Thrust Profile (N)
2.75s Burn WindowEngineered by Contrail Rockets, the J416-SP is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 1130.0 Ns over a 2.75 second burn window.
With an average thrust of 411.0 N and a peak of 1038.3 N, it features a regressive thrust curve optimal for heavy rockets requiring high off-the-pad acceleration.
Technical Specifications
Tripoli Rocketry Association, Inc.Design wings in your spreadsheet
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