Thrust Profile (N)
6.20s Burn WindowEngineered by AeroTech, the M1939W is a 98mm solid rocket motor designed for extreme high-power rocketry. As an official M-class motor, it delivers a total impulse of 10481.5 Ns over a 6.20 second burn window.
With an average thrust of 1939.0 N and a peak of 2429.7 N, it features a neutral thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the White Lightning propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
8988.22g TotalDesign wings in your spreadsheet
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