Aerospike Annular Booster home
topic index
AERO
Credit - Boeing / Rocketdyne
Engine Model: Aerospike Annular Booster. Designer: Rocketdyne. Developed in: 1967. Propellants: Lox/LH2. Thrust(vac): 1,111.662 kN (249,912 lbf). Isp: 450 sec. Country: USA.

Aerospike Typical Annular Booster . Pressure-fed. Thrust from 50,000 to 250,000 lbs at altitude.

Contact us with any corrections, additions, or comments.
Conditions for use of drawings, pictures, or other materials from this site..
To contact astronauts or cosmonauts.

© Mark Wade, 1997 - 2008 except where otherwise noted.