Thrust Profile (N)
0.32s Burn WindowEngineered by AeroTech, the H999N is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 319.9 Ns over a 0.32 second burn window.
With an average thrust of 999.0 N and a peak of 1710.0 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Warp 9 propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
331g TotalDesign wings in your spreadsheet
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