Thrust Profile (N)
0.56s Burn WindowEngineered by AeroTech, the HP-H550ST is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 312.0 Ns over a 0.56 second burn window.
With an average thrust of 552.0 N and a peak of 640.0 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
316g TotalDesign wings in your spreadsheet
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