Thrust Profile (N)
0.68s Burn WindowEngineered by Animal Motor Works, the 932J1365-P is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 932.4 Ns over a 0.68 second burn window.
With an average thrust of 1365.3 N and a peak of 1568.2 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Scalded Tiger propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
1119g TotalDesign wings in your spreadsheet
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