This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Used on stages: Martlet 4-3. Used on launch vehicles: Martlet 4. Gross Mass: 45 kg. Empty Mass: 10 kg. Propellants: Solid Thrust(vac): 550 kgf. Thrust(vac): 5.39 kN. Isp: 300 sec. Isp (sea level): 210 sec. Burn time: 19 sec. Diameter: 0.3 m. Length: 1.0 m. Chambers: 1. Country: Canada. Status: Study 1962.
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Last update 12 March 2001.
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© Mark Wade, 2001 .