Thrust Profile (N)
2.80s Burn WindowEngineered by AeroTech, the HP-K535W is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 1434.0 Ns over a 2.80 second burn window.
With an average thrust of 535.0 N and a peak of 655.0 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
1264g TotalDesign wings in your spreadsheet
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