Thrust Profile (N)
2.99s Burn WindowEngineered by AeroTech, the I154J is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official I-class motor, it delivers a total impulse of 378.0 Ns over a 2.99 second burn window.
With an average thrust of 154.0 N and a peak of 170.5 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Blackjack propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
491.904g TotalDesign wings in your spreadsheet
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