AKA: Recoverable Booster Space System. Status: Study 1962. Payload: 6,800 kg (14,900 lb). Thrust: 519.00 kN (116,675 lbf). Gross mass: 230,000 kg (500,000 lb). Height: 56.40 m (185.00 ft). Diameter: 9.14 m (29.98 ft). Span: 32.01 m (105.01 ft). Apogee: 160 km (90 mi).
LEO Payload: 6,800 kg (14,900 lb) to a 160 km orbit at 90.00 degrees.
Family: aircraft-launched, orbital launch vehicle, Winged. Country: USA. Spacecraft: Dynasoar. Agency: North American. Bibliography: 44. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9RetroSearch is an open source project built by @garambo | Open a GitHub Issue
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