Thrust Profile (N)
1.37s Burn WindowEngineered by AeroTech, the K1800ST-P is a 75mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 2443.7 Ns over a 1.37 second burn window.
With an average thrust of 1776.5 N and a peak of 2082.4 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Super Thunder propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
2771.5g TotalDesign wings in your spreadsheet
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