Thrust Profile (N)
1.85s Burn WindowEngineered by Kosdon by AeroTech, the H130W is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 246.3 Ns over a 1.85 second burn window.
With an average thrust of 133.0 N and a peak of 223.2 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the White Lightning propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
709g TotalDesign wings in your spreadsheet
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