Thrust Profile (N)
3.90s Burn WindowEngineered by Loki Research, the K527LR is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 1983.0 Ns over a 3.90 second burn window.
With an average thrust of 526.0 N and a peak of 754.0 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Loki Red propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
1973g TotalDesign wings in your spreadsheet
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