This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
- Propellant Formulation: 25%H/SH2 Free Radical. Isp: 680.00 sl. Temperature of Combustion: 2,050.00 deg K.
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Last update 3 May 2001.
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© Mark Wade, 2001 .