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AABS
Aerospike Annular - Aerospike Annular Booster
Credit: Boeing / Rocketdyne. 8,229 bytes. 166 x 233 pixels.
Designer
: Rocketdyne.
Developed in
: 1967. Propellants:
Lox/Kerosene
Thrust(vac)
: 1,813 kgf.
Isp
: 285 sec.
Comments
: Aerospike Annular Booster and Sustainer. Pressure-fed. Booster thrust 3000 to 4000 lb vac; sustainer 1500-2000 lb vac, 257 sec specific impulse.
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Last update 12 March 2001.
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© Mark Wade, 2001 .
