Thrust Profile (N)
1.60s Burn WindowEngineered by Loki Research, the HP-G69-SF is a 38mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 110.0 Ns over a 1.60 second burn window.
With an average thrust of 69.0 N and a peak of 97.0 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Spitfire 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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