| F-15 |
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Model: F-15. Gross Mass: 16,921 kg (37,304 lb). Empty Mass: 11,833 kg (26,087 lb). Thrust (vac): 127.721 kN (28,713 lbf). Isp: 1,552 sec. Burn time: 7,000 sec. Propellants: Air/Kerosene. Isp(sl): 1,411 sec. Diameter: 5.67 m (18.60 ft). Span: 13.04 m (42.78 ft). Length: 19.45 m (63.81 ft). Country: USA. No Engines: 2. Motor: F100-100. Status: In Production. Cost $ : 42.750 million. Payload: 545 kg (1,201 lb). Release velocity: 715 m/s (2,345 ft/sec). Release altitude: 12 m (38 ft). Release angle: 80 deg. Release conditions: 2,580 kph at 11.6 km. McDonnell Interceptor-cropped delta. Maximum release conditions: 545 kg (2.0 m length x 0.5 m wingspan) at 2,580 kph at 11,582 m altitude (ASAT). Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted. |