Thrust Profile (N)
4.44s Burn WindowEngineered by Cesaroni Technology, the 234H53-12A is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 234.2 Ns over a 4.44 second burn window.
With an average thrust of 52.7 N and a peak of 101.8 N, it features a regressive thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Mellow propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
286g TotalDesign wings in your spreadsheet
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