| Nova 59-4-2 |
home
topic index |
|
Model: Nova 59-4-2. Gross Mass: 590,000 kg (1,300,000 lb). Empty Mass: 45,000 kg (99,000 lb). Thrust (vac): 7,560.000 kN (1,699,550 lbf). Isp: 310 sec. Burn time: 215 sec. Propellants: Lox/Kerosene. Isp(sl): 265 sec. Diameter: 5.20 m (17.00 ft). Span: 5.20 m (17.00 ft). Length: 16.20 m (53.10 ft). Country: USA. No Engines: 1. Motor: F-1. Status: Study 1959. First Flight: 1961. Last Flight: 1961. No Launched: 1. Empty Mass Estimated 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 - 2008 except where otherwise noted. |