Thrust Profile (N)
1.45s Burn WindowEngineered by Loki Research, the J650-SF is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 942.0 Ns over a 1.45 second burn window.
With an average thrust of 648.0 N and a peak of 974.0 N, it features a neutral thrust curve optimal for general sport flying. It utilizes the Spitfire propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
1143g TotalDesign wings in your spreadsheet
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