Thrust Profile (N)
2.35s Burn WindowEngineered by AeroTech, the K1000T is a 75mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 2511.5 Ns over a 2.35 second burn window.
With an average thrust of 1066.0 N and a peak of 1674.0 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Blue Thunder propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
2602g TotalDesign wings in your spreadsheet
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