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
1g TotalDesign wings in your spreadsheet
AeroSheet loads airfoils directly into Google Sheets. Polars, 3D splines, Fusion 360 export, without leaving your spreadsheet.
Need a custom engineering simulator?
The 3D engine on this page is built by Veenie Aerospace. We build bespoke, browser-native digital twins, aerodynamic simulators, and AI physics tools for UAV startups and defense contractors.