Shuttle SERV-1

Shuttle SERV-1

home
topic index

Model: Shuttle SERV-1. Gross Mass: 2,040,816 kg (4,499,229 lb). Empty Mass: 226,757 kg (499,913 lb). Thrust (vac): 31,980.515 kN (7,189,506 lbf). Isp: 455 sec. Burn time: 249 sec. Propellants: Lox/LH2. Isp(sl): 367 sec. Diameter: 18.29 m (60.00 ft). Span: 27.44 m (90.02 ft). Length: 20.27 m (66.50 ft). Country: USA. No Engines: 1. Motor: Plug-Nozzle SERV. Status: Study 1971. First Flight: 1978.

Single stage to orbit, ballistic reentry.

Used on Launch Vehicles:

Shuttle.

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.