UR-500MK-1
Gross Mass: 137,000 kg (302,000 lb). Empty Mass: 9,300 kg (20,500 lb). Thrust (vac): 1,637.000 kN (368,012 lbf). Isp: 331 sec. Burn time: 250 sec. Propellants: Lox/Kerosene. Diameter: 4.15 m (13.61 ft). Span: 4.15 m (13.61 ft). Length: 20.00 m (65.00 ft). Country: USSR. No Engines: 1. Engine: NK-33. Status: Design 1975.

Empty mass estimated based on overall vehicle mass fraction. Length estimated based on total mass.


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.

 
Encyclopedia Astronautica
topic index
0 - A - B - C - D - E - F - G - H - I - J - K - L - M - N - O - P - Q - Ra - Re - Sa - Sf - Sp - T - U - V - W - X - Y - Z