This page no longer updated from 31 October 2001. Latest version can be found at SE-10

SE-10 -

Credit: Boeing / Rocketdyne. 5,448 bytes. 139 x 234 pixels.

Manufacturer Name: SE-10. Designer: Rocketdyne. Developed in: 1963. Propellants: N2O4/Aerozine-50 Thrust(vac): 4,760 kgf. Isp: 305 sec. Comments: Lunar Module Descent. Pressure-fed. Thrust throttleable 1050-10,500 lbs vac.
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Last update 12 March 2001.
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© Mark Wade, 2001 .