Thrust Profile (N)
3.67s Burn WindowEngineered by R.A.T.T. Works, the K600TR-P is a 64mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 2170.0 Ns over a 3.67 second burn window.
With an average thrust of 561.0 N and a peak of 1223.0 N, it features a neutral thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the Tribrid: ABS/Alcohol/Nitrous propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
14410g TotalDesign wings in your spreadsheet
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