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Sunday, September 14, 2014

Fast Bomber

Wiki Pedia: Typical Air-to-Air Missiles
Missile is faster than aircraft
Weight
Rocket Name
Country of origin
Period of manufacture and use
Warhead weight
Warhead types
Range
Speed
meter/se
43.5 kg
1974-
3 kg
8 km
Mach 2.7
926.1 m/s
86 kg
1956-
9.4 kg
18 km
Mach 2.5
87.4 kg
Diehl IRIS-T
2005-
11.4 kg
HE/fragmentation
25 km
Mach 3
88 kg
2002-
10 kg
Blast/fragmentation
18 km
Mach 3+
89 kg
1976-1986 (Magic)
1986- (Magic 2)
12.5 kg
Blast/fragmentation
15 km
Mach 2.7
105 kg
1982-
7.4 kg
Fragmentation
20–40 km
Mach 2.5
112 kg
1996- (EM)
2000- (IR)
12 kg
Blast/fragmentation
(focused splinters HE)
> 60 km
Mach 4
118 kg
1990-
23 kg
Blast/fragmentation
50 km
Mach 4
152 kg
2008
18 kg
Blast/fragmentation
180 km
Mach 4
152 kg
1996
18 kg
Blast/fragmentation
105 km
Mach 4
152 kg
1994-
23 kg
Blast/fragmentation
48 km
Mach 4
175 kg
1994-
22 kg
Blast/fragmentation
160 km
Mach 4.5
154 kg
2010-
15 kg
HE fragmentation directional warhead
80-110+ km
Mach 4.5+
185 kg
2012-
?
Blast/fragmentation
200+ km[12]
Mach 4+
748 kg
2010-
50 kg
HE fragmentation directional warhead
200-400+ km
Mach 4+
Bibliographic Entry
Result
(w/surrounding text)
Standardized
Result
"747 Jumbo Jet." Microsoft Encarta Encyclopedia. CD-ROM, 2000.
"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)."
245 m/s
Air Transportation. Aerospace Industries Association of America, 1997: 316.
"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."
241 m/s
747 Family. Boeing.
"Cruising speed: 570 mph
Range: 3,110 miles
Ceiling: 36,100 feet
Power: Three 14,000-pound-thrust P&W engines
Accommodation: 131 passengers"
250 m/s

"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."
260 m/s
Beichner, Robert J., and Raymond A. Serway. Physics for Scientists and Engineers. 5th ed. Orlando: Harcourt College, 2000. 52.
"A plane is traveling at 100 m/s …."
100 m/s
Speed of the Fastest Airplane
Edited by Glenn Elert -- Written by his students
An educational, Fair Use website
Bibliographic Entry
Result
(w/surrounding text)
Standardized
Result
Boyne, Walter. World Book Encyclopedia. New York: World Book, 1996: 208.
"… a rocket plane the fastest kind of airplane … a speed of 4,520 mph"
2020 m/s
Lockheed SR-71A. Air Force Armament Museum. Eglin Air Force Base, Florida.
"… an SR-71 set two world records for its class: an absolute speed record of 2,193.167 miles per hour"
980 m/s
Guinness Book of World Records 1968. New York: Bantam, 1968: 249.
"… the official air speed recordis 2,070.102 mph by Col. Robert L. Stephens"
925 m/s
Guinness Book of World Records 1989. New York: Bantam, 1989: 204.
"The official air speed record is 2,193.167 mph by Capt. Eldon W. Joersz in a Lockheed SR-71A"
980 m/s
In the search for the speed of the fastest airplane in air speed, the first problem was to find the difference between regular speed and air speed. Air speed is defined as the speed of an airplane with relation to the air, as compared to regular speed, which is the speed relative to the earth.

 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
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)
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
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
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
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
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
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
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)
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
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
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)
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

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)
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
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)
AGM-28 Hound Dog

Agm-28 1.jpg
AGM-28 in flight (showing the nose-high attitude)

Type
Place of origin
Service history

In service
September 13, 1960
Production history

Manufacturer
Unit cost
$690,073
Produced
April 1959
Specifications

Weight
4,603 kilograms (10,147 lb).
Length
12.95 metres (42 ft 6 in).
Height
2.84 metres (9 ft 4 in).
Diameter
710 millimetres (28 in).
Warhead
790 kilograms (1,742 lb) W28 Class D bomb.
Detonation
mechanism
Airburst or Contact
Engine
Pratt & Whitney J52-P-3 turbojet; 33 kN (7,500 lbf).
Wingspan
3.71 metres (12 ft 2 in).
Operational
range
1,263 kilometres (785 mi).
Flight ceiling
17,100 metres (56,200 ft).
Flight altitude
61 to 17,069 metres (200 to 56,000 ft).
Speed
Mach 2.1.
Guidance
system
Inertial with star-tracker correction.
Launch
platform


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