Thrust Profile (N)
1.93s Burn WindowEngineered by Cesaroni Technology, the 312H160-12A is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 311.7 Ns over a 1.93 second burn window.
With an average thrust of 161.5 N and a peak of 334.8 N, it features a neutral thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the Classic propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
319g TotalDesign wings in your spreadsheet
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