Thrust Profile (N)
2.16s Burn WindowEngineered by Gorilla Rocket Motors, the K828BT is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 1786.1 Ns over a 2.16 second burn window.
With an average thrust of 828.0 N and a peak of 1301.4 N, it features a thrust curve optimal for general sport flying. It utilizes the Blue Typhoon propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
1836g TotalDesign wings in your spreadsheet
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