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B-1A
Mach 2 rocket launch aircraft. N. American Bomber-variable geometry. Maximum release conditions: Bomb bay mounted, 16,364 kg (9.4 m length x 2.5 m diameter x 2.5 m span) at 2,096 kph at 11,900 m altitude.

Status: In Production. Payload: 16,364 kg (36,076 lb). Thrust: 302.40 kN (67,982 lbf). Gross mass: 159,637 kg (351,939 lb). Unfuelled mass: 81,587 kg (179,868 lb). Specific impulse: 1,980 s. Specific impulse sea level: 1,800 s. Burn time: 33,000 s. Height: 44.87 m (147.21 ft). Diameter: 10.24 m (33.59 ft). Span: 23.84 m (78.21 ft). Location: 580.

Cost $ : 167.100 million. No Engines: 4. Release velocity: 580 m/s (1,900 ft/sec). Release altitude: 12 m (39 ft). Release conditions: 2,096 kph at 11.9 km.



Country: USA. Engines: F101. Propellants: Air/Kerosene.

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