MAKS Tank
Gross Mass: 248,100 kg (546,900 lb). Empty Mass: 10,820 kg (23,850 lb). Thrust (vac): 0 N ( lbf). Isp: 437 sec. Burn time: 440 sec. Propellants: Lox/Kerosene/LH2. Isp(sl): 396 sec. Diameter: 6.38 m (20.93 ft). Span: 6.38 m (20.93 ft). Length: 32.10 m (105.30 ft). Country: Russia. No Engines: 1. Engine: None. Status: Development ended 1988. Cost $ : 5.000 million. First Flight: 1992.

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