Thrust Profile (N)
6.83s Burn WindowEngineered by AeroTech, the J135W is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 1069.0 Ns over a 6.83 second burn window.
With an average thrust of 157.0 N and a peak of 274.0 N, it features a regressive 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
1141.06g TotalDesign wings in your spreadsheet
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