Thrust Profile (N)
1.29s Burn WindowEngineered by Loki Research, the HP-G94-IB is a 38mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 121.0 Ns over a 1.29 second burn window.
With an average thrust of 94.0 N and a peak of 131.0 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Ice Blue propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
240g TotalDesign wings in your spreadsheet
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