Thrust Profile (N)
0.77s Burn WindowEngineered by Quest Aerospace, the MICRO_MAXX_II is a 6mm solid rocket motor designed for model rocketry. As an official A-class motor, it delivers a total impulse of 0.2 Ns over a 0.77 second burn window.
With an average thrust of 0.3 N and a peak of 2.1 N, it features a neutral thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the black powder propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
National Association of RocketryMass Budget
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