Thrust Profile (N)
0.96s Burn WindowEngineered by Cesaroni Technology, the 140G145-15A is a 24mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 139.7 Ns over a 0.96 second burn window.
With an average thrust of 145.2 N and a peak of 346.9 N, it features a regressive thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the Pink propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
161.9g TotalDesign wings in your spreadsheet
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