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Shuttle C Block II
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Shuttle-C
Credit: Boeing American orbital launch vehicle. In August 1989 NASA studied a version of the Shuttle-C with two Advanced Solid Rocket Motors (ASRM's) in place of the standard RSRM's. This would increase the payload by 4500 kg, but also require use of a new 10 m x 30 m payload module.
Status: Design 1990. Payload: 81,500 kg (179,600 lb). Apogee: 407 km (252 mi).
LEO Payload: 81,500 kg (179,600 lb) to a 407 km orbit at 28.50 degrees.
Family: orbital launch vehicle, Winged. Country: USA. Agency: Martin. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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