This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com

astronautix.com Martlet 4L-3


Gross Mass: 58 kg. Empty Mass: 9 kg. Thrust (vac): 550 kgf. Isp: 300 sec. Burn time: 30 sec. Propellants: N2O4/UDMH Isp(sl): 210 sec. Diameter: 0.4 m. Span: 0.4 m. Length: 0.7 m. Country: Canada. No Engines: 1. Martlet 4-3 Status: Study.
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Last update 12 March 2001.
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© Mark Wade, 2001 .