This page no longer updated from 31 October 2001. Latest version can be found at SE-8

SE-8 -

Credit: Boeing / Rocketdyne. 7,363 bytes. 165 x 226 pixels.

Manufacturer Name: SE-8. Designer: Rocketdyne. Developed in: 1964. Propellants: N2O4/MMH Thrust(vac): 42 kgf. Isp: 274 sec. Comments: Apollo Command Module Reaction Control. Pressure-fed.
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Last update 12 March 2001.
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© Mark Wade, 2001 .