Martlet 4A
Gross Mass: 890 kg (1,960 lb). Empty Mass: 155 kg (341 lb). Thrust (vac): 67.600 kN (15,197 lbf). Isp: 300 sec. Burn time: 30 sec. Propellants: Solid. Isp(sl): 210 sec. Diameter: 0.42 m (1.37 ft). Span: 2.20 m (7.20 ft). Length: 4.00 m (13.10 ft). Country: Canada. No Engines: 1. Engine: Martlet 4-1. Status: Development ended 1966. First Flight: 1962.

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