D-18T Designer: Lotarev. Application: An-225. Propellants: Air/Kerosene. Thrust(vac): 229.400 kN (51,571 lbf). Thrust(sl): 203.900 kN (45,839 lbf). Isp: 9,000 sec. Isp (sea level): 8,000 sec. Burn time: 3,375 sec. Mass Engine: 4,500 kg (9,900 lb). Chambers: 1. Thrust to Weight Ratio: 5.19. Country: Ukraine. Status: Development ended 1988. D-18T used on Rocket Stages Used on stage: An-124. Used on stage: An-225. on launch vehicle: Interim HOTOL. Used on stage: An-225. on launch vehicle: MAKS. Used on stage: Gerakl. Bibliography and Further Reading Gunston, Bill, The Osprey Encylopedia of Russian Aircraft 1975-1995, Osprey, London, 1995. ISBN: 1855324059. The greatest single reference on Soviet winged aircraft. More at amazon.com...                   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 Enter your search terms   Web www.astronautix.com Submit search form