Thrust Profile (N)
2.73s Burn WindowEngineered by Loki Research, the K830-SF is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 2287.0 Ns over a 2.73 second burn window.
With an average thrust of 835.0 N and a peak of 1174.0 N, it features a progressive thrust curve optimal for general sport flying. It utilizes the Spitfire propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
2400g TotalDesign wings in your spreadsheet
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