|
Saturn S-N C-5N
|
|
Gross Mass: 53,694 kg (118,375 lb). Empty Mass: 10,429 kg (22,992 lb). Thrust (vac): 266.799 kN (59,979 lbf). Isp: 800 sec. Burn time: 1,250 sec. Propellants: Nuclear/LH2. Diameter: 10.06 m (33.00 ft). Span: 10.06 m (33.00 ft). Length: 19.30 m (63.30 ft). Country: USA. No Engines: 1. Engine: Nerva. Status: Study 1961. Used as: Saturn C-5N-3. Nuclear upper stage considered in lieu of S-IVB in final Saturn C-5 study in November 1961. Used on Launch Vehicles:
|
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.
|
|
|
|