Thrust Profile (N)
4.09s Burn WindowEngineered by AeroTech, the K560W is a 75mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 2417.0 Ns over a 4.09 second burn window.
With an average thrust of 560.0 N and a peak of 753.7 N, it features a neutral thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the White Lightning propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
2744g TotalDesign wings in your spreadsheet
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