Thrust Profile (N)
1.20s Burn WindowEngineered by Loki Research, the J1026CT is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 1267.0 Ns over a 1.20 second burn window.
With an average thrust of 1026.0 N and a peak of 1212.0 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Cocktail propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
1172g TotalDesign wings in your spreadsheet
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