Tsyklon 3-3
Gross Mass: 4,600 kg (10,100 lb). Empty Mass: 1,407 kg (3,101 lb). Thrust (vac): 78.708 kN (17,694 lbf). Isp: 317 sec. Burn time: 125 sec. Propellants: N2O4/UDMH. Diameter: 2.25 m (7.38 ft). Span: 2.25 m (7.38 ft). Length: 2.58 m (8.46 ft). Country: Russia. No Engines: 1. Engine: RD-861. Status: In production. Cost $ : 2.000 million. First Flight: 1977. Last Flight: 2004. No Launched: 121. No Failed: 6. Used as: Tsyklon 3; Ikar. Other designations: 11S693; S5M.


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