Thrust Profile (N)
1.53s Burn WindowEngineered by Loki Research, the H144-LW is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 239.3 Ns over a 1.53 second burn window.
With an average thrust of 155.0 N and a peak of 254.0 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
336g TotalDesign wings in your spreadsheet
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