Thrust Profile (N)
1.50s Burn WindowEngineered by AeroTech, the HP-H115DM is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 172.0 Ns over a 1.50 second burn window.
With an average thrust of 115.0 N and a peak of 126.0 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Dark Matter propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
205g TotalDesign wings in your spreadsheet
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