Wiki Pedia: Typical Air-to-Air Missiles
Missile is faster than aircraft
Weight
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Rocket Name
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Country of origin
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Period of manufacture and use
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Warhead weight
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Warhead types
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Range
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Speed
meter/se
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43.5 kg
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1974-
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3 kg
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8 km
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Mach 2.7
926.1 m/s
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86 kg
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1956-
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9.4 kg
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18 km
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Mach 2.5
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87.4 kg
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Diehl IRIS-T
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2005-
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11.4 kg
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HE/fragmentation
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25 km
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Mach 3
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88 kg
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2002-
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10 kg
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Blast/fragmentation
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18 km
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Mach 3+
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89 kg
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1976-1986 (Magic)
1986- (Magic 2)
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12.5 kg
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Blast/fragmentation
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15 km
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Mach 2.7
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105 kg
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1982-
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7.4 kg
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Fragmentation
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20–40 km
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Mach 2.5
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112 kg
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1996- (EM)
2000- (IR)
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12 kg
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Blast/fragmentation
(focused splinters HE)
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> 60 km
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Mach 4
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118 kg
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1990-
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23 kg
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Blast/fragmentation
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50 km
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Mach 4
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152 kg
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2008
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18 kg
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Blast/fragmentation
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180 km
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Mach 4
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152 kg
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1996
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18 kg
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Blast/fragmentation
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105 km
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Mach 4
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152 kg
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1994-
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23 kg
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Blast/fragmentation
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48 km
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Mach 4
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175 kg
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1994-
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22 kg
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Blast/fragmentation
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160 km
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Mach 4.5
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154 kg
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2010-
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15 kg
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HE fragmentation directional warhead
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80-110+ km
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Mach 4.5+
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185 kg
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2012-
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?
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Blast/fragmentation
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200+ km[12]
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Mach 4+
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748 kg
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2010-
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50 kg
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HE fragmentation directional warhead
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200-400+ km
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Mach 4+
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Bibliographic Entry
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Result
(w/surrounding text)
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Standardized
Result
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"747 Jumbo Jet." Microsoft Encarta Encyclopedia. CD-ROM, 2000.
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"This Boeing 747, commonly called a jumbo jet, makes a cargo-transport flight. The 747, the first of the wide-bodied commercial jets, had its inaugural flight in 1970. Four jet engines propel the plane, which reaches cruising speeds of 885 km/hr (550 mph)."
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245 m/s
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Air Transportation. Aerospace Industries Association of America, 1997: 316.
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"Such aircraft generally cruise at speeds of approximately 540 mi/h or 870 km/hr and at altitudes high enough that aircraft pressurization is required."
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241 m/s
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747 Family. Boeing.
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"Cruising speed: 570 mph
Range: 3,110 miles
Ceiling: 36,100 feet
Power: Three 14,000-pound-thrust P&W engines
Accommodation: 131 passengers"
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250 m/s
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"And, the 747 continues to be the world's fastest subsonic jetliner, cruising at Mach 0.85 -- or 85 percent of the speed of sound. Along with the popular Boeing 777, the 747 is a key element of the Boeing long-range market strategy."
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260 m/s
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Beichner, Robert J., and Raymond A. Serway. Physics for Scientists and Engineers. 5th ed. Orlando: Harcourt College, 2000. 52.
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"A plane is traveling at 100 m/s …."
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100 m/s
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Speed of the Fastest Airplane
Edited by Glenn Elert -- Written by his students
An educational, Fair Use website
Bibliographic Entry
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Result
(w/surrounding text)
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Standardized
Result
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Boyne, Walter. World Book Encyclopedia. New York: World Book, 1996: 208.
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"… a rocket plane the fastest kind of airplane … a speed of 4,520 mph"
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2020 m/s
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Lockheed SR-71A. Air Force Armament Museum. Eglin Air Force Base, Florida.
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"… an SR-71 set two world records for its class: an absolute speed record of 2,193.167 miles per hour"
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980 m/s
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Guinness Book of World Records 1968. New York: Bantam, 1968: 249.
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"… the official air speed recordis 2,070.102 mph by Col. Robert L. Stephens"
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925 m/s
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Guinness Book of World Records 1989. New York: Bantam, 1989: 204.
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"The official air speed record is 2,193.167 mph by Capt. Eldon W. Joersz in a Lockheed SR-71A"
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980 m/s
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F-18 E/F Super Hornet (USA)
Maximum speed: Mach 1.8+ (1,190 mph, 1,900 km/h) at 40,000 ft (12,190 m)
Range: 1,275 nmi (2,346 km) clean plus two AIM-9s
Combat radius: 390 nmi (449 mi, 722 km) for interdiction mission
Ferry range: 1,800 nmi (2,070 mi, 3,330 km)
Service ceiling: 50,000+ ft (15,000+ m)
Wing loading: 92.8 lb/ft² (453 kg/m²)
Thrust/weight: 0.93
F-18 E/F Super Hornet (USA)
Maximum speed: Mach 1.8+ (1,190 mph, 1,900 km/h) at 40,000 ft (12,190 m)
Range: 1,275 nmi (2,346 km) clean plus two AIM-9s
Combat radius: 390 nmi (449 mi, 722 km) for interdiction mission
Ferry range: 1,800 nmi (2,070 mi, 3,330 km)
Service ceiling: 50,000+ ft (15,000+ m)
Wing loading: 92.8 lb/ft² (453 kg/m²)
Thrust/weight: 0.93
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J-10 (People’s Republic of China)
Maximum speed: Mach 1.9 at altitude, Mach 1.2 at sea level
g-limits: +9/-3 g (+88/-29 m/s², +290/-97 ft/s²)
Combat radius:
On hi-lo-hi mission: 2,540 km (1,370 nautical miles) with 4,000lb/1,814kg bombload and two air-to-air missiles
On lo-lo-lo mission: 1,310 km (710 nautical miles with 4,000lb/1,814kg bombload and two air-to-air missiles
Maximum range (without refueling): 3,400 km (2,113 mi) ()
Service ceiling: 18,000 m (59,055 ft)
Wing loading: 335 kg/m² (64 lb/ft²)
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Dassault Rafale (France)
Maximum speed:
High altitude: Mach 2 (1,290 knots)
Low altitude: 1,390 km/h, 750 knots
Range: 3,700+ km (2,000+ nmi)
Combat radius: 1,852+ km (1,000+ nmi) on penetration mission
Service ceiling: 16,800 m (55,000 ft)
Rate of climb: 304.8+ m/s (1,000+ ft/s)
Wing loading: 326 kg/m² (83 1/3 lb/ft²)
Thrust/weight: 1.13
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F-16 E Fighting Falcon Block 60 (USA)
Maximum speed:
At sea level: Mach 1.2 (915 mph, 1,470 km/h)
At altitude: Mach 2+ (1,500 mph, 2,414 km/h)
Combat radius: 340 mi (295 nm, 550 km) on a hi-lo-hi mission with six 1,000 lb (450 kg) bombs
Ferry range: 2,280 NM (2,620 mi, 4,220 km) with drop tanks
Service ceiling: 60,000+ ft (18,000+ m)
Rate of climb: 50,000 ft/min (254 m/s)
Wing loading: approx 40 lb/ft² (430 kg/m²)
Thrust/weight: 1.095
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Mig-35 (Russia)
Maximum speed: Mach 2.25 (2,400 km/h, 1,491 mph) at altitude
Range: 2,000 km (1,240 mi)
Ferry range: 3,100 km (1,930 mi) with 3 external fuel tanks
Service ceiling: 17,500 m (57,400 ft)
Rate of climb: 330 m/s (65,000 ft/min)
Thrust/weight: 1.03
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Su-27 (Russia)
Maximum speed: Mach 2.35 (2,500 km/h, 1,550 mph) at altitude
Range: 3,530 km (2,070 mi) at altitude; (1,340 km / 800 mi at sea level)
Service ceiling: 18,500 m (62,523 ft)
Rate of climb: 300 m/s (64,000 ft/min)
Wing loading: 371 kg/m² (76 lb/ft²)
Thrust/weight: 1.09
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F-18 E/F Super Hornet (USA)
Maximum speed: Mach 1.8+ (1,190 mph, 1,900 km/h) at 40,000 ft (12,190 m)
Range: 1,275 nmi (2,346 km) clean plus two AIM-9s
Combat radius: 390 nmi (449 mi, 722 km) for interdiction mission
Ferry range: 1,800 nmi (2,070 mi, 3,330 km)
Service ceiling: 50,000+ ft (15,000+ m)
Wing loading: 92.8 lb/ft² (453 kg/m²)
Thrust/weight: 0.93
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Dassault Rafale (France)
Maximum speed:
High altitude: Mach 2 (1,290 knots)
Low altitude: 1,390 km/h, 750 knots
Range: 3,700+ km (2,000+ nmi)
Combat radius: 1,852+ km (1,000+ nmi) on penetration mission
Service ceiling: 16,800 m (55,000 ft)
Rate of climb: 304.8+ m/s (1,000+ ft/s)
Wing loading: 326 kg/m² (83 1/3 lb/ft²)
Thrust/weight: 1.13
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J-10 (People’s Republic of China)
Maximum speed: Mach 1.9 at altitude, Mach 1.2 at sea level
g-limits: +9/-3 g (+88/-29 m/s², +290/-97 ft/s²)
Combat radius:
On hi-lo-hi mission: 2,540 km (1,370 nautical miles) with 4,000lb/1,814kg bombload and two air-to-air missiles
On lo-lo-lo mission: 1,310 km (710 nautical miles with 4,000lb/1,814kg bombload and two air-to-air missiles
Maximum range (without refueling): 3,400 km (2,113 mi) ()
Service ceiling: 18,000 m (59,055 ft)
Wing loading: 335 kg/m² (64 lb/ft²)
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F-16 E Fighting Falcon Block 60 (USA)
Maximum speed:
At sea level: Mach 1.2 (915 mph, 1,470 km/h)
At altitude: Mach 2+ (1,500 mph, 2,414 km/h)
Combat radius: 340 mi (295 nm, 550 km) on a hi-lo-hi mission with six 1,000 lb (450 kg) bombs
Ferry range: 2,280 NM (2,620 mi, 4,220 km) with drop tanks
Service ceiling: 60,000+ ft (18,000+ m)
Rate of climb: 50,000 ft/min (254 m/s)
Wing loading: approx 40 lb/ft² (430 kg/m²)
Thrust/weight: 1.095
Fighting Falcons in Flight
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Su-27 (Russia)
Maximum speed: Mach 2.35 (2,500 km/h, 1,550 mph) at altitude
Range: 3,530 km (2,070 mi) at altitude; (1,340 km / 800 mi at sea level)
Service ceiling: 18,500 m (62,523 ft)
Rate of climb: 300 m/s (64,000 ft/min)
Wing loading: 371 kg/m² (76 lb/ft²)
Thrust/weight: 1.09
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Eurofighter Typhoon (U.K., Germany, Italy, Spain)
Maximum speed:
At altitude: Mach 2+ (2,495 km/h, 1,550 mph)
At sea level: Mach 1.2 (1470 km/h / 913.2 mph)
Supercruise: Mach 1.1-1.5
Range: 2,900 km (1,840 mi)
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Su-35 (Russia)
Maximum speed: Mach 2.25 (2,410 km/h, 1,500 mph) at altitude
Range: 3,600 km (1,940 nmi) ; (1,580 km, 850 nmi near ground level)
Ferry range: 4,500 km (2,430 nmi) with external fuel tanks
Service ceiling: 18,000 m (59,100 ft)
Rate of climb: >280 m/s (>55,100 ft/min)
Wing loading: 408 kg/m² (84.9 lb/ft²)
Thrust/weight: 1.14
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Combat radius:
Ground attack, lo-lo-lo: 601 km (373 nmi)
Ground attack, hi-lo-hi: 1,389 km (863 nmi)
Air defence with 3-hr CAP: 185 km (115 nmi)
Air defence with 10-min loiter: 1,389 km (863 mi)
Ferry range: 3,790 km (2,300 mi)
Service ceiling: 19,810 m (65,000 ft)
Rate of climb: >315 m/s (62,000 ft/min)
Wing loading: 307 kg/m² (63 lb/ft²)
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Mig-35 (Russia)
Maximum speed: Mach 2.25 (2,400 km/h, 1,491 mph) at altitude
Range: 2,000 km (1,240 mi)
Ferry range: 3,100 km (1,930 mi) with 3 external fuel tanks
Service ceiling: 17,500 m (57,400 ft)
Rate of climb: 330 m/s (65,000 ft/min)
Thrust/weight: 1.03
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F-15 C/D Eagle (USA)
Maximum speed:
High altitude: Mach 2.5+ (1,650+ mph, 2,660+ km/h)
Low altitude: Mach 1.2 (900 mph, 1,450 km/h)
Combat radius: 1,061 nmi (1,222 mi, 1,967 km) for interdiction mission
Ferry range: 3,450 mi (3,000 nmi, 5,550 km) with conformal fuel tanks and three external fuel tanks
Service ceiling: 65,000 ft (20,000 m)
Rate of climb: >50,000 ft/min (254 m/s)
Wing loading: 73.1 lb/ft² (358 kg/m²)
Thrust/weight: 1.12 (-220), 1.30 (-229)
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AGM-28 Hound Dog
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AGM-28 in flight (showing the nose-high attitude)
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Type
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Place of origin
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Service history
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In service
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September 13, 1960
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Production history
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Manufacturer
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Unit cost
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$690,073
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Produced
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April 1959
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Specifications
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Weight
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4,603 kilograms (10,147 lb).
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Length
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12.95 metres (42 ft 6 in).
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Height
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2.84 metres (9 ft 4 in).
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Diameter
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710 millimetres (28 in).
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Warhead
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Detonation
mechanism
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Airburst or Contact
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Engine
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Pratt & Whitney J52-P-3 turbojet; 33 kN (7,500 lbf).
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Wingspan
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3.71 metres (12 ft 2 in).
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Operational
range
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1,263 kilometres (785 mi).
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Flight ceiling
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17,100 metres (56,200 ft).
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Flight altitude
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61 to 17,069 metres (200 to 56,000 ft).
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Speed
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Mach 2.1.
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Guidance
system
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Launch
platform
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End
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