Thrust Profile (N)
1.63s Burn WindowEngineered by Cesaroni Technology, the 660J381-15A is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 659.9 Ns over a 1.63 second burn window.
With an average thrust of 380.6 N and a peak of 503.1 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Skidmark propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
688g TotalDesign wings in your spreadsheet
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