Thrust Profile (N)
1.27s Burn WindowEngineered by AeroTech, the H128W is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 172.9 Ns over a 1.27 second burn window.
With an average thrust of 128.0 N and a peak of 168.7 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
206g TotalDesign wings in your spreadsheet
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