Thrust Profile (N)
3.30s Burn WindowEngineered by AeroTech, the J275W is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 774.0 Ns over a 3.30 second burn window.
With an average thrust of 275.0 N and a peak of 370.0 N, it features a neutral 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
864.192g TotalDesign wings in your spreadsheet
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