Thrust Profile (N)
0.70s Burn WindowEngineered by AeroTech, the H283ST-15A is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 201.0 Ns over a 0.70 second burn window.
With an average thrust of 283.0 N and a peak of 327.0 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Super Thunder propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
247g TotalDesign wings in your spreadsheet
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