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Martlet 4-1
Part of Martlet 4 Family
Bull solid rocket engine. Development ended 1966. Used on Martlet 4 launch vehicle.

AKA: Martlet 4A;Martlet 4i-1. Status: Development ended 1966. Thrust: 67.70 kN (15,220 lbf). Gross mass: 570 kg (1,250 lb). Unfuelled mass: 110 kg (240 lb). Specific impulse: 300 s. Specific impulse sea level: 210 s. Burn time: 20 s. Diameter: 0.30 m (0.98 ft).

Thrust (sl): 47.400 kN (10,656 lbf). Thrust (sl): 4,830 kgf.



Country: Canada. Launch Vehicles: Martlet 4, Martlet 3D. Propellants: Solid. Stages: Martlet 4-1. Agency: Bull.

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