Thrust Profile (N)
0.57s Burn WindowEngineered by AeroTech, the 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 320.0 Ns over a 0.57 second burn window.
With an average thrust of 550.0 N and a peak of 667.0 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
323g TotalDesign wings in your spreadsheet
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