Thrust Profile (N)
3.09s Burn WindowEngineered by Gorilla Rocket Motors, the M1952BT is a 75mm solid rocket motor designed for extreme high-power rocketry. As an official M-class motor, it delivers a total impulse of 6032.0 Ns over a 3.09 second burn window.
With an average thrust of 1952.0 N and a peak of 2692.0 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Blue Typhoon propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
5443g TotalDesign wings in your spreadsheet
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