Aircraft > Fighterjets

Jet Fighters

Translated by BabelFish



Dassault Rafale - Eurofighter - F-117A Night Hawk - F-16C Fighting Falcon -
F/A-18E Hornet - Grumman F-14D Tomcat - Harrier Gr.Mk 7 - Lockheed / Boeing F-22A -
McDonnell Douglas F-15C Eagle - MiG-21 'Fishbed' - MiG-29M 'Fulcrum' - Mirage 2000N -
Sukhoi Su-27 'Flanker-B' - Sukhoi Su-35 'Flanker' - Tornado GR.Mk 1


~ Dassault Rafale ~


Dassault Rafale Voilure: Scale 10,90m with air-to-air missiles in end of wing; wing surface 46 m²
Fuselage and empennage: Length 15,30 m
Moteurs: Two Snecma M88-3 delivering each one 86,98 with afterburning
Poids: Maximum on takeoff 21500 kg
Carburant and charge: Fuel interns more than 5325 liters; external fuel up to 1700 liters, two releasable reserves of 2000 liters and/or two reserves of 1300 liters; maximum loading 6000 kg
Vitesse: Maximum speed on the level and "stringer" with 36090 FT (11000 m) 1147 KT (2125 km/h)
Rayon of action: Combat range 590 Nm (1093 km)en mission of penetration with low altitudeavec of the bombs of 12250 kg, four air-to-air missiles MICA and 4300 liters of fuel in three releasable tanks, or 1000 Nm (1853 km) on mission air-to-air with longua carried with 8 air-to-air missiles MICA and 6600 liters of fuel in four releasable tanks
Performances: Takeoff distance 1312 FT (400 m) to the weight of normal takeoff for a mission from air defense or 1969 FT (600 m) with the maximum weight of takeoff for a mission of attack
Acceleration limite: -3,6 with +9G
(Rafale)

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~ Eurofighter ~


Eurofighter Voilure: Scale 10,50m; lengthening of wing 2,205; wing surface 50 m²; surface duck 2,40 m²
Fuselage and empennage: Length 14,50 m; height approximately 4m
Moteurs: Two Eurojet EJ2000 delivering each one approximately 60 kN in dryness and 90 kN with afterburning
Poids: With vacuum 9750 kg; maximum on takeoff 21000 kg
Carburant and charge: Fuel interns 4000 kg; external fuel out of releasable tank being able to reach 1500 liters and two of 1000 liters; charge maximum 6500 kg
Vitesse: Maximum speed on the level and "stringer" with 36090 FT (11000 m) 1147 KT (2125 km/h)
Rayon of action: Combat range between 250 and 300 Nm (463 and 556 km)
Performances: Takeoff distance 1640 FT (500 m) to the standard weight of takeoff; Landing distance 1640 FT (500 m) to the standard weight of landing
Acceleration limite: -3 with +9G
(EF 2000)

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~ F-117A Night Hawk ~


F-117A Night Hawk Voilure: Scale 13,20 m; lengthening approximately 4,3; surface approximately 105,9 m²
Fuselage and empennage: Length 20,08 m; height 3,78
Moteurs: Two General Electric F404-GE-F1D2 to 58,04 kN each one
Poids: With vacuum 13608 kg; maximum on takeoff 23814 kg
Carburant and charge: Maximum armament 2268 kg
Vitesse: Maximum speed in smooth configuration and level at high altitude probably more Mach 1; speed of operation maximum at optimum altitude at Mach 0,9
Rayon of action: Autonomy in combat of 1112 km with maximum armament
Limite G: +6G
(F-117 NightHawk)

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~ F-16C Fighting Falcon ~


F-16C Fighting Falcon Voilure: Scale 9,45 m without the air-to-air missiles assembled in end of wing and 10 m with the air-to-air missiles; lengthening 3,09; wing surface 28,87 m²
Fuselage and empennage: Length 15,03 m; height 5,09 m; scale of the empennage 5,58 m; train sees 2,36 m; footing 4 m
Moteurs: A dual flow jet engine Pratt & Whitney F100-P-220 emitting 104,31 kN with afterburning or a dual flow jet engine General Electric F110-GE-100 emitting 122,77 kN with afterburning
Poids: With vacuum 8663 kg with the dual flow jet engine F110 or 8316 kg with F100; weight of takeoff of combat 9791 kg; weight of maximum takeoff 11372 kg for an air-to-air mission without releasable tanks or 19187 kg with maximum external load
Carburant and charge: Reserve of fuel interns 3162 kg; external fuel up to 3066 kg distributed in three releasable tanks of 1136, 1400, 1703 or 2271 liters; maximum warhead 6894 kg
Vitesse: Maximum level speed without carrying with 40000 FT (12190 m) more than 1146 KT (2124 km/h) and on the sea level 795 KT (1472 km/h)
Rayon of action: Convoying more than 2100 Nm (3891 km) with releasable tanks; combat range 295 Nm (547 km) at the time of a mission Ho-Ba-Ho equipped with six bombs with 454 kg
Performances: Maximum climbing speed on the sea level more than 50000 FT (15240 m) per minute; ceiling more than 50000 FT (15240 m); takeoff distance 762 m to the maximum design weight on takeoff; landing distance 762 m to the normal mass of landing
Acceleration limite: +9G
(F-16 Fighting Falcon)

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~ F/A-18E Hornet ~


F/A-18E Hornet Voilure: Scale 13,62 m; width folded up wing 9,32 m; lengthening 3,51; surface 46,45 m²
Fuselage and empennage: Length 18,31 m; height 4,82 m
Moteurs: Two dual flow jet engines General Electric F110-GE-400 delivering each one to 97,86 kN with afterburning
Poids: Vacuum 13880 kg; maximum on takeoff 29937 kg
Carburant and charge: Fuel interns 6531 kg; external fuel up to 4436 kg divided into three reserves of 1818 liters
Vitesse: Maximum speed more than 1033 KT (1915 km/h) on the level in smooth configuration at high altitude
Rayon of action: Autonomy of combat 591 Nm (1095 km) on mission Ho-Ho-Ho or 486 Nm (901 km) on mission Ho-Ba-Ho
Performances: Ceiling of use fights 15242 m of them
(F/A-18 Hornet)

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~ Grumman F-14D Tomcat ~


Grumman F-14D Tomcat Voilure: Scale 19,54 m completely deployed, 11,65 m in position of average arrow and 10,15 m in maximum position of arrow; lengthening 7,28; surface 52,49 m²
Fuselage and empennage: Length 19,10 m; height 4,88 m; scale empennage 9,97 m; train sees 5 m; footing 7,02 m
Moteurs: Two turbojets with double flow General Electric F110-GE-400 of a push of 62,27 kN in dryness and 102,75kN with afterburning
Poids: With vacuum 18951 kg; normal on takeoff for a mission of combat/escorte 29072 kg or for a mission of air defense 33157 kg; maximum on takeoff 33724 kg
Vitesse: Maximum speed on the level and "stringer" and at high altitude 1078 KT (1997 km/h); cruising speed at optimum altitude 413 KT (764 km/h)
Rayon of action: Maximum autonomy with inboard and external fuel tanks approximately 1600 Nm (2965 km); operating range of combat in air patrol of combat with 6 AIM-7 Sparrows and 4 AIM-9 Sidewinders 1075 Nm (1994 km)
Performances: Maximum climbing speed on the sea level of more than 30000 FT (9145 m) per minute; ceiling of use more than 53000 FT (16150 m); takeoff distance on terrestrial track 762 m with the maximum weight of takeoff; landing distance on terrestrial track 732 m.
(F-14 Tomcat)

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~ Harrier Gr.Mk 7 ~


Harrier Gr.Mk 7 Voilure: Scale 9,25 m; lengthening 22,18 m² including 0,81 m² for the two extensions of leading edge
Fuselage and empennage: Length 14,36 m; height 3,55 m; scale of the empennage 4,24 m; train with balancine sees 5,18 m
Moteurs: Rolls Royce Pegasus Mk 105 with a push of 96,75 kN dry
Poids: With vacuum 7050 kg including/understanding the pilot and carburizing it not used; weight of normal takeoff 10410 kg for short takeoff; Maximum weight of takeoff 14061 kg for short takeoff 8595 kg for vertical takeoff
Carburant and charge: Fuel interns 3519 kg; external fuel up to 3661 kg in four releasable reserves of 1136 liters; maximum warhead 4173 kg
Vitesse: Maximum level speed without carrying with 36090 FT (11000 m) 522 KT (967 km/h) and 575 KT (1065 km/h) on the sea level
Rayon of action: Convoying 2000 Nm (3891 km) with releasable of the empty tanks or 1750 Nm (3243 km) with empty tanks; combat range 90 Nm (167 km) after short takeoff and in a mission of attack Ba-Ba-Ba with one hour of overflight and a load of seven bombs of 227 kg, or 627 Nm (1162 km) at the time of a mission of interception Ho-Ho-Ho equipped with two air-to-air missiles AIM-9 Sidewinder and two releasable tanks, or 100 Nm (185 km) for a CAPE mission three hour old
Performances: Takeoff distance 405 m to the maximum weight of takeoff; landing distance 0 m to the weight of normal landing
Acceleration limite: -3 with +8G
(Harrier)

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~ Lockheed / Boeing F-22A ~


Lockheed / Boeing F-22A Voilure: Scale 13,56 m; Lengthening 2,36; Surface 78,04 m²
Fuselage and empennage: Length 18,92 m; height 5m
Moteurs: 2 Pratt & Whitney F119-P-100 delivering each one 155,69 kN with afterburning
Poids: With vacuum more than 13608 kg; maximum on takeoff 26308 kg
Vitesse: Maximum level speed ' in lisse' at optimal altitude Mach 1,58 as a supercroisière mode and with 30000 FT (9145 m) Mach 1,7 in afterburning mode
Performances: Ceiling of service 50000 FT (15240 m)
Acceleration limite: +7,9 G
(F-22 Raptor)

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~ McDonnell Douglas F-15C Eagle ~


McDonnell Douglas F-15C Eagle Voilure: Scale 13,05 m; report/ratio of lengthening 3,01; surface 56,48 m²
Fuselage and empennage: Length 19,43 m; height 5,63 m; scale of the empennage 8,61 m; distance between centres 2,75 m; footing 5,42 m
Moteurs: Two dual flow jet engines Pratt & Whitney F100-PW-220 each one to 65,26 kN (dry engines) and of 106,0 kN with afterburning
Poids: Vacuum 12793 kg; normal takeoff 20244 kg on a mission of interception with four air-to-air missiles AIM-7 Sparrow; maximum on takeoff 26521 kg with three releasable reserves of 2309 liters or 30844 kg with CFT
Carburant and charge: Fuel interns 6103 kg; external fuel up to 4423 kg in two CFT and 5395 kg in three releasable reserves of 2271 liters; maximum armament 7257 or 10755 kg respectively without or with CFT
Vitesse: Maximum level speed to 10975 m higher than 2655 km/h; cruising speed at optimal altitude 917 km/h
Rayon of action: Ferrying distance with releasable tanks higher than 4633 or 5745 km respectively without or with CFT; operating range in combat with mission of interception1967 km; autonomy 5h15 with CFT or 15 hours with in-flight refueling
Performances: Maximum climbing speed on the sea level higher than 15240 m per minute; ceiling practises 18290 m; absolute ceiling 30480 m;Distance of takeoff 274 m with weight of normal takeoff; landing distance 1067 m with weight of normal landing without parachute of tail
Limite G: -3 with +9G
(F-15 Eagle)

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~ MiG-21 'Fishbed' ~


MiG-21 'Fishbed' Voilure: Scale 7,154 m; lengthening 2,23; surface 23 m²
Fuselage and empennage: Length 15,76 m including the pole; height 4,125 m; train sees 2,787 m; footing 4,71 m
Moteurs: A turbojet MNPK ' Soyuz' (Tumanskii) R-25-300 delivering 97,12 kN with the top of Mach 1 at a maximum altitude of 13123 FT (4000 m) for periods going up to three minutes; two auxiliary rocket engines with powder SPRD-99 delivering 24,52 kN can be assembled
Poids: With vacuum 5450 kg; of normal takeoff 8725 kg; of maximum takeoff 9800 kg or 8800 kg on a difficult ground, or 10400 kg with wheels KT-92D and tires 058
Carburant and charge: Fuel interns 2880 liters; external fuel 1750 liters in three releasable tanks; charge maximum 2000 kg
Vitesse: Maximum speed on the level and "stringer" with 42650 FT (13000 m) 1177 KT (2175 km/h)
Rayon of action: 795 Nm (1470 km) with 32800 FT (10000 m) with a releasable reserve of 800 liters
Performances: Rate of rise on the sea level with two missiles and 50% of its fuel more than 45275 FT (13800 m) per minute; ceiling of service 57415 FT (13800 m); takeoff distance 1800 FT (830 m); landing distance 2720 FT (550 m) for a standard weight of landing with SPS and parachute brake
(MiG-21 Fishbed)

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~ MiG-29M 'Fulcrum' ~


MiG-29M 'Fulcrum' Voilure: Scale 11,36m; lengthening 3,4; wing surface 38 m²
Fuselage and empennage: Length 17,37 m with pole; height 4,73 m; scale of the drift 7,78 m; train sees 3,10 m; footing 3,67 m
Moteurs: Two dual flow jet engines Leningrad/Klimov (Isotov/Sarkisov) RD-33K delivering 53,95 kN "in dryness", 86,33 kN with afterburning, and an emergency mode delivering 92,22 kN
Poids: With vacuum 10900 kg; normal on takeoff 15240 kg; maximum on takeoff 18500 kg
Carburant and charge: Fuel interns 5000 kg (6250 liters); external fuel a central tank of 1500-1520 liters and (on certain Soviet apparatuses) two reserves of convoying under the wing of 1150 liters; maximum loading 4500 kg
Vitesse: Maximum speed on the level and "stringer" with 36090 FT (11000 m) 1319 KT (2445 km/h) or on the sea level 810 KT (1500 km/h)
Rayon of action: 1080 Nm (2000 km) with internal fuel; 1728 Nm (3200 km) with external tanks
Performances: Maximum rate of rise on the sea level 64961 FT (19800 m) per minute; ceiling of service 55775 FT (17000 m);Distance of takeoff 820 FT (250 m) to the standard weight of takeoff; Landing distance 1969 FT (600 m) to the standard weight of landing with brake chute
Acceleration limite: +9G under Mach 0,85 and +7G with the top of Mach 0,85
(MiG-29 Fulcrum)

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~ Mirage 2000N ~


Mirage 2000N Voilure: Scale 9,29 m; lengthening 2,03
Fuselage and empennage: Length 14,55 m; height 5,15 m; train sees 3,40 m; footing 5 m
Moteurs: A SNECMA M53-P2 of a push of 64,33 kN in dryness and 95,12 kN with afterburning
Poids: With vacuum approximately 7500 kg; weight of normal takeoff 10680 kg; Maximum weight of takeoff 17000 kg
Carburant and charge: Fuel capacity interns 3160 kg; external fuel capacity up to 3720 kg in a reserve of 1300 liters and two releasable reserves of 1700 liters; maximum warhead 16300 kg
Vitesse: Maximum level speed without carrying with 36090 FT (11000 m) 1262 KT (2338 km/h); speed of penetration with 197 FT (60 m) 600 KT (1112 km/h)
Rayon of action: Convoying 1800 Nm (3335 km) with releasable tanks; fights more than 800 Nm (1480 km) with four bombs of 250 kg, or more than 1000 Nm (1850 km) with two releasable tanks
Performances: Maximum climbing speed on the sea level 55971 FT (17060 m) per minute; ceiling 59055 FT (18000 m); rise with 49215 FT (15000 m) 4 minutes; time of interception of a target at Mach 3 to 80050 FT (24400 m) five minutes after takeoff; takeoff distance 1476 FT (450 m) to the weight of normal takeoff
Acceleration limite: +9G normal and +13,5G maximum
(Mirage 2000)

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~ Sukhoi Su-27 'Flanker-B' ~


Sukhoi Su-27 'Flanker-B' Voilure: Scale 14,70 m; lengthening 5,6; wing surface 45,50 m²
Fuselage and empennage: Length 21,90 m without the pole; height 5,90 m; scale of the empennage 9,90 m; train sees 4,33 m; footing 5,88 m
Moteurs: Two turbojets NPO Saturn (Lyul' ka) AL-31F delivering each one 79,43 kN dry and 122,58 kN with afterburning
Poids: With vacuum 17700 kg; weight of normal takeoff 23250 kg; maximum weight of takeoff 33000 kg
Carburant and charge: Fuel capacity interns normal 5270 kg; internal fuel capacity maximum 9400 kg; charge maximum 6000 kg
Vitesse: Limit Mach 2,35; maximum level speed with 36090 FT (11000 m) 1230 KT (2280 km/h) and on the sea level 739 KT (1370 km/h)
Rayon of action: At high altitude 1986NM (3680 km); at low altitude 739 Nm (1370 km)
Performances: Speed of rise maximum on the sea level 64960 FT (19800 m) per minute; ceiling 58071 FT (17700 m); Takeoff distance 450 m to the maximum weight of takeoff; landing distance 700 m to the weight of normal landing
Acceleration limite: +8G

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~ Sukhoi Su-35 'Flanker' ~


Sukhoi Su-35 'Flanker' Voilure: Scale 15,16 m on pods ESM; Lengthening 5,6; wing surface 46,50 m²
Fuselage and Empennage: Length 22,183 m; height 6,84; scale of the empennage 9,90 m; train sees 4,33 m; footing 5,88 m
Moteurs: 2 dual flow jet engines NPO Saturn (Lyul' ka) AL-31FM, delivering each one 130,42 kN with afterburning.
Poids: To vacuum, 18253,8 kg; standard weight on takeoff 26000 kg; maximum weight on takeoff 34000 kg.
Carburant and charge: maximum external load 8000 kg
Vitesse: Maximum level speed out of stringer with 36089 FT (11000 m) 2500 Km/h, and on the sea level 756 KT (1400 lm/h)
Rayon of action: At altitude raised with 4 air-to-air missiles 1889 Nm (3500 km); operating range at low altitude with 4 air-to-air missiles 783 Nm (1450 km); Convoying 2267 Nm (4200 Km); Operating range with in-flight refueling more than 3670 Nm (6800 km)
Performances: Maximum climbing speed on the sea level 64960 FT (19800 m) per minute; ceiling of use 58071 FT (17700m); takeoff distance 1476 FT (450 m) (with the weight of maximum takeoff); landing distance 2297 FT (700 m) to the standard weight of landing.
(Su-35 Flanker (Su-27M))

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~ Tornado GR.Mk 1 ~


Tornado GR.Mk 1 Voilure: Scale 13,91 m with sweptback wings at least (25°) and 8,60 m with sweptback wings to the maximum (67°); lengthening 7,73 with open wings and 2,96 with sweptback wings; wing surface 26,60 m²
Fuselage and empennage: Length 16,72 m; height 5,95 m; scale of the empennage 6,80 m; train sees 3,10 m; footing 6,20 m
Moteurs: Two turbojets Turbo-Union RB.199-34R Mk101 of a poussee of 37,70 kN in dryness each one and 66,01 kN with afterburning or, on the more recent planes, of the turbojets Turbo-Union RB.199-34R Mk103 of a poussee of 38,48 kN in dryness each one and 71,50 kN with afterburning
Poids: Basic with vacuum approximately 13890 kg; operationnel with vacuum 14091 kg; normal of takeoff 20411 kg; maximum of takeoff approximately 27951 kg
Carburant and charge: Fuel capacity interns 5090 kg; external fuel capacity up to 5988 kg distributed in two reserves of 2250 liters and two reserves of 1500 liters or four releasable reserves of 1500 liters; maximum warhead higher than 9000 kg
Vitesse: Limiting Mach: Mach 1,4 with LRMTS, M1,3 with decontaminated air intakes (all apparatuses of the RAF); speed indicated limit 800 KT (1482 km/h); maximum level speed without carrying with 36000 FT (10975 m) 1262 KT (2338 km/h)
Rayon of action: Convoying approximately 2100 Nm (3890 km) with quatres releasable tanks; 750 Nm (1390 km) at the time of a mission of standard attack fight Ho-Ba-Ho equipped with a heavy warhead
Performances: Rise with 30000 FT (9145 m) in less than 2 minutes after takeoff; ceiling of service 50000 FT (15240 m);Distance of takeoff lower than 900 m with the weight of maximum takeoff; landing distance 370 m to the maximum weight of landing
Acceleration limite: +7,5G
(Tornado)

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