Thrust Profile (N)
1.42s Burn WindowEngineered by Cesaroni Technology, the 51F36-14A is a 29mm solid rocket motor designed for model rocketry. As an official F-class motor, it delivers a total impulse of 51.5 Ns over a 1.42 second burn window.
With an average thrust of 36.4 N and a peak of 46.3 N, it features a neutral thrust curve optimal for general sport flying. It utilizes the Blue Streak propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
101g TotalDesign wings in your spreadsheet
AeroSheet loads airfoils directly into Google Sheets. Polars, 3D splines, Fusion 360 export, without leaving your spreadsheet.
Install in Google Sheets coming soonNeed 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.