Thrust Profile (N)
7.75s Burn WindowEngineered by AeroTech, the J125W is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 1202.4 Ns over a 7.75 second burn window.
With an average thrust of 125.0 N and a peak of 338.9 N, it features a regressive thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the White Lightning propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
1288g TotalDesign wings in your spreadsheet
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