Timberwind 75 Propellants: Nuclear/LH2. Thrust(vac): 735.500 kN (165,347 lbf). Thrust(sl): 654.600 kN (147,160 lbf). Isp: 1,000 sec. Isp (sea level): 890 sec. Burn time: 357 sec. Mass Engine: 2,500 kg (5,500 lb). Diameter: 2.03 m (6.67 ft). Chambers: 1. Thrust to Weight Ratio: 30.00. Country: USA. Status: Development ended 1992. Timberwind 75 used on Rocket Stages Used on stage: Timberwind 75. on launch vehicle: Timberwind Titan.                   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.

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