ejemplos rfp usfaero.us.es/adesign/rfp/ejemplos/ejemplos rfp usf.pdf · 2008. 6. 1. · 01/06/2008...

01/06/2008 1Cálculo de Aviones © 2008 Sergio Esteban Roncero

Ejemplos de aeronaves existentes similares a las propuestas en los RFP 2007

Ultimate Supercruise Fighter(USF)

Sergio [email protected]

201/06/2008 Cálculo de Aviones © 2008 Sergio Esteban Roncero

F22 - RaptorGeneral characteristics

Crew: 1Length: 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 tipEmpty weight: 31,700 lb (14,379 kg)Loaded weight: 55,352 lb (25,107 kg)Max takeoff weight: 80,000 lb (36,288 kg)Powerplant: 2× Pratt & Whitney F119-PW-100 Pitch "Thrust" vectoring turbofans, 35,000+ lb (156+ kN) each

PerformanceMaximum speed: ≈Mach 2+[1] (1,325+ mph, 2,132+ km/h) ; >Mach 2.42 (Paul Metz)Cruise speed: Mach 1.72[52] (1,140 mph, 1,825 km/h) supercruise at altitudeFerry range: 2,000 mi (1,738 nmi, 3,219 km)Service ceiling: 65,000 ft (19,812 m)Wing loading: 66 lb/ft² (322 kg/m²)Thrust/weight: 1.26Maximum g-load: −3.5/+9.5 g

ArmamentGuns: 1× 20 mm (0.787 in) M61A2 Vulcan gatling gun in starboard wing root, 480 roundsAir to air loadout:

6× AIM-120 AMRAAM2× AIM-9 Sidewinder

Air to ground loadout:2× AIM-120 AMRAAM and2× AIM-9 Sidewinder and one of the following:

2× 1,000 lb JDAM or2× Wind Corrected Munitions Dispensers (WCMDs) or8× 250 lb GBU-39 Small Diameter Bombs

AvionicsRWR (Radar warning receiver): 250 nmi (463 km) or more[23]Radar: 125-150 miles (200-240 km) against 1 m² targets (estimated range)[21]

Bibliography Data from USAF [1] - "USAF Fact sheets: F-22A Raptor." United States Air Force. August 2007, Access date: 21 September 2007. F-22 Raptor Team web site,[52] "Flight Test Data." Access date: 18 April 2006. Aviation Week,[21] Klass, Philip J. "Sanders Will Give BAE Systems Dominant Role in Airborne EW." Aviation Week & Space TechnologyVolume 153, issue 5, 31 July 2000. p. 74. Journal of Electronic Defense[23] - Sweetman, Bill. "Fighter EW: The next generation." Journal of Electronic Defense, Volume 23, issue 7, July 2000. p. 41-47.


Eurofighter - TyphonGeneral characteristics

Crew: 1 or 2Length: 15.96 m (52 ft 5 in)Wingspan: 10.95 m (35 ft 11 in)Height: 5.28 m (17 ft 4 in)Wing area: 50 m² (540 ft²)Empty weight: 11,000 kg[55] (24,250 lb)Loaded weight: 15,550 kg (34,280 lb)Max takeoff weight: 23,000 kg[55] (51,809 lb)Powerplant: 2× Eurojet EJ200 afterburning turbofansDry thrust: 60 kN (13,500 lbf) eachThrust with afterburner: 90 kN (20,250 lbf) each

PerformanceMaximum speed:

At altitude: Mach 2[56][57]At sea level: Mach 1.2 (1,470 km/h, 915 mph)[citation needed]Supercruise: Mach 1.2[55] (1,470 km/h, 915 mph)

Range: 1390 km (864 mi)Ferry range: 3790 km (2,300 mi)Service ceiling: 19,812 m (65,000 ft[58])Rate of climb: >315 m/s[59] [60] [61][verification needed] (62,007 ft/min)Wing loading: 311 kg/m² (63.7 lb/ft²)Thrust/weight: 1.18

ArmamentGun: 1x 27 mm Mauser BK-27 cannonAir-to-Air missiles: AIM-9 Sidewinder, AIM-132 ASRAAM, AIM-120 AMRAAM, IRIS-T and in the future MBDA MeteorAir-to-Ground missiles: AGM-84 Harpoon, AGM-88 HARM, ALARMs, Storm Shadow (AKA "Scalp EG"), Brimstone, Taurus, Penguin and in the future AGM ArmigerBombs: Paveway 2, Paveway 3, Enhanced Paveway, JDAM, HOPE/HOSBOLaser designator, e.g. LITENING pod

Bibliography Data from USAF [1] - "USAF Fact sheets: F-22A Raptor." United States Air Force. August 2007, Access date: 21 September 2007. F-22 Raptor Team web site,[52] "Flight Test Data." Access date: 18 April 2006. Aviation Week,[21] Klass, Philip J. "Sanders Will Give BAE Systems Dominant Role in Airborne EW." Aviation Week & Space TechnologyVolume 153, issue 5, 31 July 2000. p. 74. Journal of Electronic Defense[23] - Sweetman, Bill. "Fighter EW: The next generation." Journal of Electronic Defense, Volume 23, issue 7, July 2000. p. 41-47.


JAS 39 Gripen

General characteristicsCrew: 1–2Length: 14.1 m (46 ft 3 in)Wingspan: 8.4 m (27 ft 7 in)Height: 4.5 m (14 ft 9 in)Wing area: 25.54 m (274.9 ft)Empty weight: 6,620 kg (14,600 lb)Loaded weight: 8,720 kg (19,200 lb)Max takeoff weight: 14,000 kg (31,000 lb)Powerplant: 1× Volvo Aero RM12 (GE F404) afterburning turbofan, 54 kN dry, 80 kN with afterburner (12,000 lbf / 18,100 lbf)Wheel track: 2.4 m (7 ft 10 in)

PerformanceMaximum speed: Mach 2Range: Combat radius 800 km, (500 mi), (430 NM). ()Service ceiling: 15,000 m (50,000 ft)Rate of climb: m/s (ft/min)Wing loading: 341 kg/m² (70,3 lb/ft²)Thrust/weight: 0.94

Armament1 × 27 mm Mauser BK-27 cannon6 × Rb 74 or Rb 984 × Rb 99, Rb 71, MICA or MeteorRb 75, KEPD 350, or various other laser-guided bombs, rocket pods.Rb 15F anti-ship missileBk 90 cluster bomb


F35 – Lightning II

General characteristics* Crew: 1* Length: 50 ft 6 in (15.37 m)* Wingspan: 35 ft 0 in (10.65 m)* Height: 17 ft 4 in (5.28 m)* Wing area: 459.6 ft² (42.7 m²)* Empty weight: 26,000 lb (12,000 kg)* Loaded weight: 44,400 lb (20,100 kg)* Max takeoff weight: 60,000 lb (27,200 kg)* Powerplant: 1× Pratt & Whitney F135 afterburning turbofan

o Dry thrust: 25,000 lbf[52] (111 kN)o Thrust with afterburner: >40,000 lbf[52] (178 kN)

* Secondary Powerplant: 1× General Electric/Rolls-Royce F136 afterburning turbofan, >40,000 lbf (178 kN) [in development]

* Lift fan (STOVL): 1× Rolls-Royce Lift System driven from either F135 or F136 power plant, 18,000 lbf (80 kN)Performance

* Maximum speed: Mach 1.6+ [52] (1,200 mph, 1,931 km/h)* Range: ≈1,200 nmi (1,400 mi, 2,200 km) on internal fuel* Combat radius: 600 nmi (690 mi, 1,110 km)* Rate of climb: classified (not publicly available)* Wing loading: 91.4 lb/ft² (446 kg/m²)* Thrust/weight:

o With full fuel: 0.968o With 50% fuel: 1.12(A); 1.10(B); 1.01(C) [52]


Dassault Mirage 2000

General characteristics* Crew: 1* Length: 14.36 m (50 ft 3 in)* Wingspan: 9.13 m (29 ft)* Height: 5.30 m (17 ft 5 in)* Wing area: 41 m² (441.32 ft²)* Empty weight: 7,600 kg (17,000 lb)* Loaded weight: 13,800 kg (30,420 lb)* Max takeoff weight: 17,000 kg (37,500 lb)* Powerplant: 1× SNECMA M53-P2 afterburning turbofan, 95 kN (21,400 lbf)

Performance* Maximum speed: (Mach 2.2) altitude* Range: 1,480 km (770 nmi, 890 mi)* Service ceiling: 18,000 m (59,000 ft)* Rate of climb: 285 m/s (56,000 ft/min)* Wing loading: 337 kg/m² (69 lb/ft²)* Thrust/weight: 0.70

Armament* Guns: 2× 30 mm (1.18 in) DEFA cannons* Missiles: 4× MBDA MICA air-to-air missiles


Sukhoi Su-27

General characteristicsCrew: OneLength: 21.9 m (72 ft)Wingspan: 14.7 m (48 ft 3 in)Leading edge sweep: 42°)Height: 5.93 m (19 ft 6 in)Wing area: 62 m² (667 ft²)Empty weight: 16,380 kg (36,100 lb)Loaded weight: 23,000 kg (50,690 lb)Max takeoff weight: 33,000 kg (62,400 lb)Powerplant: 2× Lyulka AL-31F turbofans, 122.8 kN (27,600 lbf) each

PerformanceMaximum speed: 2,500 km/h at altitude (1,550 mph Mach 2.35)Range: 1,340km combat mission at sea level 3,530 km combat mission at high altitude (800 mi at sea level / 2070 mi at high altitude)Service ceiling: 18,500 m (60,700 ft)Rate of climb: 325 m/s (64,000 ft/min)Wing loading: 371 kg/m² (76 lb/ft&sup2')Thrust/weight: 1.085

Armament1x 30 mm GSh-30-1 cannon with 150 rounds8,000 kg (17,600 lb) on 10 external pylons

Up to 6 medium-range AA missiles R-27, 4 short-range heat-seeking AA missiles R-73Upgraded Su-27SM is capable of using R-77 instead of R-27

Su-27IB can be used to launch X-31 anti-radiation missiles, air-to-ground missiles X-29L/T (laser/TV guidance, which may be projected to helmet), KAB-150 and UAB-500 bombs with laser, TV, or IR guidance


Sukhoi Su-30

General characteristicsCrew: 2Length: 22.10 m (72 ft 51 in)Wingspan: 14.70 m (48 ft 23 in)Height: 6.38 m (22 ft 89 in)Wing area: 62.04 m² (667.8 ft²)Empty weight: 17,700 kg (39,300 lb)Loaded weight: 34,500 kg (76,100 lb)Max takeoff weight: 38,800 kg (85,600 lb)Powerplant: 2× Lyulka AL-31FP turbofans with thrust vectoring, 131 kN (29,400 lbf) each

PerformanceRange: 5,000 km (1,600 nm, 1,900 mi) unrefueledService ceiling: 20,000 m (59,000 ft)Rate of climb: >303 m/s (60,000 ft/min)Wing loading: 556 kg/m² (113 lb/ft²)Thrust/weight: 0.77

Weapons and payloadThe Su-30MKI combat load is mounted on 12 stations. The maximum advertised combat load is 8000 kg (17,600 lb). The aircraft features the built-in single-barrel GSh-301 gun, a 30 mm weapon, and space for 150 rounds. Over 70 versions of guided and unguided weapon stores may be employed, which allows the aircraft to fly the most diverse tactical missions.


Sukhoi Su-33

General characteristicsCrew: 1Length: 21.94 m (72 ft 0 in)Wingspan: 7.40 m folded, 14.70 m extended (24 ft 3 in / 48 ft 3 in)Height: 5.93 m (19 ft 6 in)Wing area: 62 m² (667.4 ft²)Empty weight: 18,400 kg (40,600 lb)Loaded weight: 29,940 kg (66,010 lb)Max takeoff weight: 33,000 kg (72,750 lb)Powerplant: 2× Lyulka AL-31F afterburning turbofans, 123 kN (27,650 lbf) each

PerformanceMaximum speed: Mach 2.17, 2,300 km/h at 10,000 m (1,430 mph at 33,000 ft)Stall speed: 240 km/h (150 mp/h)Range: 3,000 km (1,860 miMaximum turn: +8 gs (+78 m/s²)Landing speed: 235-250 km/h (145-155 mph))Service ceiling: 17,000 m (55,800 ft)Rate of climb: 230 m/s (45,275 ft/min)Wing loading: 483 kg/m²; (98.9 lb/ft²)Thrust/weight: 0.83

Armament1x 30 mm GSh-30-1 cannon with 150 roundsUp to 6,500 kg (14,300 lb) of munitions on twelve external hardpoints, including:

R-27/R-73 air-to-air missilesVarious bombs and rocketsECM pods


Sukhoi Su-35

General characteristicsCrew: OneLength: 22.20 m (72.83 ft)Wingspan: 15.15 m (49.70 ft)Height: 6.43 m (21.08 ft)Wing area: 62.0 m² (666 ft²)Empty weight: 17,500 kg (38,600 lb)Loaded weight: 25,700 kg (56,660 lb)Max takeoff weight: 34,000 kg (74,995 lb)Powerplant: 2× Lyulka AL-35F turbofans

PerformanceMaximum speed: 2,450 km/h (1,520 mph)Range: 4,000 km (2,500 mi)Service ceiling: 18,000 m (59,100 ft)Rate of climb: 230 m/s (45,245 ft/min)Wing loading: 85.1 lb/ft² (414.5 kg/ft²)

Armament1× 30 mm GSh-30 cannon with 150 rounds2× wingtip rails for R-73 (AA-11 'Archer') air-to-air missiles12× wing and fuselage stations for up to 8,000 kg (17,630 lb) of ordnance, including:

Air-to-Air MissilesAA-12 AdderAA-11 ArcherAA-10 Alamo

Air-to-Surface MissilesAS-17 KryptonAS-16 KickbackAS-10 KarenAS-14 KedgeAS-15 KentAS-13 Kingbolt

BombsKAB-500LKAB-1500 laser/TV Guided BombFAB-100/250/500/750/1000


Sukhoi Su-37

General characteristicsCrew: One pilotLength: 22.183 m (72 ft 9 in)Wingspan: 14.7 m (48 ft 3 in)Height: 6.43 m (21 ft 1 in)Wing area: 62.0 m² (667 ft²)Empty weight: 18,500 kg (40,790 lb)Max takeoff weight: 35,000 kg (77,160 lb)Powerplant: 2× Lyulka AL-37FU turbofans, 145 kN (32,000 lbf) each

PerformanceMaximum speed: 2,500 km/h at high altitude (1,550 mph [1])Range: 3,700 km (2,230 mi)Service ceiling: 18,000 m (59,100 ft)

Armament1× 30 mm GSh-30 cannon with 150 rounds12× wing and fuselage stations for up to 8,200 kg (18,080 lb) of ordnance


Northrop YF-23

General characteristicsCrew: 1 (pilot)Length: 67 ft 5 in (20.60 m)Wingspan: 43 ft 7 in (13.30 m)Height: 13 ft 11 in (4.30 m)Wing area: 900 ft² (88m²)Empty weight: 29,000 lb (14,970 kg)Loaded weight: 51,320 lb (23,327 kg)Max takeoff weight: 62,000 lb (29,029 kg)Powerplant: × General Electric YF120 or Pratt & Whitney YF119 , 35,000 lbf (156 kN) each

Performance* Maximum speed: Mach 2.2+ (1,650+ mph, 2,655+ km/h) at altitude* Cruise speed: Mach 1.6+ est. (1,060+ mph, 1,706+ km/h) supercruise at altitude* Combat radius: 865-920 mi [5] (750-800 nmi, 1,380-1480 km)* Service ceiling: 65,000 ft (19,800 m)* Wing loading: 54 lb/ft² (265 kg/m²)* Thrust/weight: 1.36

ArmamentNone as tested but provisions made for1× 20 mm M61 Vulcan cannon4× air-to-air missiles, AIM-120 AMRAAM and AIM-9 Sidewinder

ejemplos rfp usfaero.us.es/adesign/rfp/ejemplos/ejemplos rfp usf.pdf · 2008. 6. 1. · 01/06/2008...

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