Thrust Profile (N)
1.64s Burn WindowEngineered by AeroTech, the J435WS is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 742.8 Ns over a 1.64 second burn window.
With an average thrust of 441.6 N and a peak of 712.9 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Super White Lightning propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
616.4g TotalDesign wings in your spreadsheet
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