Translated by BabelFish
Dassault Rafale
 Eurofighter
 F117A Night Hawk
 F16C Fighting Falcon

F/A18E Hornet
 Grumman F14D Tomcat
 Harrier Gr.Mk 7
 Lockheed / Boeing F22A

McDonnell Douglas F15C Eagle
 MiG21 'Fishbed'
 MiG29M 'Fulcrum'
 Mirage 2000N

Sukhoi Su27 'FlankerB'
 Sukhoi Su35 'Flanker'
 Tornado GR.Mk 1
~ Dassault Rafale ~
Voilure: Scale 10,90m with airtoair missiles in end of wing; wing surface 46 m²
Fuselage and empennage: Length 15,30 m
Moteurs: Two Snecma M883 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 airtoair missiles MICA and 4300 liters of fuel in three releasable tanks, or 1000 Nm (1853 km) on mission airtoair with longua carried with 8 airtoair 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)
~ 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)
~ F117A 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 F404GEF1D2 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
(F117 NightHawk)
~ F16C Fighting Falcon ~
Voilure: Scale 9,45 m without the airtoair missiles assembled in end of wing and 10 m with the airtoair 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 F100P220 emitting 104,31 kN with afterburning or a dual flow jet engine General Electric F110GE100 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 airtoair 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 HoBaHo 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
(F16 Fighting Falcon)
~ F/A18E 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 F110GE400 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 HoHoHo or 486 Nm (901 km) on mission HoBaHo
Performances: Ceiling of use fights 15242 m of them
(F/A18 Hornet)
~ Grumman F14D 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 F110GE400 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 AIM7 Sparrows and 4 AIM9 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.
(F14 Tomcat)
~ 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 BaBaBa 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 HoHoHo equipped with two airtoair missiles AIM9 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)
~ Lockheed / Boeing F22A ~
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 F119P100 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
(F22 Raptor)
~ McDonnell Douglas F15C 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 F100PW220 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 airtoair missiles AIM7 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 inflight 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
(F15 Eagle)
~ MiG21 '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) R25300 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 SPRD99 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 KT92D 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
(MiG21 Fishbed)
~ MiG29M '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) RD33K 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 15001520 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
(MiG29 Fulcrum)
~ 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 M53P2 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)
~ Sukhoi Su27 'FlankerB' ~
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) AL31F 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
~ Sukhoi Su35 '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) AL31FM, 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 airtoair missiles 1889 Nm (3500 km); operating range at low altitude with 4 airtoair missiles 783 Nm (1450 km); Convoying 2267 Nm (4200 Km); Operating range with inflight 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.
(Su35 Flanker (Su27M))
~ 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 TurboUnion RB.19934R 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 TurboUnion RB.19934R 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 HoBaHo 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)