MB-3 Press Mod Propellants: Lox/Kerosene. Thrust(vac): 755.100 kN (169,753 lbf). Thrust(sl): 662.400 kN (148,913 lbf). Isp: 285 sec. Isp (sea level): 250 sec. Burn time: 128 sec. Mass Engine: 643 kg (1,417 lb). Diameter: 3.00 m (9.80 ft). Chambers: 1. Chamber Pressure: 40.00 bar. Area Ratio: 8.00. Thrust to Weight Ratio: 119.75. Country: USA. Status: Test 1962. MB-3 Press Mod used on Rocket Stages Used on stage: Sea Horse-1. on launch vehicle: Sea Horse.                   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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