Thrust Profile (N)
4.44s Burn WindowEngineered by AeroTech, the L875DM is a 75mm solid rocket motor designed for extreme high-power rocketry. As an official L-class motor, it delivers a total impulse of 3887.0 Ns over a 4.44 second burn window.
With an average thrust of 875.0 N and a peak of 1355.0 N, it features a dual-peak thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Dark Matter propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
4577g TotalDesign wings in your spreadsheet
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Install in Google Sheets coming soonBB-75-2500
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