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Engine Model: Martlet 4-3. Designer: Bull. Gross Mass: 45 kg (99 lb). Empty Mass: 10 kg (22 lb). Propellants: Solid. Thrust(vac): 5.390 kN (1,212 lbf). Thrust(sl): 3.776 kN (849 lbf). Isp: 300 sec. Isp (sea level): 210 sec. Burn time: 19 sec. Diameter: 0.30 m (0.98 ft). Length: 1.00 m (3.20 ft). Chambers: 1. Country: Canada. Status: Development ended 1966.
Martlet 4-3 used on Rocket Stages
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