Thrust Profile (N)
1.50s Burn WindowEngineered by AeroTech, the J350W is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 700.0 Ns over a 1.50 second burn window.
With an average thrust of 445.0 N and a peak of 822.5 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the White Lightning propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
665g TotalDesign wings in your spreadsheet
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