| Ikar |
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Model: Ikar. Gross Mass: 3,164 kg (6,975 lb). Empty Mass: 820 kg (1,800 lb). Thrust (vac): 2.940 kN (661 lbf). Isp: 326 sec. Burn time: 600 sec. Propellants: N2O4/UDMH. Diameter: 2.72 m (8.92 ft). Span: 2.72 m (8.92 ft). Length: 2.56 m (8.39 ft). Country: Russia. No Engines: 1. Motor: 17D61. Status: Design 1999. Derived from propulsion module of Yantar spysat, over 30 flights to 1998. 50 restarts. 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 - 2008 except where otherwise noted. |