Thrust Profile (N)
4.00s Burn WindowEngineered by AeroTech, the M1600R is a 98mm solid rocket motor designed for extreme high-power rocketry. As an official M-class motor, it delivers a total impulse of 7084.0 Ns over a 4.00 second burn window.
With an average thrust of 1600.0 N and a peak of 1917.0 N, it features a neutral thrust curve optimal for general sport flying. It utilizes the Redline propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
6917.12g TotalDesign wings in your spreadsheet
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