Thrust Profile (N)
1.24s Burn WindowEngineered by AeroTech, the HP-I500T is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official I-class motor, it delivers a total impulse of 620.0 Ns over a 1.24 second burn window.
With an average thrust of 500.0 N and a peak of 613.0 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Blue Thunder propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
576g TotalDesign wings in your spreadsheet
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