Tsyklon 2-3
Gross Mass: 3,200 kg (7,000 lb). Empty Mass: 400 kg (880 lb). Thrust (vac): 77.960 kN (17,526 lbf). Isp: 317 sec. Burn time: 112 sec. Propellants: N2O4/UDMH. Diameter: 2.00 m (6.50 ft). Span: 2.00 m (6.50 ft). Length: 2.50 m (8.20 ft). Country: Russia. No Engines: 1. Engine: RD-861. Status: In production. Cost $ : 2.000 million. First Flight: 1965. Last Flight: 2006. No Launched: 108.

Integral portion of payload.

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