Thrust Profile (N)
1.14s Burn WindowEngineered by AeroTech, the HP-H195NT is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 236.1 Ns over a 1.14 second burn window.
With an average thrust of 206.7 N and a peak of 247.2 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the New Blue Thunder propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
197g TotalDesign wings in your spreadsheet
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