Thrust Profile (N)
2.89s Burn WindowEngineered by AeroTech, the K456DM is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 1281.0 Ns over a 2.89 second burn window.
With an average thrust of 438.0 N and a peak of 534.0 N, it features a regressive 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
1484g TotalDesign wings in your spreadsheet
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