Thrust Profile (N)
1.98s Burn WindowEngineered by Loki Research, the K960-LW is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 1946.5 Ns over a 1.98 second burn window.
With an average thrust of 960.0 N and a peak of 1528.6 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Loki White propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
1746g TotalDesign wings in your spreadsheet
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