Thrust Profile (N)
2.45s Burn WindowEngineered by AeroTech, the H55W is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 162.3 Ns over a 2.45 second burn window.
With an average thrust of 55.0 N and a peak of 113.3 N, it features a regressive thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the White Lightning propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
188.16g TotalDesign wings in your spreadsheet
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