|
260 inch solid TL
|
|
Gross Mass: 561,000 kg (1,236,000 lb). Empty Mass: 60,600 kg (133,600 lb). Thrust (vac): 10,105.311 kN (2,271,764 lbf). Isp: 275 sec. Burn time: 130 sec. Propellants: Solid. Diameter: 6.60 m (21.60 ft). Span: 6.60 m (21.60 ft). Length: 21.65 m (71.03 ft). Country: USA. No Engines: 1. Engine: AJ-260-1/3. Status: Study NASA 1969. Study NASA 1969
|
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 - 2007 except where otherwise noted.
|
|
|
|