Thrust Profile (N)
1.80s Burn WindowEngineered by Cesaroni Technology, the 141G78-15A is a 38mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 140.9 Ns over a 1.80 second burn window.
With an average thrust of 78.4 N and a peak of 137.3 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Blue Streak propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
197g TotalDesign wings in your spreadsheet
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