or objectives closer to home. The system provides pilots the full range of sensory information acquired by other secured network aircraft, AEWACs, EAE DETECTION EARLY WARNING (DEW) Long and Short Range RADARs along with ground support from EAE Air Support mobile RADARs and IR DETECTION STATIONS, SPECTATOR CLASS MILITARY SATELLITES and other detection networks validated by the AMC. When combined with BEYOND VISUAL RANGE missiles, the FCS and Networking system allows the pilots to even target and fire on enemies outside of their current sensor range, using the other systems information as the targeting system to acquire a "lock". 3. Networking is also a valuable system here as it can automatically assign targets to each individual missile according to priority, and the weapon best designed for the given target via a INTERNAL REFERENCE SYSTEM (IRS) which is continuously updated during combat operations via the network grid so pilots can have the best understanding possible of the enemy. This allows the group to utilize it's munitions to their fullest potential by rapidly assigning each weapon a unique target and allowing them an instant opportunity to fire or disregard each target at their discretion. With proper authorization, the system also has an auto-fire command allowing weapons to be fired as soon as the system has a lock-on on a non-friendly IDENTIFICATION FRIEND OR FOE (IFF) signature that has been designated as that systems target. It also allows pilots to enter the combat situation with an optimal understanding of the enemy as interactions occur on the battlefield. 5. The FCS system will also be able to make optimum use of new LOCK-ON AFTER LAUNCH (LOAL) capable missiles, allowing the user to fire the missile at the general vicinity of the target and then program the target into the missile after it is already in flight (also critical for internal bay launched missiles), or even allowing said missile to acquire a lock on its own via active seeking or networked tracking information from allied platforms. After launch, programming capabilities also allow for "nape of the earth" near-surface combat attack orientations. These allow the aircraft to fire upon enemy forces near the ground while using terrain as an active cover. On board navigation systems will soon also allow the programming of a BEYOND VISUAL RANGE (BVR) missile's flight trajectory so that it acts as a temporary "cruise-mode" before rising up to strike at it's opponents in the distance. ON-BOARD NAVIGATION SYSTEM 1. The on-board navigation system utilizes a RING LASER GYROSCOPIC INERTIAL NAVIGATION SYSTEM combined with on-board GPS positioning (developed from the lessons learned from MILAC's Deathstalker). On-board systems determine the aircraft's location in space on Earth, allowing the pilot to know their position at all times relative to their environment. The aircraft also has an AUTOMATIC GROUND-COLLISION AVOIDANCE SYSTEM (Auto GCAS). This system allows the aircraft to safely navigate along the "nape of the earth", utilizing terrain features to reduce the probability of detection by hostile forces and allowing for deep penetration into enemy territory. ARMARMENT 1. The smaller size of the Brown Widow, requires a significantly reduced internal weapons bay, providing room for up to six weapons mounts opposed to eight, as found on the F-23 Black Widow. It compensates for this lack of fire-power with a larger assortment of weapons and cheaper cost. Gun: 1 x 30mm Lancer auto-cannon, 540 CTA rounds Missiles: Aim 9x Sidewinder, SIR-73, SIR-74AC and SIR-74AC-ER, JAGM Missile, AGM-84 Harpoon, AGM-88E AARGM, AGM-154 JSOW, MBDA Meteor, SARAH-37 Missile, ADM-160A MALD, SEAD-MA and SEAD-MA-EM, 'Punisher' Tactical Assault Missile(TAM) Bombs: CBU-100 Cluster Bombs, JDAM Series, Mark 82, 83 and 84 GPBs, Paveway Series Bombs, Small Diameter Bombs All craft are additionally armed with chaff and flares for aircraft defense. More advanced defensive systems are as follows: 2 x Tanzanian Arms AN/AAQ-24 directional infrared countermeasure (DIRCM) system AN/AAR-54 missile warning system Small Laser Targeting Assembly (SLTA) 4 x Dorsal Bay mounting TA/MILAC 'mini-Nulka' cold launched Active Radar Expendable Decoy (ARED) 4 x ALE-50 Towed Decoy System NEXT GENERATION JAMMING AND CYBERATTACK 1. The Brown Widow mounts a NEXT GENERATION JAMMER (NGT) system, designed to escort stealthy and non-stealthy aircraft to the edge of an enemy threat zone, jamming radars used by the enemy to launch munitions at allied targets. The NGT is designed to open the envelope of safety given to allied units in order to successfully deploy stand-off attack munitions, escape a projected kill zone, or mount concerted close-in attacks to destroy high priority targets. The AESA based NGJ system is designed to exploit electronic warfare, operating across a broad swath of the electromagnetic spectrum. This electronic surveillance and attack system utilizes the very skin of the Black Widow as a giant AESA array, breaking it up into four 'quadrants', elements that are steerable, directable and assignable in frequency. Each quadrant is tasked for use in differing functions, as well as for pointing at differing targets. In addition, this quadrant based system can be used in its totality to provide a very high power capability, producing nearly three times the power in a much smaller package. 2. The NGT is capable of directing its energy in a concerted attack against sensitive enemy electronics. In addition, it is capable of inserting malicious information into enemy data streams, allowing for suppression of enemy intelligence gathering assets or their outright disablement. RADAR, EWS AND SECURITY 1. The Brown Widow Utilizes a MILAC/APG-77 ACTIVE ELECTRONICALLY SCANNED ARRAY (AESA) RADAR system. The RADAR system is controlled by via two TENSOR COMMON INTEGRATED PROCESSORS (CIP)s, which can process 10.5 billion instructions per second and have 300 MB of memory. This information is processed further by the on-board FCS XN7 computer system which provides the information in an easy to understand, informative display in the cockpit. The RADAR system has an expected range of approximately 200-250 km, with up to a 400 km range when utilizing a narrow beam search pattern. Additionally the aircraft has 6 EO/IR-sensors, and a Ultra-Violet MISSILE APPROACH EARLY WARNING SYSTEM (MAWS) both of which combine to be as a missile warning system with continuous coverage on all angles of the aircraft. The system is integrated with the FCS XN7 system and an AN/ASQ-239 (Barracuda) ELECTRONIC WARFARE SYSTEM (EWS). Additionally, the aircraft has seperate ECM and CECM pods smoothly integrated into the wing-tips for additional support of the NGJ system. Internal electronics are protected by concentrated Electro-magnetic shielding to lessen the effects of concerted EM attacks. 2. In addition to the EWS used to protect the aircraft from electromagnetic attacks, an extensive on-board security suite is installed to avoid interference with the network via "hacking". All MILAC networks run on a SECURE ISOLATED NETWORK (SIN). The system utilizes FULL 1024 BIT ADVANCED ENCRYPTION STANDARD (AES) technology to encode all relevant information between parties, in conjunction with an indigenously developed Reduced Instruction Set driving hardware. In addition to these encryption technologies, all networks will operate in "stealth mode", acting as though the network didn't exist to any party outside of those programmed into the main system. No party can acquire /ROOT ACCESS to the software while the aircraft is operating, nor while the wireless network system is active. Data transmissions are monitored by MILAC personnel to observe that no erroneous information is being fed to the system by an errant enemy source. Furthermore, aircraft /ROOT ACCESS requires a high level manual password validation that would allow the user more then simple "use" of the software and transmitting authorized data forms (passing and receiving information from various programs). If such authorization cannot be acquired within five tries, the system invokes an F-DISK and destroys the hard-drive, destroying all internal code and the ability of the unit to interact via networking. Access to this screen requires it's own separate pass code to avoid accidental or sabotage based attacks, this has an unlimited number of tries, but would be impossible to enter without a proper code (only valid for the hour of it's entry). 3. In the event that a system within the network is considered compromised, the system can be cut off manually from a central network from the inside given the proper authorization codes. The system will not take effect on aircraft however, until it has safely landed on the ground. The on-board electronics, such as the hard-drive, cannot be removed from the system without proper coded authorization (similar to the /ROOT authorization protection), such systems are in place to prevent the physical removal of critical pieces of hardware and subsequent analysis by an external separately built device. All of this works to create an extremely secure defense around the working network, to prevent unwanted access by enemy forces. AIRCRAFT DESIGN AND LOW OBSERVABILITY CHARACTERISTICS 1. The F/A-0 utilizes a LOW OBSERVABLE TECHNOLOGY throughout the design of the aircraft to minimize it's RADAR cross section, IR signature, visual image and sensor systems. VEHICLE SHAPE attributes reflect RADAR off the aircraft at large angles, reducing returns and an S-Shaped air intake reduces the returns from the turbo-fans, while a thin layer of conducting Indium-Tin-Oxide, reduces the RCS of the cockpit. The hybrid control/close-coupled canard system is highly swept, with software control tailored to automatically manage and reduce the increased RCS they threaten the airframe with. The tailless design of the Widow also contributes to an all aspect RCS. 2.IR emissions from the engine are reduced by avoiding a circular tailpipe, such as the slit tail-pipe design found on the F-23 Black Widow and F-22 Raptor. This engine design also finds it's way onto the Brown Widow, which helps to reduce the aircraft's vulnerability to IR detection stations and heat-seeking missiles. The advent of optical systems also requires further stealth characteristics, which is why aircraft coloring scheme is designed to prevent shadows and blend into it's environment ((OOC: via the same techniques used on the Bird of Prey demonstrator)). 3. However, for the sake of protecting our critical resources, Air Militant Command often recommends that one or even two BLACK WIDOW ace pilots accompany each squadron, providing additional cover from an off-formation vector. Ever vigilant but not directly visible, these aircraft serve several purposes. They provide dedicated air-combat focused specialists on the field, the Black Widows can act as "mini-AEWACS", and they also provide increased endurance on the battlefield in intense air-combat situations because of their larger fuel capacity. 4. The largest radar reflector on the frontal aspect of a fighter is the compressor turbine. In order to compensate for this source of detection, there is a perceived misalignment of the turbine in relation to air intakes. This prevents radar waves from directly reaching the compressor. The result is a very small frontal RCS due to the curvature of the airducts of the turbine. 5. Exhaust from the single power plant flows through a winding path within the airframe of the F/A-0. Along this path, the troughs are lined with heat ablating materials which in turn feeds the heat into the main combustion cavity. The exhaust is shielded from infrared missile detection from below. 6. The majority of the BLACK WIDOW's airframe is built with composite materials opposed to conventional metallics. While this does not aid in the ease of production, it was determined that unless catastrophic damage has been incurred by an airframe, export clients would not necessarily need to deal with such concerns. Furthermore, 3D-Manufacturing technology would serve to consolidate all construction woes into a single, easier to manage package, allaying cost and intricacy concerns somewhat. 7. Low wing aspect ratio is used to optimize supercruise performance. The tailless aspect of the Widow lends itself not only to a reduced RCS, but also reduced mechanical complexity and greater agility due to inherent instability. Longitudinal control is facilitated by the hybrid canards at a zero angle of attack. At high angles of attack the canard surface directs airflow downwards over the wing, reducing turbulence and drag while increasing lift in both supercruise and low speed flight. [size="3"][b]Neptune Hypersonic Missile[/b][/size] Weight 1500 kg 1000 kg (air-launched) Length 8.4 m Diameter 0.6 m Warhead 300 kg Conventional semi-armour-piercing Engine Two-stage integrated Rocket/Ramjet Operational range 1600 km Flight altitude Sea-skimming as low as 10 m (30 feet) Speed Mach 7.0 Launch platform Ship, submarine, aircraft and land-based mobile launchers. [b]Neptune I ICBM[/b] Weight 100,000 Length 70 ft Diameter 7 ft Warhead 500 kt Fission Warhead Detonation mechanism Airburst Engine Two-stage liquid propellant Operational range 10,000 miles Speed Mach 20 (15400 mph) Guidance system Inertial, autonomous Accuracy 220–700 m CEP (depending on R-36M missile variants) Launch platform Silo [size="3"][b]Neptune Supersonic Missile[/b][/size] Weight 1250 kg 800 kg (air-launched) Length 8.4 m Diameter 0.6 m Warhead 200 kg Conventional semi-armour-piercing Engine Two-stage integrated Rocket/Ramjet Operational range 1600 km Flight altitude Sea-skimming as low as 10 m (30 feet) Speed Mach 2.6 Launch platform Ship, submarine, aircraft and land-based mobile launchers. [size="3"][b]Sukhoi SU-37 Multi-role Fighter[/b][/size] General characteristics Crew: 1 Length: 19.8 m (65.9 ft) Wingspan: 14 m (46.6 ft) Height: 6.05 m (19.8 ft) Wing area: 78.8 m2 (848.1 ft2) Empty weight: 18,500 kg (40,785 lb) Loaded weight: 26,000 kg (57,320 lb) Useful load: 7,500 kg (combat load) (16,534 lb) Max. takeoff weight: 37,000 kg (81,570 lb) Powerplant: 2 × AL-41F1 for prototypes[N 1][91] turbofan, 147 kN (33,047 lb) for prototypes;[92] 157+ kN (34,620+ lbf) for definitive engine version[92] each Fuel capability: 10,300 kg (22,711 lb)[89] Performance Maximum speed: Mach 2+, 2,100-2,600 km/h[89][93][91] (1,300-1,560 mph) ; at 17,000 m (45,000 ft) altitude Cruise speed: 1,300-1,800 km/h[91] (808-1,118 mph) Ferry range: 5,500 km[79] (3,417 mi) Service ceiling: 20,000 m (65,600 ft) Rate of climb: 350 m/s (68,900 ft/min) Wing loading: 330-470 kg/m2 (67-96 lb/ft2) Thrust/weight: 1.19[89] Maximum g-load: -3/9+ g[89] Armament S-25LD laser-guided rocket KAB-500L laser-guided bomb KAB-1500 laser-guided bomb LGB-250 laser-guided bomb Kh-31: Kh-31A, Kh-31P Anti-Radiation Missile 1 × 30 mm GSh-30 internal cannon with 150 rounds 2 × wingtip rails for R-73 air-to-air missiles or ECM pods 12 × wing and fuselage stations Avionics BRLS AFAR/AESA built by Tikhomirov NIIP and based on Tikhomirov NIIP N035 Irbis-E. It will be the second aircraft based AESA Radar to be built by Russia, the first being the Phazotron NIIR ZHUK-A Radar in the MiG-35.[94] [b]Classified[/b] New RADAR specs [size="3"][b]AESA[/b][/size] air target tracking of over 200 targets out to 150 km[2] surface target tracking of over 150 targets out to 32 km[2] horizon search out to 75 km[2] "limited" volume search out to 150 km[2] (in order to back up the volume search capabilities of the SMART-L) cued search (a mode in which the search is cued using data originating from another sensor) surface gunfire support[2] missile guidance using the Interrupted Continuous Wave Illumination (ICWI) technique, thus allowing guidance of 32 semi-active radar homing missiles in flight simultaneously, including 16 in the terminal guidance phase[3] "innovative" Electronic Counter-Countermeasures (ECCM) Low Probability of Intercept Radar systems work by sending out a signal and then listening for its echo off distant objects. Each of these paths, to and from the target, is subject to the inverse square law of propagation. That means that a radar's received energy drops with the fourth power of distance, which is why radar systems require high powers, often in the megawatt range, to be effective at long range.[1] The radar signal being sent out is a simple radio signal, and can be received with a simple radio receiver. It is common to use such a receiver in the targets, normally aircraft, to detect radar broadcasts. Unlike the radar unit, which must send the pulse out and then receive its reflection, the target's receiver does not need the reflection and thus the signal drops off only as the square of distance. This means that the receiver is always at an advantage over the radar in terms of range - it will always be able to detect the signal long before the radar can see the target's echo. Since the position of the radar is extremely useful information in an attack on that platform, this means that radars generally must be turned off for lengthy periods if they are subject to attack; this is common on ships, for instance. Turning that received signal into a useful display is the purpose of the "radar warning receiver" (RWR). Unlike the radar, which knows which direction it is sending its signal, the receiver simply gets a pulse of energy and has to interpret it. Since the radio spectrum is filled with noise, the receiver's signal is integrated over a short period of time, making periodic sources like a radar add up and stand out over the random background. Typically RWRs store the detected pulses for a short period of time, and compare their broadcast frequency and pulse repetition frequency against a database of known radars. The rough direction can be calculated using a rotating antenna, or similar passive array, and combined with symbology indicating the likely purpose of the radar - airborne early warning, surface to air missile, etc. This technique is much less useful against AESA radars. Since the AESA can change its frequency with every pulse, and generally does so using a pseudo-random sequence, integrating over time does not help pull the signal out of the background noise. Nor does the AESA have any sort of fixed pulse repetition frequency, which can also be varied and thus hide any periodic brightening across the entire spectrum. Traditional RWRs are essentially useless against AESA radars. [edit]High jamming resistance Jamming is likewise much more difficult against an AESA. Traditionally, jammers have operated by determining the operating frequency of the radar and then broadcasting a signal on it to confuse the receiver as to which is the "real" pulse and which is the jammer's. This technique works as long as the radar system cannot easily change its operating frequency. When the transmitters were based on klystron tubes this was generally true, and radars, especially airborne ones, had only a few frequencies to choose among. A jammer could listen to those possible frequencies and select the one to be used to jam. Since an AESA changes its operating frequency with every pulse, and spreads the frequencies across a wide band even in a single pulse, jammers are much less effective. Although it is possible to send out broadband white noise against all the possible frequencies, this means the amount of energy being sent at any one frequency is much lower, reducing its effectiveness. In fact, AESAs can then be switched to a receive-only mode, and use these powerful jamming signals instead to track its source, something that required a separate receiver in older platforms. AESA radars can be much more difficult to detect, and so much more useful in receiving signals from the targets, that they can broadcast continually and still have a very low chance of being detected. This allows such radar systems to generate far more data than traditional radar systems, which can only receive data periodically, greatly improving overall system effectiveness. [edit]Other advantages Since each element in a AESA is a powerful radio receiver, active arrays have many roles besides traditional radar. One use is to dedicate several of the elements to reception of common radar signals, eliminating the need for a separate radar warning receiver. The same basic concept can be used to provide traditional radio support, and with some elements also broadcasting, form a very high bandwidth data link. The F-35 uses this mechanism to send sensor data between aircraft in order to provide a synthetic picture of higher resolution and range than any one radar could generate. In 2007, tests by Northrop Grumman, Lockheed Martin, and L-3 Communications enabled the AESA system of a Raptor to act like a WiFi access point, able to transmit data at 548 megabits per second and receive at gigabit speed; this is far faster than the Link 16 system used by US and allied aircraft, which transfers data at just over 1 Mbit/s.[2] AESAs are also much more reliable than either a PESA or older designs. Since each module operates independently of the others, single failures have little effect on the operation of the system as a whole. Additionally, the modules individually operate at low powers, perhaps 40 to 60 watts, so the need for a large high-voltage power supply is eliminated. Replacing a mechanically scanned array with a fixed AESA mount (such as on the F/A-18E/F Super Hornet) can help reduce an aircraft's overall radar cross-section (RCS), but some designs (such as the Eurofighter Typhoon) forgo this advantage in order to combine mechanical scanning with electronic scanning and provide a wider angle of total coverage [size="3"][b]OTH[/b][/size] Radar Type FM/CW Bistatic Doppler Antenna Types Horizontal Linear Phased Arrays Maximum CW Radiated Power 1,000,000 W (12 transmitters) Effective Radiated Power 80 dBW (100 MW) Transmit Array Design Canted Dipoles, Vertical Backscreen Transmit Frequency 5-28 MHz in 6 Bands Transmit Array Elements 12 per band Subarray Apertures 304, 224,167,123, 92, 68 m Transmit Azimuth Beamwidth (3 dB) 7.5 deg Transmit Elevation Beam (3-dB points) 8-33 deg @ 5 MHz, 5-15 deg @ 28 MHZ Transmit Azimuth Beam Steer �30 deg Receive Array Design 246 5.4-m Vertical Elements with 20-m Backscreen Receive Frequency 5-28 MHz in 3 Bands Receive Array Aperture 1519, 1013, 506 m Number of Active Receive Elements 82 Receive Azimuth Beamwidth (3 dB) 1.25 deg (no weighting), 2.5 deg (raised-cosine weighting) Receive Elevation Beam (3-dB points) 8-33 deg @ 5 MHz, 5-15 deg @ 28 MHZ Receive Azimuth Beam Steer �30 deg ECRS Receive Location 44.79 N, 67.79 W ECRS Azimuth Limits (modified) 31.5-91.5-151.5-211.5 deg East of North ECRS Transmitter-Receiver Separation 160 km ECRS Operations Center Bangor ANGB, ME WCRS Receive Location 41.70 N, 121.18 W WCRS Azimuth Limits (3 segments) 160-220-280-340 deg East of North WCRS Transmitter-Receiver Separation 160 km WCRS Operations Center Mountain Home AFB, ID Waveform Repetition Frequency 10-60 Hz Waveform (chirp) Bandwidth 5-40 kHz Coherent Integration Time 0.7-20.5 s [size="3"][b]DEW[/b][/size] Frequency range 1220–1350 MHz Peak power output 160 kW Average power output -400 W Pulse rate 400 pulses/per second Pulse width 6.0 usec Range 1000 yard to 160 nmi Antenna radiation pattern Horizontal 2.8 degrees Vertical cosecant (elevation single) Receiver noise figure 11.7 db IF bandwidth and frequency 5 MHz at 60 MHz Required prime power 8.5 KW Approximate weight of Radar 4800 lb Total volume 1000 ft to the third [size="3"][b]1. Tor Missile System[/b][/size] [b]-Launch Pad[/b] Weight 34 tonnes Length 7.5 m Width 3.3 m Height 5.1 m (radar mast unstowed) Crew 3 Main armament 9M330, 9M331 Engine V-12 diesel 618 kW (830 hp) Suspension torsion bar Ground clearance 450 mm Operational range 500 km Speed 65 km/h [b]-Missile[/b] Weight 167 kg Length 2900 mm Diameter 235 mm Warhead Frag-HE Warhead weight 15 kg Detonation mechanism RF Proximity Propellant Solid-fuel rocket Operational range 12 kilometres (7.5 mi)[11] Flight altitude 6,000 metres (20,000 ft) Boost time Cold launch ejection for 20 m Speed 850 m/s Guidance system Radio command Steering system Gas dynamic control system, with four control surfaces Launch platform 9A331 combat vehicle Transport GM-569 tracked vehicle [size="3"][b]2. Buk-M2 Missile System[/b][/size] Missiles Per TEL: 12/24/36 Missile Weight: 581kg Engagement Range: 2-50km Engagement Altitude: 15-25,000 m Missile Speed: Mach 4.5 Maximum Target Speed: Mach 6 Maximum Maneuverability: 25 G Simultaneous Engagements: 6 [size="3"][b]3. S-300V [/b][/size] The "GLADIATOR" missiles have a maximum engagement range of around 75 km (47 mi) while the "GIANT" missiles can engage targets out to 100 km (62 mi) and up to altitudes of around 32 km (100,000 ft). In both cases the warhead is around 150 kg (331 lb). While it was created from the same project (hence the common S-300 designation) different priorities resulted in a design quite different from the other versions. The S-300V system is carried on tracked MT-T transporters, which gives it better cross-country mobility than even the S-300Ps on 8x8 wheeled transporters. It is also somewhat more distributed than the S-300P's. For example, while both have mechanically-scanned radar for target acquisition (9S15 BILL BOARD A), the battery level 9S32 GRILL PAN has autonomous search ability and SARH delegated to illumination radar on TELARs. The early 30N6 FLAP LID on the S-300P handles tracking and illumination, but is not equipped with autonomous search (later upgraded). The S-300V places a greater emphasis on ABM, with the dedicated 9M82 (SA-12B Giant). This missile is larger and only two can be held on each TELAR. It also has a dedicated ABM radar – the 9S19 HIGH SCREEN phased array radar at battalion level. A typical S-300V battalion is made up out of a target detection and designation unit, a guidance radar and up to 6 TELARs. The detection and designation unit consists of the 9S457-1 command post, a 9S15MV or 9S15MT BILL BOARD all-round surveillance radar and 9S19M2 HIGH SCREEN sector surveillance radar.[9] The S-300V uses the 9S32-1 GRILL PAN multi-channel guidance radar. Four types of missile-launcher vehicles can be used with the system:[10] Transporter erector and radar (TELAR) vehicles, which not only transport the missiles, but also fire and guide them. There are two models: the 9A83-1 TELAR holding four 9M83 GLADIATOR missiles and the 9A82 TELAR holding two 9M82 GIANT missiles.[10] Launcher/loader vehicles (LLV), which transport the missiles and can reload the TELARs, and also fire missiles under the control of a TELAR. There are two models: the 9A84 LLV holding two 9M83 GLADIATOR missiles and the 9A85 LLV holding two 9M82 GIANT missiles.[10] S-300V system may be controlled by a upper level command post system 9S52 Polyana-D4 integrating it with Buk missile system into a brigade. [size="3"][b]4. GMD Missile[/b][/size] Exoatmospheric Kill Vehicle (EKV) Ground Based Interceptor (GBI); for every interceptor missile there is a missile silo and a Silo Interface Vault (SIV), which is an underground electronics room adjacent to the silo. Battle Management Command, Control and Communications (BMC3) Ground Based Radars (GBR) Upgraded Early Warning Radars (UEWR) (aka PAVE PAWS) Forward Based X-Band Radars (FBXB) such as the Sea based X band platform [size="3"][b]5. S-450[/b][/size] Ceiling: 175km Radar Range: 1,500km Missile Range: 600km Speed: Mach 11 [size="3"][b]LY67 'Widowmaker' 40mm grenade launcher[/b][/size] Weight: 1.7 kg (3.3 lb) Length: 520 mm (20.47 in.) Barrel length: 400 mm (15.7 in.) Cartridge: LY1020-series 40x43mm Action: stacked-projectile, electronically-fired, caseless multishot system Rate of Fire: 120 rounds per minute (cyclic) 45 rounds per minute (rapid) Muzzle velocity : 76 m/s Effective range (point targets): 250 m Maximum range (with ER ammunition): 700 m Feed system: tubular integral magazine [b]Safety system[/b] The first is a simple push-through safety, similar to that of the LY21. With the safety set to ‘safe’, the trigger is not able to be pulled to the rear. Further, not only can the trigger not be pulled, but the electrical system that controls the ignition sequence passes through the safety. Should it be set to safe, the circuit is not completed, and the weapon may not fire. Should the weapon be set to fire, it still may not do so unless the trigger is pulled, again by means of circuit completion. For safety DURING firing a microchip is used in the same manner as the earlier MS3GL. It is located at the barrel muzzle, and detects the passage of each projectile and locks the firing mechanism (of each subsequent shell) until the fired shell has cleared the muzzle. Further, and lastly, the rounds themselves do not arm until 6m clear of the muzzle, by default, to prevent self-harm. The simple impact, of course, will still have an effect. The weapon’s safety and readiness state is provided by a backlit display on the rear of the weapon’s battery port. The illumination is activated by a simple toggle switch. [size="3"][b]Neptune I Missile Boat[/b][/size] Type: Fast attack craft Displacement: 950t (full load) Length: 95m (LOA) Beam: 14m (BOA) Draft: 2m Installed power: 32MW Propulsion: 2 x NBP 45KL Diesel Engines 2 x Waterjets Speed: 36 knots Range: 3,500km Complement: 18 officers 60 crew 12 airwing Sensors: NBMI Sea and Air Search, 2 Arrays, 2 Antennas NBMI 41 Radar Warning Receiver Sonar Equipment Navigation Equipment Armament: 1 x 55mm autocannon 4 x 12.7mm machineguns 12 x Mk. 41 VLS (SM-2, Tomahawk, Harpoon, quad-ESSM etc) Armor: Armoured against shrapnel and light autocannons. Aircraft carried: 1 Light helicopter [size="3"][b]LY47 'Stormhammer' SMG[/b][/size] Weight, unloaded: 3.35kg Weight, loaded: 4kg Length: 559mm (22 inches) Barrel length: 254mm (10 inches) Cartridge: 12.7mm x 35mm caseless telescoping (.50 Lyran CaseLess) Action: gas-operated, balanced automatic, closed-bolt Rate of fire: semi-automatic, 600 rpm automatic. Muzzle velocity: 460m/s Muzzle energy: 2284.5 J Effective range: 100m Feed system: twin-single stacked, 30rnd magazine Sights: dorsal picatinny rail. [size="3"][b]LY23 'Songbird' 14.7mm Anti-Materiel Rifle[/b][/size] Weight: 7.6kg (unloaded) Length: 1550mm Barrel length: 800mm Cartridge: 14.7mm x 115mm (14.7 Lyran) Action: semi-automatic, gas operated, rotating bolt, long-recoil Rate of fire: 400rpm (cyclic) Muzzle velocity: 1030 m/s Effective range: ~2,000 m Maximum range: ~2,700m Penetration: ~40mm RHAe @ 500m. ~25mm RHAe @1000m. Feed system: 5rd detachable box or 10 rd drum [size="3"][b]LY20 High Lethality Assault Rifle[/b][/size] Weight: 4.0 kg (unloaded), 4.4 kg (unloaded) Length: 1015mm (41 inches) Barrel length: 675mm (27 inches) Cartridge: 6.5 x 45mm JMC Mk5 Action: gas operated, rotating bolt (2 lugs), balanced automatic recoil system Rate of fire: 700rpm (cyclic) Muzzle velocity: 880 m/s Effective range: 600 m Feed system: 30 rd detachable box (top feeding) Sights: Aperture rear, hooded post front. Picatinny rails allow alternates. Sights: Aperture rear, hooded post front. Picatinny rails allow alternates. [size="3"][b]Atlantis M-1[/b][/size] Length: 4.8m Height: 2m Width: 2m Weight: 5 tonnes Ground Clearance: Variable. Default at 50cm Performance Maximum rated speed: 140 kph (87.5mph) Cross Country Speed: 55 kph Speed, 10% Slope: 125 kph Speed, 60% slope: 45 kph Towing capacity: 5.9 tonnes Range: 590 km (efficiency setting) Suspension: Independent double a-arm. Armament Weapon Station: 2 gunrings for a variety of weapon systems, optional use of remote weapon stations. Power Propulsion: 8L LY694 multifuel, propane-injected, twin-turbocharged V8 350hp (197kW) diesel-electric. Transmission: Automatic transmission (6 fwd gears, 2 rvse) Power-to-Weight Ratio: 87.5hp/ton Armour and Protection Armour Internal modular armour, sacrificial anti-mine segments NBC Protection SCFM, clean cooled air, LYMkII CBRN overpressure system. [size="3"][b]Atlantis Air Annihilator[/b][/size] Primary Function: Surface-to-air missile Propulsion: Solid propellant rocket motor and attitude control motors (180 very small solid propellant rocket motors) Length: 204.7 in (5.2 m) Diameter: 9.8 in (25 cm) Wingspan: 20.1 in (51 cm) Weight: 700 lbs (318 kg) Speed: Mach 5+ Range: 10.8 nm/12.4 miles (20 km) Seeker: Ka band active radar seeker Guidance System: Inertial guidance (INS) Warhead: "Hit-to-kill" lethality enhancer explosive warhead The system contributes to the Ballistic Missile Defense System's overall situational awareness for short range terminal ballistic missile threats. It can cue other systems while protecting BMDS assets. The Patriot system is further enhanced by networked BMDS remote sensors supplying early warning data, thus, increasing the probability of successful threat engagement. The PAC-3 units are the combatant commanders' most capable system to protect soldiers, allies, and assets against these threats. The PAC-3 consists of the PAC-3 missile, the PAC-3 missile canisters (in four packs), a fire solution computer and an Enhanced Launcher Electronics System (ELES). These elements are integrated into Patriot Missile System, a high to medium altitude, long-range air defense missile system providing air defense of ground combat forces and high-value assets. The heart of the Patriot Missile System is the fire control section, which consists of the AN/MPQ-65 Radar Set, the AN/MSQ-104 Engagement Control Station (ECS), the OE-349 Antenna Mast Group (AMG), and the EPP-III Electric Power Plant. The missiles are transported by and launched from the M901 Launching Station (mounted on M860 semi-trailers and towed by the M983 HEMTT Patriot Tractor), which carries up to sixteen PAC-3 missiles. The task of the AN/MPQ-65 Radar Set (mounted on M860 semi-trailers and towed by the M983 HEMTT Patriot Tractor) is to sweep the sky for enemy threats and determine whether the incoming object is an aircraft, missile, or UAV. The AN/MPQ-65 is a passive electronically scanned array radar. From the AN/MSQ-104 ECS, a crew of three operators communicate and monitor/prioritize threats. The ECS consists of a shelter mounted on the chassis of the M927 Medium Tactical Vehicle or on the chassis of a Light Medium Tactical Vehicle (LMTV). The OE-349 AMG is mounted on the chassis of a M927 Medium Tactical Vehicle. It includes four 4 kW antennas in two pairs on remotely controlled masts. The EPP-III Diesel-Electric Power Plant is the power source for the ECS and Radar Set. The EPP consists of two 150 kW diesel engines interconnected with 400 hertz generators. The generators are mounted on a modified M977 HEMTT. When launched, the PAC-3 missile flies to an intercept point specified prior to launch by its ground-based fire solution computer. Target trajectory data can be updated during flyout by the means of a radio frequency uplink/downlink. Shortly before arrival at the intercept point, the missile's on board Ka band seeker acquires the target, selects the optimal aim point and initiates terminal guidance. The attitude control motors, located in the missile forebody, fire explosively to refine the PAC-3 missile's course to assure direct body-to-body impact. [size="3"][b]Atlantis I Frigate[/b][/size] Displacement: 5,500 tonnes, standard Length: 148 m (489 ft 6 in) Beam: 19 m (62 ft 1 in) Speed: 28+ knots Range: 11,265 km (7,000 miles) at 15 knots (28 km/h) Endurance: 60 days Troops: 36 embarked troops Complement: 130 Sensors and processing systems: Artisan 3D search radar Sonar 2087 (towed array sonar) Armament: Anti-air missiles; Sea Ceptor air-defence missile system. A 16 cell VLS with provision for up to 64 Sea Ceptor missiles (range 1-25 km)[1] Anti-ship missiles; 2× quadruple anti-ship missile launchers. (possibly 8 Harpoon anti-ship missiles) Anti-submarine torpedoes; A torpedo launching system. (possibly armed with Stingray torpedoes) Any missile in Atlantis inventory Guns; 1× 127mm Medium calibre gun, or, 1× BAE 4.5 inch Mk8 gun 2× 30mm DS30M automated guns 2× Miniguns 4× General-purpose machine guns Aircraft carried: 1×Lynx Wildcat, armed with; anti ship missiles (possibly Sea Skua), or anti submarine torpedoes or 1×Westland Merlin, armed with; 4× anti submarine torpedoes Aviation facilities: Flight deck Enclosed hangar Accommodation for UAVs [size="3"][b]XF-32 GREY WIDOW[/b][/size] [b]General Characteristics & Performance[/b] Crew: 1 Powerplant: 2 x MILAC F135-100 Afterburning turbofan Cruise Speed: Mach 2.0 Max Speed: Mach 2.8 Combat Radius: 5,500 km Maximum Design g-Load: 9 g 1. The XF-32 "GREY WIDOW" is a 5th+++ generation, fully operational test bed for the AU's JOINT SIXTH GENERATION AIR SUPERIORITY project developed by MILITARY AVIATION COMPLEX (MILAC) in collaboration AIR MILITANT COMMAND (AMC). It is designed as a fully capable platform capable of delivering a high volume of air to air ordinance in order to gain allied air supremacy. It has a secondary role of a high endurance ECM, ELINT ECCM aircraft, while also serving as an usher to newer advancements to continue developing the AFRICAN UNION's CONSOLIDATED AIRFORCE into a formidable fighting force. Utilizing the lessons learned by its immediate cousin, the F/A-0 "BROWN WIDOW" the XF-32 has a tailless all-aspect broadband stealth airframe, a pair of IR-shielded thrust-vectoring engines, while forgoing the BROWN WIDOW's hybrid control/close-coupled canards for enhanced low and top aspect radar profiles. 2. The "GREY WIDOW" carries the large assortment weapons its cousin does, while retaining a larger design for both fuel and operational range. It is intended to replace, or help develop a replacement for the air-dominance role currently held by the F-23 BLACK WIDOW. It leaves AIR INTERDICTION, TACTICAL ground attack and CLOSE AIR SUPPORT to the F/A-0 and priority interdiction sorties to the A-1 KRIEG. 3. The aircraft is designed to be easy to fix and maintain by utilizing a standard set of equipment present in both the F-23 BLACK WIDOW and F/A-0 BROWN WIDOW. It is designed for ease of procurement while shirking none of the performance, enhancing the ability of the AU to both mass produce airframes and parts with a cheaper long-term maintenance plan for the trio of aircraft. The GREY WIDOW is the second aircraft designed from conceptual stages to be primarily a full capability export aircraft, with production rights solely given to allied states. 4. THIS AIRCRAFT IS DESIGNED TO IMPLEMENT THE STANAG (STANDARD AGREEMENT) AND FULL INTEGRATION OF THE AFRICAN UNION COMBINED FORCES COMMAND (COMFOR) TOGETHER WITH THE AFRICAN UNION SECURITY FORCES (AUSF) INTO A COHESIVE PAN-AFRICAN MILITARY FORCE. IT IS A PRIMARY AIR DOMINANCE FIGHTER WITH EMPHASIS ON USAGE IN NORTH AND EAST MILITARY AIR OFFENSIVE ROLES AND A DEFENSIVE ROLE ACROSS THE AFRICAN CONTINENT. [b]COCKPIT[/b] 1. The Cockpit of the MILAC XF-32 features a roomy "glass-cockpit" design. Commands can be entered manually or via an integrated "user dependent" Adacel DVI (Direct Voice Input) system which accepts commands from the pilot verbally. The plane also contains a full-panel-width "cockpit panoramic display" to display warnings, RADAR systems, sensor-fuzed identification, targeting and tracking information and other relevant stimuli. The on-board computer can accesses an INTERNAL REFERENCE SYSTEM (IRS), which provides color and shape coordinated information on an enemy aircraft type and provides CURRENT battlefield knowledge of the maximum enemy RADAR detection range (yellow line) and missile range (red line). Overlapping enemy RADAR and missile regions are combined to avoid user clutter and the pilot is informed via a HELMET MOUNTED DISPLAY SYSTEM (HDMS) when they have fallen into either. Pilots can also use touch screen commands to share information with other pilots, by clicking on particular targets, or setting way-points at their command allowing for a fluid flow of information from one pilot to the group during a conversation (priority being given to the group leader). 2. All planes will utilize a HELMET MOUNTED DISPLAY SYSTEM (HMDS) to display enemy aircraft with missile systems cued to lock on by simply looking in the direction of the desired target if desired via combination of HIGH OFF-BORESIGHT weapons (HOBS). Alternative methods that can be sent to the FIRE CONTROL SYSTEM (FCS) including "manual" or "automatic" target selection. The aircraft contains a HEADS UP DISPLAY (HUD) system as a back up, relying primarily on the HMDS to convey information to the pilot. 3. All aircraft are equipped with a MARTIN-BAKER US16E ejection seat. Furthermore, control of the aircraft utilizes a right hand stick controller and a left throttle control. [b]FIRE CONTROL SYSTEM (FCS) XN8 AND NETWORKING [/b] 1. The FCS XN8 fire control system is an upgraded version of the XN7 present on the BROWN WIDOW based on the enhanced electronics warfare capability of the GREY WIDOW. The aircraft is designed to acquire and track up to 75 targets air, land and sea on the COCKPIT DISPLAY PANEL and HMDS, and fire up to twelve weapons simultaneously. Target acquisition is performed utilizing a combination of continuous radio-frequency and Infra-red tracking systems via SAIRST. Autonomous tracking for standoff weapons and further enemy information can be acquired via an onboard ELECTRO-OPTICAL TRACKING SYSTEM (EOTS) (OOC: Stealthy version of this) and IIDU based sensors. In combination, this array of sensors integrates with the FCS to provide full HIGH OFF-BORESIGHT weapon (HOBS) capabilities to all weapons - making aircraft orientation unimportant. The combined might of this multi-spectrum sensory information is realized as a sensor-fused advancement of the contemporary Target Acquisition System Software (TASS) utilized in the BLACK WIDOW, a marked improvement incorporating both legacy Nodic as well as modern Aeon advancements into a single cohesive package. 2. These systems are designed to work with a local "Group AEWACs", local group networks or space based networks via a MULTIFUNCTION ADVANCED DATA LINK (MADL), which transmits data between the planes and various military networks without compromising stealth features of the plane. The application of a satellite based WIDE AREA NETWORK (WAN), which can transmit data at 848 megabits per second and receive at gigabit speeds, allows for pilots to have full battlefield combat situational awareness and at the same time allows them to focus in on a smaller region to handle threats or objectives closer to home. The system provides pilots the full range of sensory information acquired by other secured network aircraft, AEWACs, AUSF DETECTION EARLY WARNING (DEW) Long and Short Range RADARs along with ground support from AUSF Air Support mobile RADARs and IR DETECTION STATIONS, SPECTATOR CLASS MILITARY SATELLITES and other detection networks validated by the AMC and the AUSF. When combined with BEYOND VISUAL RANGE missiles, the FCS and Networking system allows the pilots to even target and fire on enemies outside of their current sensor range, using the other systems information as the targeting system to acquire a "lock". 3. Networking is also a valuable system here as it can automatically assign targets to each individual missile according to priority, and the weapon best designed for the given target via a INTERNAL REFERENCE SYSTEM (IRS) which is continuously updated during combat operations via the network grid so pilots can have the best understanding possible of the enemy. This allows the group to utilize it's munitions to their fullest potential by rapidly assigning each weapon a unique target and allowing them an instant opportunity to fire or disregard each target at their discretion. With proper authorization, the system also has an auto-fire command allowing weapons to be fired as soon as the system has a lock-on on a non-friendly IDENTIFICATION FRIEND OR FOE (IFF) signature that has been designated as that systems target. It also allows pilots to enter the combat situation with an optimal understanding of the enemy as interactions occur on the battlefield. 4. The FCS system will also be able to make optimum use of new LOCK-ON AFTER LAUNCH (LOAL) capable missiles, allowing the user to fire the missile at the general vicinity of the target and then program the target into the missile after it is already in flight (also critical for internal bay launched missiles), or even allowing said missile to acquire a lock on its own via active seeking or networked tracking information from allied platforms. After launch, programming capabilities also allow for "nape of the earth" near-surface combat attack orientations. These allow the aircraft to fire upon enemy forces near the ground while using terrain as an active cover. On board navigation systems will soon also allow the programming of a BEYOND VISUAL RANGE (BVR) missile's flight trajectory so that it acts as a temporary "cruise-mode" before rising up to strike at it's opponents in the distance. [b]ON-BOARD NAVIGATION SYSTEM [/b] 1. The on-board navigation system utilizes a RING LASER GYROSCOPIC INERTIAL NAVIGATION SYSTEM combined with on-board GPS positioning (developed from the lessons learned from MILAC's Deathstalker). On-board systems determine the aircraft's location in space on Earth, allowing the pilot to know their position at all times relative to their environment. The aircraft also has an AUTOMATIC GROUND-COLLISION AVOIDANCE SYSTEM (Auto GCAS). This system allows the aircraft to safely navigate along the "nape of the earth", utilizing terrain features to reduce the probability of detection by hostile forces and allowing for deep penetration into enemy territory. [b]ARMARMENT [/b] 1. The larger size of the GREY WIDOW, provides a significant internal weapons bay, providing room for up to ten weapons mounts opposed to eight, as found on the F-23 Black WIDOW. It complements its fire-power by opting to fit two small diameter bombs or SIR-73/74 class weapons on each hardpoint. Gun: 2 x 30mm Lancer auto-cannon, 540 CTA rounds Missiles: Aim 9x Sidewinder, SIR-73, SIR-74AC and SIR-74AC-ER, JAGM Missile, AGM-84 Harpoon, AGM-88E AARGM, AGM-154 JSOW, MBDA Meteor, SARAH-37 Missile, ADM-160A MALD , SEAD-MA and SEAD-MA-EM, 'Punisher' Tactical Assault Missile(TAM) Bombs: CBU-100 Cluster Bombs, JDAM Series, Mark 82, 83 and 84 GPBs, Paveway Series Bombs , Small Diameter Bombs All craft are additionally armed with chaff and flares for aircraft defense. More advanced defensive systems are as follows: 4 x Tanzanian Arms AN/AAQ-24 directional infrared countermeasure (DIRCM) system AN/AAR-54 missile warning system Small Laser Targeting Assembly (SLTA) 6 x Dorsal Bay mounting TA/MILAC 'mini-Nulka' cold launched Active Radar Expendable Decoy (ARED) 6 x ALE-50 Towed Decoy System NEXT GENERATION JAMMING AND CYBERATTACK 1. The GREY WIDOW mounts a NEXT GENERATION PLUS JAMMER (NGPT) system, designed to escort stealthy and non-stealthy aircraft to the edge of an enemy threat zone, jamming radars used by the enemy to launch munitions at allied targets. The NGPT is designed to open the envelope of safety given to allied units in order to successfully deploy stand-off attack munitions, escape a projected kill zone, or mount concerted close-in attacks to destroy high priority targets. The AESA based NGPJ system is designed to exploit electronic warfare, operating across a broad swath of the electromagnetic spectrum. This electronic surveillance and attack system utilizes the very skin of the GREY WIDOW as a giant AESA array, breaking it up into several 'sectors', elements that are steerable, directable and assignable in frequency. Each sector is tasked for use in differing functions, as well as for pointing at differing targets. In addition, this section based system can be used in its totality to provide a very high power capability, producing nearly three times the power in a much smaller package. 2. The NGPT is capable of directing its energy in a concerted attack against sensitive enemy electronics. In addition, it is capable of inserting malicious information into enemy data streams, allowing for suppression of enemy intelligence gathering assets or their outright disablement. 3. The NGPT addresses the dual nature of the code insertion capability AESA based systems are vulnerable to. The NGPT integrates a protective, intelligent countermeasure system to guard against such cyberattacks. This system practices secured input and output handling to ensure defense against compromisation. It includes: - Input validation against a secured and duplicated database of known/accepted inputs - Proactive conversion of potentially dangerous input code into standardized, safe characters - Input and output encoding - Utilizing a unique, indigenously produced programming language that draws heavily upon 'prepared statements', 'bound variables' and 'bound values' The successes encountered with the NGPT during the GREY WIDOW program have been deployed to legacy systems and will be included in future systems employed by the AUSF. [b]RADAR, EWS AND SECURITY [/b] 1. The BROWN WIDOW Utilizes a MILAC/APG-77 based ACTIVE ELECTRONICALLY SCANNED ARRAY (AESA) RADAR system. The RADAR system is controlled by via two TENSOR COMMON INTEGRATED PROCESSORS (CIP)s, which can process 10.5 billion instructions per second and have 800 MB of memory. This information is processed further by the on-board FCS XN78 computer system which provides the information in an easy to understand, informative display in the cockpit. The RADAR system has an expected range of approximately 300-350 km, with up to a 500 km range when utilizing a narrow beam search pattern. Additionally the aircraft has 6 EO/IR-sensors, and a Ultra-Violet MISSILE APPROACH EARLY WARNING SYSTEM (MAWS) both of which combine to be as a missile warning system with continuous coverage on all angles of the aircraft. The system is integrated with the FCS XN8 system and an AN/ASQ-239 (Barracuda) ELECTRONIC WARFARE SYSTEM (EWS). Additionally, the aircraft has seperate ECM and CECM pods smoothly integrated into the wing-tips for additional support of the NGPJ system. Internal electronics are protected by concentrated Electro-magnetic shielding to lessen the effects of concerted EM attacks. 2. In addition to the EWS used to protect the aircraft from electromagnetic attacks, an extensive on-board security suite is installed to avoid interference with the network via "hacking". All MILAC networks run on a SECURE ISOLATED NETWORK (SIN). The system utilizes FULL 1024 BIT ADVANCED ENCRYPTION STANDARD (AES) technology to encode all relevant information between parties, in conjunction with an indigenously developed Reduced Instruction Set driving hardware. In addition to these encryption technologies, all networks will operate in "stealth mode", acting as though the network didn't exist to any party outside of those programmed into the main system. No party can acquire /ROOT ACCESS to the software while the aircraft is operating, nor while the wireless network system is active. Data transmissions are monitored by MILAC personnel to observe that no erroneous information is being fed to the system by an errant enemy source. Furthermore, aircraft /ROOT ACCESS requires a high level manual password validation that would allow the user more then simple "use" of the software and transmitting authorized data forms (passing and receiving information from various programs). If such authorization cannot be acquired within five tries, the system invokes an F-DISK and destroys the hard-drive, destroying all internal code and the ability of the unit to interact via networking. Access to this screen requires it's own separate pass code to avoid accidental or sabotage based attacks, this has an unlimited number of tries, but would be impossible to enter without a proper code (only valid for the hour of it's entry). 3. In the event that a system within the network is considered compromised, the system can be cut off manually from a central network from the inside given the proper authorization codes. The system will not take effect on aircraft however, until it has safely landed on the ground. The on-board electronics, such as the hard-drive, cannot be removed from the system without proper coded authorization (similar to the /ROOT authorization protection), such systems are in place to prevent the physical removal of critical pieces of hardware and subsequent analysis by an external separately built device. All of this works to create an extremely secure defense around the working network, to prevent unwanted access by enemy forces. 4. The GREY WIDOW is capable of communicating in a secure, zero-probability of intercept 'hunting pack' capability via point-to-point laser transmissions strobed onto an appropriately equipped allied unit. This transmission is useable when supreme electronic silence must be maintained, especially when two or more communicating vehicles are in close proximity (tight formation). [b]AIRCRAFT DESIGN AND LOW OBSERVABILITY CHARACTERISTICS [/b] 1. The XF-32 utilizes a LOW OBSERVABLE TECHNOLOGY throughout the design of the aircraft to minimize it's RADAR cross section, IR signature, visual image and sensor systems. VEHICLE SHAPE attributes reflect RADAR off the aircraft at large angles, reducing returns and an S-Shaped air intake reduces the returns from the turbo-fans, while a thin layer of conducting Indium-Tin-Oxide, reduces the RCS of the cockpit. The removal of the hybrid control/close-coupled canard system of the BROWN WIDOW reduces the radar cross section of the aircraft substantially. The tailless design of the WIDOW also contributes to an all aspect RCS. 2. IR emissions from the engine are reduced by avoiding a circular tailpipe, such as the slit tail-pipe design found on the F-23 Black WIDOW and F-22 Raptor. This engine design also finds it's way onto the GREY WIDOW, which helps to reduce the aircraft's vulnerability to IR detection stations and heat-seeking missiles. The advent of optical systems also requires further stealth characteristics, which is why aircraft coloring scheme is designed to prevent shadows and blend into it's environment ((OOC: via the same techniques used on the Bird of Prey demonstrator)). 3. For the sake of protecting our critical resources, Air Militant Command often recommends that one or even two GREY WIDOW ace pilots accompany every squadron, providing additional cover from an off-formation vector. Ever vigilant but not directly visible, these aircraft serve several purposes. They provide dedicated air-combat focused specialists on the field, and can act as "mini-AEWACS", and they also provide increased endurance on the battlefield in intense air-combat situations because of their larger fuel capacity and armaments. 4. The largest radar reflector on the frontal aspect of a fighter is the compressor turbine. In order to compensate for this source of detection, there is a perceived misalignment of the turbine in relation to air intakes. This prevents radar waves from directly reaching the compressor. The result is a very small frontal RCS due to the curvature of the airducts of the turbine. 5. Exhaust from the single power plant flows through a winding path within the airframe of the XF-32. Along this path, the troughs are lined with heat ablating materials which in turn feeds the heat into the main combustion cavity. The exhaust is shielded from infrared missile detection from below. 6. The majority of the GREY WIDOW's airframe is built with composite materials opposed to conventional metallics, and is designed to 'trap' incoming radar waves that penetrate the external skin, allowing for more energy to be absorbed and turned into much more manageable heat. This heat may be shunted by liquid cooling to the combustion chambers of the XF-32's powerplant, aiding in propulsion and reducing radar returns substantially. While this does not aid in the ease of production, it was determined that unless catastrophic damage has been incurred by an airframe, export clients would not necessarily need to deal with such concerns. Furthermore, 3D-Manufacturing technology would serve to consolidate all construction woes into a single, easier to manage package, allaying cost and intricacy concerns somewhat. 7. Low wing aspect ratio is used to optimize supercruise performance. The tailless aspect of the WIDOW lends itself not only to a reduced RCS, but also reduced mechanical complexity and greater agility due to inherent instability. Edited June 22, 2012 by Joel James Quote Link to comment Share on other sites More sharing options...
Joel James Posted February 16, 2012 Author Report Share Posted February 16, 2012 i AZ7 Protector 19:55 Yui Mk. I (2014) 19:55 Yui Mk. II (2020) 19:55 Yui Systems 19:55 Yui Crew: 3 (Commander, Driver, Gunner) 19:55 Yui Autoloader: AAZL795 Autoloader 19:55 Yui Computer: AvecNord AZK4 Advanced Electronics Management System 19:55 Yui Operating System: Linux Defender 6 'Freelancer' 19:55 Yui Communications: Thialfi II Advanced BattComm Network 19:55 Yui Dimensions 19:55 Yui Height: 2.5m 19:55 Yui Length: 7.90m 19:55 Yui Length (w/ gun): 9.5m 19:55 Yui Width: 4.05m 19:55 Yui Weight: 76.5 tonnes (+2.7 tonnes w/ slat armor additions) 19:55 Yui Propulsion 19:55 Yui Engine: AZE2462 Multi-Fuel LPG and Water Injection F-8 Hyperbar Diesel Engine [2200 HP] 19:55 Yui Engine Fuel Storage: 2500 Liter Insulated Fuel Storage Compartment 19:55 Yui APU: 2x AZE3025 Brushless DC Electric Engine, 1x AZE2258 Compact Gas Turbine 19:55 Yui APU Fuel Storage: 13x Lithium-Ion Battery (2014), 9x Lithium-Ion Manganese spinel cathode Battery (2016) 19:55 Yui Power/Weight: 29.93 hp/metric ton 19:55 Yui Transmission: Continuously Variable Transmission (Hydraulic Mechanical Transmission) 19:55 Yui Performance 19:55 Yui Suspension: Hydropneumatic Active Suspension 19:55 Yui Ground Clearance: 0.5m (Adjustable) 19:55 Yui Range: 725 to 815 km 19:55 Yui Max Onroad Speed: 84 kmph 19:56 Yui Max Reverse Onroad Speed: 84 kmph 19:56 Yui Max Offroad Speed: 65 kmph 19:56 Yui Max Reverse Offroad Speed: 65 kmph 19:56 Yui Fording Depth: 1.15 m [4.2 m w/ proper equipment] 19:56 Yui Protection 19:56 Yui Armor: Wyvelt-Orvald Advanced Composite Armor, RHA steel alloys, titanium ceramic composites, titanium alloy, depleted uranium, Draakskild/Weinik-Draakskild ERA/NERA, Slat Armor (optional) 19:56 Yui Anti-spall: Cenodyne Advanced Spall Liner 19:56 Yui Countermeasures: Invictus APS [Cato-3 Soft-kill Protection Suite; Langskild Hard-kill Protection Suite; Kobalt Hard-kill Protection Suite], AvecNord 'Ermit' CBRN Protection System 19:56 Yui Armament 19:56 Yui Main Armament: AZ1125 140 mm L50 LP ETC Smoothbore (2014), AZ1127 135mm L52 LP ETC EM-Rifled Smoothbore (2020) 19:56 Yui Right Coaxial Armament: AZ932 45 mm Autocannon 19:56 Yui Left Coaxial Armament: 7.62 mm pintle-mount machine gun 19:56 Yui Secondary Armaments: .50 caliber swing-mount heavy automated machinegun, 4x lateral mounted grenade launchers 19:56 Yui Tertiary Armaments (optional; pick one): Rear-mounted mortar launcher, Rear-mounted laser-guided MANPADS, Rear-mounted MSTAR, None 19:56 Yui Costs 19:56 Yui Unit Price: $17.4 million (2014), $20.7 million (2020) Quote Link to comment Share on other sites More sharing options...
Joel James Posted March 2, 2012 Author Report Share Posted March 2, 2012 BUMPITY BUMPITY BUMPITY Quote Link to comment Share on other sites More sharing options...
Joel James Posted March 12, 2012 Author Report Share Posted March 12, 2012 no one tops me on the list. Quote Link to comment Share on other sites More sharing options...
Recommended Posts
Join the conversation
You can post now and register later. If you have an account, sign in now to post with your account.