Thrust Profile (N)
2.27s Burn WindowEngineered by AeroTech, the J510W is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 1162.0 Ns over a 2.27 second burn window.
With an average thrust of 509.9 N and a peak of 1041.7 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
1080g TotalDesign wings in your spreadsheet
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