|
N1F 1965 - V
|
|
Gross Mass: 300,000 kg (660,000 lb). Empty Mass: 20,000 kg (44,000 lb). Thrust (vac): 2,450.000 kN (550,780 lbf). Isp: 347 sec. Burn time: 380 sec. Propellants: Lox/Kerosene. Diameter: 4.80 m (15.70 ft). Span: 6.80 m (22.30 ft). Length: 16.00 m (52.00 ft). Country: Russia. No Engines: 4. Engine: 11D53F. Status: Study 1965. As per N1 improvement study, 1965. Engine thrust increased and stretched propellant tanks with almost 50% increase.
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.
|
|
|
|