LAPSTAR

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Engine Model: LAPSTAR. Designer: WRE. Gross Mass: 300 kg (660 lb). Propellants: Solid. Thrust(vac): 80.000 kN (17,984 lbf). Burn time: 2.70 sec. Diameter: 0.41 m (1.34 ft). Length: 1.80 m (5.90 ft). Country: Australia. LAPSTAR used on Rocket Stages Used on stage: Aeolus-1. on launch vehicle: Aeolus. Used on stage: LAPSTAR. on launch vehicle: HAD. Used on stage: LAPSTAR. on launch vehicle: HAT. 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.