This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Used on stages: Martlet 4-1. Used on launch vehicles: Martlet 4. Gross Mass: 570 kg. Empty Mass: 110 kg. Propellants: Solid Thrust(vac): 6,900 kgf. Thrust(vac): 67.70 kN. Isp: 300 sec. Isp (sea level): 210 sec. Burn time: 20 sec. Diameter: 0.3 m. Chambers: 1. Country: Canada. Status: Study 1962.
Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .