Thrust Profile (N)
6.48s Burn WindowEngineered by Loki Research, the K250-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 1607.7 Ns over a 6.48 second burn window.
With an average thrust of 250.0 N and a peak of 728.3 N, it features a regressive thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the Loki White propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
1791g TotalDesign wings in your spreadsheet
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