East Harlack
14-03-2005, 19:55
Here is a list of weapons and systems commonly fielded by nations in Greater Harlack. This is to give everyone in the "Call for international peacekeepers" thread an idea of exactly what sort of armies are fielded by each nation...of course, this is the *declassified* material. All aircraft information is taken from www.fighter-planes.com, go there to look up some of the more specific information on the aircraft.
West Harlack:
Air Craft:
Vulcan, Avro
Large, delta-wing jet bomber. Its service life was reduced when its role was changed from high-altitude to low-altitude bombing, but it can be considered the most successful of the V-bombers. According to the fans, it was also the most beautiful one. Its saw operational use in the Falklands war, when Vulcan bombers attacked the local airfield at Port Stanly after a long flight during which they were refuelled several times by Victor tankers. There was also a reconnaissance version.
Type: Vulcan B Mk.2
Function: bomber
Year: 1960
Crew: 5
Engines: 4 * 9980 kg Bristol Siddeley Olympus 301
Wing Span: 33.83 m
Length: 32.15 m
Height:
Empty Weight:
Max.Weight: 113400 kg
Speed: 1030 km/h
Ceiling: 19800 m
Range: 7650 km
Armament: 21454 kg
The B-70 was a high-flying Mach 3 bomber, intended to replace the B-52. It was a canarded delta wing aircraft, designed to 'ride' on the shock wave contained between the lower fuselage and its movable, downturned wingtips. Because of kinetic heating at high speed, the B-70 was built from titanium and steel honeycomb parts. The advent of surface-to-aircraft missiles made the high-flying bomber obsolete. Two were built, as two-seat research aircraft.
Type: XB-70
Year: 1964
Crew: 4 (pilot, copilot, bombardier, and defensive systems operator)
Engines: 6 * 13075 kg G.E. YJ93-GE-3
Wing Span: 32.00 m
Length: 59.75 m
Height: 9.22 m
Wing Area: 585.43 m2
Empty Weight: 92990 kg
Max.Weight: 249470 kg
Speed: 3200 km/h
Ceiling: 22860 m
Range: 9650 km
Unit (prototype) cost: $700 millions
Armament: No defensive weapons except ECM. Internal bay for up to 14 nuclear or thermonuclear bombs, or an assortment of conventional bombs. Externally carried stand-off missiles were also considered
The U-2, a high-flying reconaissance aircraft, was camouflaged by this inoccent 'utility' designation. Ironically, it has become the most famous U-designated aircraft... The extremely high-flying U-2 spyplane became infamous in 1960 by being shot down over the Soviet Union. After that, the U-2 was claimed to be restricted to meteorological and environment control flights, but it continued to spy above countries other than the USSR, such as China and Cuba. Some were shot down. The WU-2 was used for sampling of the stratosphere, and examining the fall-out from nuclear tests. Later versions had a J75 engine. The U-2R is a much-modified version with two large pods on the wing, built in the second and third production runs --- the aircraft of the third series were named TR-1 for some time. The latest U-2R models were still present during the 1991 Gulf War. Reengining with the lighter and more powerful G.E. F118-GE-F29 engine is under way.
Type: U-2B
Task: reconaissance
Year: 1956
Crew: 1
Engines: 1 * 7710kg P&W J57-P-13B
Max. Speed: 850km/h
Ceiling: 27400m
Max. Range: 6640km
Type: A-7B
Year: 1968
Crew: 1
Wing Span: 11.81 m
Length: 14.05 m
Height: 4.87 m
Engines: 1 * 54.8 kN P&W TF30-P-8
Empty Weight: 8165 kg
Max.Weight: 19050 kg
Speed: Mach 0.8
Ceiling 12800 m
Range: 4540 km
Armament: 2*g 20 mm, 2*msl AIM-9, 9072 kg
Unit cost: 15 million USD
The four-engined B-17 was designed as a heavily-armed, long-range medium bomber. It became the mainstay of the USAF bomber offensive over Europe. The B-17 had a long range, and was easy to fly except when -- as was often the case -- it was overloaded; but its bomb-carrying capacity on long range was very limited. Even the 13 machine guns of the B-17G were not enough to fight off enemy fighters, but on the other hand the B-17 could have a lot of hits and still bring its crew home. Some B-17 Flying Fortress bombers were stripped of armament and used as CB-17 transports. 12731 built.
Type: B-17G
Function: bomber
Year: 1943
Crew: 10
Engines: 4 * 880 kW Wright R-1820-97
Wing Span: 31.62 m
Length: 22.66 m
Height: 5.82 m
Wing Area: 131.92 m2
Empty Weight: 16391 kg
Max.Weight: 29710 kg
Speed: 462 km/h
Ceiling: 10850 m
Range: 5080 km
Armament: 13 * mg12.7 mm, 9453 kg payload
South Harlack:
The SR-71 is a famous Mach 3+ spy plane. This is the fastest aircraft ever known to be in service with an air force. The large, delta-winged SR-71 gets is performance from the unusual J-58 engines, that act at as ramjets at high altitude and speed. It was related to the the YF-12 fighter and its precessor, the A-12 CIA-operated spy aircraft. Recently, the a number of SR-71s was put back in service from a premature retirement
Type: MiG-25
Function: fighter
Year: 1978
Crew: 1
Engines: 2 * 12250kg Tumansky R-31
Wing Span: 13.95 m
Length: 23.82 m
Height: 6.10 m
Wing Area: 56.83m2
Empty Weight: 20000 kg
Max.Weight: 36200 kg
Speed: 3000+ km/h
Ceiling: 24400 m
Range: 1730km
Type: MiG-25PD Foxbat-E
Function: fighter
Year: 1978
Crew: 1
Engines: 2 * 11200kg Tumansky R-15D-300
Wing Span: 14.02 m
Length: 21.67 m
Height: 6.50 m
Max.Weight: 36720kg
Speed: 3000km/h at 13000m, 1200km/h at S/L
Ceiling: 20700m Range: 1730km
Armament: 4 missiles
Type: MiG-25RB Foxbat-B
Function: reconaissance / attack
Year: 1970
Crew: 1
Engines: 2 * 10210 kg Tumansky R-15B-300
Wing Span: 13.42 m
Length: 21.55 m
Height: 6.5 m
Empty Weight: 20755
Max.Weight: 41200 kg
Speed: 3000 km/h at 13000 m
Ceiling: 23000 m
Range: 2900 km
Armament: bombs 4000 kg
Type: F-5A
Function: fighter
Year: 1963
Crew: 1
Engines: 2 * 1800 kg G.E. J85-GE-13
Wing Area: 15.79 m2
Wing Span: 7.70 m
Length: 14.38 m
Height: 4.01 m
Empty Weight: 3667 kg
Max.Weight:
Max. Speed: 1490 km/h
Range: 2600 km
Ceiling: 15200 m
Armament: 2*g20mm
Unit cost: 5 million USD
Northrop F-5E Tiger II
Type: F-5E
Function: fighter
Year: 1973
Crew: 1
Engines: 2 * 22.24 kN G.E. J85-GE-21A
Wing Span: 8.13 m
Length: 14.68 m
Height: 4.08 m
Wing Area: 17.28 m2
Empty Weight: 4410 kg
Max. Weight:
Max. Speed: Mach 1.64
Ceiling: 15790 m
Max. Range: 2860 km
Armament: 2*g20mm
Type: A-10A
Function: attack
Year: 1976
Crew: 1
Engines: 2 * 40.3kN G.E. TF34-GE-100
Wing Span: 17.53 m
Length: 16.26 m
Height: 4.47 m
Wing Area: 47.01 m2
Empty Weight: 11321 kg
Speed: 805 km/h
Range: 4200 km
Max.Weight: 22680 kg
Armament: 1*g30 mm, 7260 kg
Unit cost: 20 million USD
Type: Me 262A-1a
Function: fighter
Year: 1944 Crew: 1
Engines: 2 * 900kg Junkers Jumo 004B-1
Wing Span: 12.48 m
Length: 10.60 m
Height: 3.84 m
Wing Area: 21.70 m2
Empty Weight: 3800 kg
Max.Weight: 6400 kg
Speed: 870 km/h
Ceiling: 11450 m
Range: 1050 km
Armament: 4*g30 mm
Type: F-86A
Function: fighter
Year: 1948
Engines: 1 * 23.13kN G.E. J47-GE-13
Wing Area: 26.75m2
Empty Weight: 4780 kg
Max.Weight: 7359 kg
Armament: 6*mg12.7mm 2*b454kg
Type: F-86D
Function: fighter
Year: 1953
Engines: 1 * 3026kg G.E. J47-GE-17
Wing Area: 26.75m2
Empty Weight: 6123 kg
Type: F-86F (with "6/3" wing)
Function: fighter
Year: 1952
Engines: 1 * 26.40kN G.E. J47-GE-27
Wing Area: 29.11m2
Empty Weight: 5046 kg
Max.Weight: 6894 kg
Armament: 6*mg12.7mm 2*b454kg
East Harlack:
Type: B-52H
Function: bomber
Year: 1955
Crew: 6
Engines: 8 * 75.6 kN P&W TF-33-P-3
Wing Span: 56.39 m
Length: 49.05 m
Height: 12.40 m
Wing Area: 371.60 m2
Max.Weight: +221353 kg
Speed: 957 km/h
Ceiling: 16765 m
Range: 16093 km
Armament: up to 58 500-lb or 42 750-lb bombs in weapons bay and 12 750-lb bombs at each of the two underwing pylons. Or conventional or nuclear free-falling stores internally and two AGM-28A or -28B Hound Dog missiles (B-52 G & H). Four ½ inch guns in MD-9 tail turret, or one 20-mm ASG-21 rotary canon (B-52H)
Type: F-104A
Function: fighter
Year: 1958
Crew: 1
Engines: 1 * 65.78 kN P&W J79-GE-3B
Wing Span: 6.68 m
Length: 16.69 m
Height: 4.11 m
Wing Area: 18.21 m2
Empty Weight: 6071 kg
Max.Weight: 11721 kg
Speed: Mach 2.2
Ceiling: 19750 m
Range: 2250 km
Armament: 1*g 20 mm
Unit cost: 1,471,000 USD
Type: F-104G
Function: fighter
Year: 1960
Crew: 1
Engines: 1 * 7170kg G.E. J79-GE-11A
Wing Span: 6.36 m
Length: 16.66 m
Height: 4.09 m
Wing Area: 18.22 m2
Empty Weight: 6348 kg
Max.Weight: 13170 kg
Speed: Mach 2.2
Ceiling: 15240 m
Range: 3500 km
Armament: 1*g 20 mm
Type: F-20
Function: fighter
Year: 1982
Crew: 1
Engines: 1 * 7711 kg G.E. F404-GE-100
Wing Span: 8.13 m
Length: 14.17 m
Height: 4.22 m
Wing Area: 17.28 m2
Empty Weight: 5089 kg
Max.Weight: 12475 kg
Max. Speed: 2124 km/h
Ceiling:
Max. Range: 2965 km
Armament: 2*g 20 mm 3175 kg
Federated Harlack:
Type: F-117A
Function: attack
Year: 1982
Crew: 1
Engines: 2 * 48kN G.E. F404-GE-F102
Wing Span: 13.20 m
Length: 20.08 m
Height: 3.80 m
Wing Area: 105.9 m2
Empty Weight: 13609 kg
Max.Weight: 23814 kg
Max. Speed: 700 mph
Armament: 5000 lb
Unit cost: 120 million USD
Type: B-1B
Function: bomber
Year: 1986
Crew: 4
Engines: 4 * 13600 kg G.E. F101-GE-11
Wing Span: 41.67 m/23.84 m
Length: 44.81 m
Height: 10.36 m
Wing Area: 181.16 m2
Max.Weight: 216364 kg
Speed: 1375 km/h
Ceiling: 14600 m
Range: 12000 km
Armament: 29030 kgs
Unit cost: 200 million USD
Type: Rafale C
Country: France
Export: N/A
Function: Multi-role fighter
Year: (1997)
Crew: 1
Engines: 2 * 77 kN SNECMA M88-2
Wing Span: 10.90 m
Length: 15.30 m
Height: 5.34 m
Wing Area: 46.0 m2
Wing Aspect Ratio: 2.6
Canard Area: Unknown
Tail Plane Area: N/A
Empty Weight: 9060 kg
Max.Weight: 19500 kg
Internal Fuel: 4000 kg
Speed: Mach 2.0
Ceiling: 18290 m
Ferry Range: 3125 km
Combat Radius: 925 km
G-limits: 9/-3.2
Maximum instantenous turn rate: 30 degrees/second
Maximum sustained turn rate: Unknown
Rollrate: 270 degrees/sec
TWR(50% fuel, 2 EM A2A missile, 2 IR A2A missile): 1.3:1
TWR(100% fuel, 2 EM A2A missile, 2 IR A2A missile): 1.10:1
Armament: One internal 30 mm Giat DEFA 791B cannon. Normal external load up to 6000 kg (13,230lb) on 6 underwing, 2 wingtip, 2 centerline, and 4 underfuselage stations. Options include an ASMP nuclear standoff missile, up to 8 Matra Mica AAMs, AM 39 Exocets, LGBs, AS 30L LGASMs, or Apache dispensers with antiarmour or anti runway munitions.
Unit cost: 50 million USD
Prime contractor: Saab Military Aircraft
Nation of origin: Sweden
Function: Multi-role fighter, attack, and recon
Crew: 1
Year: 1988
In-service year: 1997
Engine: One General Electric/Volvo Flygmotor RM12 afterburning turbofan, 18,100 lb thrust
Dimensions
Wing span: 8.4 m / 27 ft 7 in
Length: 14.1 m / 46 ft 3 in
Height: 4.5 m / 14 ft 9 in
Weight: 14,600 lb empty / 27,560 lb max. take off
Ceiling: 50,000 ft
Speed: 2,126 km/h / 1,321 mph
Armament: One Mauser BK27 27mm cannon, plus up to 14,330 lb including Rb74/AIM-120 AAMs, Rb15F/Rb75 ASMs,
free-fall bombs, rockets, DWS 39 submunition dispensor weapons, recce/sensor pods, and fuel tanks on eight external points
Type: MiG-31
Function: fighter
Year: 1983
Crew: 2
Engines: 2 * 15500kg Perm D-30F6
Wing Span: 13.40 m
Length: 22.6 m
Height: 6.1 m
Wing Area: 61.6 m2
Empty Weight: 21825 kg
Max.Weight: 46200 kg
Speed: 3000 km/h
Ceiling: 20600 m
Range: 3000km
Armament: 1*g30 mm
Naval and Ground forces to come later.
West Harlack:
Air Craft:
Vulcan, Avro
Large, delta-wing jet bomber. Its service life was reduced when its role was changed from high-altitude to low-altitude bombing, but it can be considered the most successful of the V-bombers. According to the fans, it was also the most beautiful one. Its saw operational use in the Falklands war, when Vulcan bombers attacked the local airfield at Port Stanly after a long flight during which they were refuelled several times by Victor tankers. There was also a reconnaissance version.
Type: Vulcan B Mk.2
Function: bomber
Year: 1960
Crew: 5
Engines: 4 * 9980 kg Bristol Siddeley Olympus 301
Wing Span: 33.83 m
Length: 32.15 m
Height:
Empty Weight:
Max.Weight: 113400 kg
Speed: 1030 km/h
Ceiling: 19800 m
Range: 7650 km
Armament: 21454 kg
The B-70 was a high-flying Mach 3 bomber, intended to replace the B-52. It was a canarded delta wing aircraft, designed to 'ride' on the shock wave contained between the lower fuselage and its movable, downturned wingtips. Because of kinetic heating at high speed, the B-70 was built from titanium and steel honeycomb parts. The advent of surface-to-aircraft missiles made the high-flying bomber obsolete. Two were built, as two-seat research aircraft.
Type: XB-70
Year: 1964
Crew: 4 (pilot, copilot, bombardier, and defensive systems operator)
Engines: 6 * 13075 kg G.E. YJ93-GE-3
Wing Span: 32.00 m
Length: 59.75 m
Height: 9.22 m
Wing Area: 585.43 m2
Empty Weight: 92990 kg
Max.Weight: 249470 kg
Speed: 3200 km/h
Ceiling: 22860 m
Range: 9650 km
Unit (prototype) cost: $700 millions
Armament: No defensive weapons except ECM. Internal bay for up to 14 nuclear or thermonuclear bombs, or an assortment of conventional bombs. Externally carried stand-off missiles were also considered
The U-2, a high-flying reconaissance aircraft, was camouflaged by this inoccent 'utility' designation. Ironically, it has become the most famous U-designated aircraft... The extremely high-flying U-2 spyplane became infamous in 1960 by being shot down over the Soviet Union. After that, the U-2 was claimed to be restricted to meteorological and environment control flights, but it continued to spy above countries other than the USSR, such as China and Cuba. Some were shot down. The WU-2 was used for sampling of the stratosphere, and examining the fall-out from nuclear tests. Later versions had a J75 engine. The U-2R is a much-modified version with two large pods on the wing, built in the second and third production runs --- the aircraft of the third series were named TR-1 for some time. The latest U-2R models were still present during the 1991 Gulf War. Reengining with the lighter and more powerful G.E. F118-GE-F29 engine is under way.
Type: U-2B
Task: reconaissance
Year: 1956
Crew: 1
Engines: 1 * 7710kg P&W J57-P-13B
Max. Speed: 850km/h
Ceiling: 27400m
Max. Range: 6640km
Type: A-7B
Year: 1968
Crew: 1
Wing Span: 11.81 m
Length: 14.05 m
Height: 4.87 m
Engines: 1 * 54.8 kN P&W TF30-P-8
Empty Weight: 8165 kg
Max.Weight: 19050 kg
Speed: Mach 0.8
Ceiling 12800 m
Range: 4540 km
Armament: 2*g 20 mm, 2*msl AIM-9, 9072 kg
Unit cost: 15 million USD
The four-engined B-17 was designed as a heavily-armed, long-range medium bomber. It became the mainstay of the USAF bomber offensive over Europe. The B-17 had a long range, and was easy to fly except when -- as was often the case -- it was overloaded; but its bomb-carrying capacity on long range was very limited. Even the 13 machine guns of the B-17G were not enough to fight off enemy fighters, but on the other hand the B-17 could have a lot of hits and still bring its crew home. Some B-17 Flying Fortress bombers were stripped of armament and used as CB-17 transports. 12731 built.
Type: B-17G
Function: bomber
Year: 1943
Crew: 10
Engines: 4 * 880 kW Wright R-1820-97
Wing Span: 31.62 m
Length: 22.66 m
Height: 5.82 m
Wing Area: 131.92 m2
Empty Weight: 16391 kg
Max.Weight: 29710 kg
Speed: 462 km/h
Ceiling: 10850 m
Range: 5080 km
Armament: 13 * mg12.7 mm, 9453 kg payload
South Harlack:
The SR-71 is a famous Mach 3+ spy plane. This is the fastest aircraft ever known to be in service with an air force. The large, delta-winged SR-71 gets is performance from the unusual J-58 engines, that act at as ramjets at high altitude and speed. It was related to the the YF-12 fighter and its precessor, the A-12 CIA-operated spy aircraft. Recently, the a number of SR-71s was put back in service from a premature retirement
Type: MiG-25
Function: fighter
Year: 1978
Crew: 1
Engines: 2 * 12250kg Tumansky R-31
Wing Span: 13.95 m
Length: 23.82 m
Height: 6.10 m
Wing Area: 56.83m2
Empty Weight: 20000 kg
Max.Weight: 36200 kg
Speed: 3000+ km/h
Ceiling: 24400 m
Range: 1730km
Type: MiG-25PD Foxbat-E
Function: fighter
Year: 1978
Crew: 1
Engines: 2 * 11200kg Tumansky R-15D-300
Wing Span: 14.02 m
Length: 21.67 m
Height: 6.50 m
Max.Weight: 36720kg
Speed: 3000km/h at 13000m, 1200km/h at S/L
Ceiling: 20700m Range: 1730km
Armament: 4 missiles
Type: MiG-25RB Foxbat-B
Function: reconaissance / attack
Year: 1970
Crew: 1
Engines: 2 * 10210 kg Tumansky R-15B-300
Wing Span: 13.42 m
Length: 21.55 m
Height: 6.5 m
Empty Weight: 20755
Max.Weight: 41200 kg
Speed: 3000 km/h at 13000 m
Ceiling: 23000 m
Range: 2900 km
Armament: bombs 4000 kg
Type: F-5A
Function: fighter
Year: 1963
Crew: 1
Engines: 2 * 1800 kg G.E. J85-GE-13
Wing Area: 15.79 m2
Wing Span: 7.70 m
Length: 14.38 m
Height: 4.01 m
Empty Weight: 3667 kg
Max.Weight:
Max. Speed: 1490 km/h
Range: 2600 km
Ceiling: 15200 m
Armament: 2*g20mm
Unit cost: 5 million USD
Northrop F-5E Tiger II
Type: F-5E
Function: fighter
Year: 1973
Crew: 1
Engines: 2 * 22.24 kN G.E. J85-GE-21A
Wing Span: 8.13 m
Length: 14.68 m
Height: 4.08 m
Wing Area: 17.28 m2
Empty Weight: 4410 kg
Max. Weight:
Max. Speed: Mach 1.64
Ceiling: 15790 m
Max. Range: 2860 km
Armament: 2*g20mm
Type: A-10A
Function: attack
Year: 1976
Crew: 1
Engines: 2 * 40.3kN G.E. TF34-GE-100
Wing Span: 17.53 m
Length: 16.26 m
Height: 4.47 m
Wing Area: 47.01 m2
Empty Weight: 11321 kg
Speed: 805 km/h
Range: 4200 km
Max.Weight: 22680 kg
Armament: 1*g30 mm, 7260 kg
Unit cost: 20 million USD
Type: Me 262A-1a
Function: fighter
Year: 1944 Crew: 1
Engines: 2 * 900kg Junkers Jumo 004B-1
Wing Span: 12.48 m
Length: 10.60 m
Height: 3.84 m
Wing Area: 21.70 m2
Empty Weight: 3800 kg
Max.Weight: 6400 kg
Speed: 870 km/h
Ceiling: 11450 m
Range: 1050 km
Armament: 4*g30 mm
Type: F-86A
Function: fighter
Year: 1948
Engines: 1 * 23.13kN G.E. J47-GE-13
Wing Area: 26.75m2
Empty Weight: 4780 kg
Max.Weight: 7359 kg
Armament: 6*mg12.7mm 2*b454kg
Type: F-86D
Function: fighter
Year: 1953
Engines: 1 * 3026kg G.E. J47-GE-17
Wing Area: 26.75m2
Empty Weight: 6123 kg
Type: F-86F (with "6/3" wing)
Function: fighter
Year: 1952
Engines: 1 * 26.40kN G.E. J47-GE-27
Wing Area: 29.11m2
Empty Weight: 5046 kg
Max.Weight: 6894 kg
Armament: 6*mg12.7mm 2*b454kg
East Harlack:
Type: B-52H
Function: bomber
Year: 1955
Crew: 6
Engines: 8 * 75.6 kN P&W TF-33-P-3
Wing Span: 56.39 m
Length: 49.05 m
Height: 12.40 m
Wing Area: 371.60 m2
Max.Weight: +221353 kg
Speed: 957 km/h
Ceiling: 16765 m
Range: 16093 km
Armament: up to 58 500-lb or 42 750-lb bombs in weapons bay and 12 750-lb bombs at each of the two underwing pylons. Or conventional or nuclear free-falling stores internally and two AGM-28A or -28B Hound Dog missiles (B-52 G & H). Four ½ inch guns in MD-9 tail turret, or one 20-mm ASG-21 rotary canon (B-52H)
Type: F-104A
Function: fighter
Year: 1958
Crew: 1
Engines: 1 * 65.78 kN P&W J79-GE-3B
Wing Span: 6.68 m
Length: 16.69 m
Height: 4.11 m
Wing Area: 18.21 m2
Empty Weight: 6071 kg
Max.Weight: 11721 kg
Speed: Mach 2.2
Ceiling: 19750 m
Range: 2250 km
Armament: 1*g 20 mm
Unit cost: 1,471,000 USD
Type: F-104G
Function: fighter
Year: 1960
Crew: 1
Engines: 1 * 7170kg G.E. J79-GE-11A
Wing Span: 6.36 m
Length: 16.66 m
Height: 4.09 m
Wing Area: 18.22 m2
Empty Weight: 6348 kg
Max.Weight: 13170 kg
Speed: Mach 2.2
Ceiling: 15240 m
Range: 3500 km
Armament: 1*g 20 mm
Type: F-20
Function: fighter
Year: 1982
Crew: 1
Engines: 1 * 7711 kg G.E. F404-GE-100
Wing Span: 8.13 m
Length: 14.17 m
Height: 4.22 m
Wing Area: 17.28 m2
Empty Weight: 5089 kg
Max.Weight: 12475 kg
Max. Speed: 2124 km/h
Ceiling:
Max. Range: 2965 km
Armament: 2*g 20 mm 3175 kg
Federated Harlack:
Type: F-117A
Function: attack
Year: 1982
Crew: 1
Engines: 2 * 48kN G.E. F404-GE-F102
Wing Span: 13.20 m
Length: 20.08 m
Height: 3.80 m
Wing Area: 105.9 m2
Empty Weight: 13609 kg
Max.Weight: 23814 kg
Max. Speed: 700 mph
Armament: 5000 lb
Unit cost: 120 million USD
Type: B-1B
Function: bomber
Year: 1986
Crew: 4
Engines: 4 * 13600 kg G.E. F101-GE-11
Wing Span: 41.67 m/23.84 m
Length: 44.81 m
Height: 10.36 m
Wing Area: 181.16 m2
Max.Weight: 216364 kg
Speed: 1375 km/h
Ceiling: 14600 m
Range: 12000 km
Armament: 29030 kgs
Unit cost: 200 million USD
Type: Rafale C
Country: France
Export: N/A
Function: Multi-role fighter
Year: (1997)
Crew: 1
Engines: 2 * 77 kN SNECMA M88-2
Wing Span: 10.90 m
Length: 15.30 m
Height: 5.34 m
Wing Area: 46.0 m2
Wing Aspect Ratio: 2.6
Canard Area: Unknown
Tail Plane Area: N/A
Empty Weight: 9060 kg
Max.Weight: 19500 kg
Internal Fuel: 4000 kg
Speed: Mach 2.0
Ceiling: 18290 m
Ferry Range: 3125 km
Combat Radius: 925 km
G-limits: 9/-3.2
Maximum instantenous turn rate: 30 degrees/second
Maximum sustained turn rate: Unknown
Rollrate: 270 degrees/sec
TWR(50% fuel, 2 EM A2A missile, 2 IR A2A missile): 1.3:1
TWR(100% fuel, 2 EM A2A missile, 2 IR A2A missile): 1.10:1
Armament: One internal 30 mm Giat DEFA 791B cannon. Normal external load up to 6000 kg (13,230lb) on 6 underwing, 2 wingtip, 2 centerline, and 4 underfuselage stations. Options include an ASMP nuclear standoff missile, up to 8 Matra Mica AAMs, AM 39 Exocets, LGBs, AS 30L LGASMs, or Apache dispensers with antiarmour or anti runway munitions.
Unit cost: 50 million USD
Prime contractor: Saab Military Aircraft
Nation of origin: Sweden
Function: Multi-role fighter, attack, and recon
Crew: 1
Year: 1988
In-service year: 1997
Engine: One General Electric/Volvo Flygmotor RM12 afterburning turbofan, 18,100 lb thrust
Dimensions
Wing span: 8.4 m / 27 ft 7 in
Length: 14.1 m / 46 ft 3 in
Height: 4.5 m / 14 ft 9 in
Weight: 14,600 lb empty / 27,560 lb max. take off
Ceiling: 50,000 ft
Speed: 2,126 km/h / 1,321 mph
Armament: One Mauser BK27 27mm cannon, plus up to 14,330 lb including Rb74/AIM-120 AAMs, Rb15F/Rb75 ASMs,
free-fall bombs, rockets, DWS 39 submunition dispensor weapons, recce/sensor pods, and fuel tanks on eight external points
Type: MiG-31
Function: fighter
Year: 1983
Crew: 2
Engines: 2 * 15500kg Perm D-30F6
Wing Span: 13.40 m
Length: 22.6 m
Height: 6.1 m
Wing Area: 61.6 m2
Empty Weight: 21825 kg
Max.Weight: 46200 kg
Speed: 3000 km/h
Ceiling: 20600 m
Range: 3000km
Armament: 1*g30 mm
Naval and Ground forces to come later.