Thrust Profile (N)
4.83s Burn WindowEngineered by AeroTech, the I132W is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official I-class motor, it delivers a total impulse of 610.7 Ns over a 4.83 second burn window.
With an average thrust of 132.0 N and a peak of 512.9 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
512.064g TotalDesign wings in your spreadsheet
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