Thrust Profile (N)
2.98s Burn WindowEngineered by AeroTech, the K780R is a 75mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 2371.0 Ns over a 2.98 second burn window.
With an average thrust of 780.0 N and a peak of 965.0 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Redline propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
2934.4g TotalDesign wings in your spreadsheet
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