Thrust Profile (N)
1.65s Burn WindowEngineered by AeroTech, the H130W is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 210.0 Ns over a 1.65 second burn window.
With an average thrust of 130.0 N and a peak of 260.0 N, it features a dual-peak 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
237g TotalDesign wings in your spreadsheet
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