Thrust Profile (N)
1.74s Burn WindowEngineered by AeroTech, the H178DM is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 283.0 Ns over a 1.74 second burn window.
With an average thrust of 162.0 N and a peak of 202.0 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Dark Matter propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
324g TotalDesign wings in your spreadsheet
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