Thrust Profile (N)
2.60s Burn WindowEngineered by AeroTech, the HP-J270W is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 703.0 Ns over a 2.60 second burn window.
With an average thrust of 270.0 N and a peak of 356.0 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the White Lightning propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
642g TotalDesign wings in your spreadsheet
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