Thrust Profile (N)
1.49s Burn WindowEngineered by Loki Research, the J474-CT is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 709.1 Ns over a 1.49 second burn window.
With an average thrust of 474.0 N and a peak of 1243.1 N, it features a regressive thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the Cocktail propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
755.6g TotalDesign wings in your spreadsheet
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