|
Vulkan 1
|
|
Gross Mass: 800,000 kg (1,760,000 lb). Empty Mass: 80,000 kg (176,000 lb). Thrust (vac): 7,450.000 kN (1,674,820 lbf). Isp: 452 sec. Burn time: 420 sec. Propellants: Lox/LH2. Isp(sl): 351 sec. Diameter: 7.75 m (25.42 ft). Span: 8.00 m (26.20 ft). Length: 52.00 m (170.00 ft). Country: Russia. No Engines: 4. Engine: RD-0120. Status: Development ended 1976. Original version of Energia core as used on Vulkan booster, with in-line upper stages and payloads. Developed 1974-1976; cancelled when Energia / Buran development begun.
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.
|
|
|
|