Thrust Profile (N)
6.71s Burn WindowEngineered by Gorilla Rocket Motors, the O4925WC is a 152mm solid rocket motor designed for extreme high-power rocketry. As an official O-class motor, it delivers a total impulse of 33005.1 Ns over a 6.71 second burn window.
With an average thrust of 4925.0 N and a peak of 6826.9 N, it features a thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the White Cloud propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
33883g TotalDesign wings in your spreadsheet
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