Thrust Profile (N)
4.80s Burn WindowEngineered by AeroTech, the M1305M is a 98mm solid rocket motor designed for extreme high-power rocketry. As an official M-class motor, it delivers a total impulse of 6891.0 Ns over a 4.80 second burn window.
With an average thrust of 1406.0 N and a peak of 2098.0 N, it features a dual-peak thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Metalstorm propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
7098g TotalDesign wings in your spreadsheet
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