This page no longer updated from 31 October 2001. Latest version can be found at Aerospike Annular Booster


Credit: Boeing / Rocketdyne. 9,568 bytes. 166 x 236 pixels.

Designer: Rocketdyne. Developed in: 1967. Propellants: Lox/LH2 Thrust(vac): 113,358 kgf. Isp: 450 sec. Comments: Aerospike Typical Annular Booster . Pressure-fed. Thrust from 50,000 to 250,000 lbs at altitude.
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Last update 12 March 2001.
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© Mark Wade, 2001 .