Thrust Profile (N)
6.00s Burn WindowEngineered by Loki Research, the M900-LR is a 76mm solid rocket motor designed for extreme high-power rocketry. As an official M-class motor, it delivers a total impulse of 5477.0 Ns over a 6.00 second burn window.
With an average thrust of 920.0 N and a peak of 1060.0 N, it features a neutral thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Loki Red propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
5530g TotalDesign wings in your spreadsheet
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