Thrust Profile (N)
1.91s Burn WindowEngineered by Cesaroni Technology, the 276H152-15A is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 275.9 Ns over a 1.91 second burn window.
With an average thrust of 152.4 N and a peak of 212.4 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Blue Streak propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
298g TotalDesign wings in your spreadsheet
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