Thrust Profile (N)
0.60s Burn WindowEngineered by AeroTech, the I599N is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official I-class motor, it delivers a total impulse of 404.9 Ns over a 0.60 second burn window.
With an average thrust of 667.8 N and a peak of 763.5 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Warp 9 propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
512g TotalDesign wings in your spreadsheet
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