Thrust Profile (N)
1.19s Burn WindowEngineered by Loki Research, the I426LB is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official I-class motor, it delivers a total impulse of 505.0 Ns over a 1.19 second burn window.
With an average thrust of 425.7 N and a peak of 718.3 N, it features a neutral thrust curve optimal for general sport flying. It utilizes the Loki Blue propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
553.1g TotalDesign wings in your spreadsheet
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