Thrust Profile (N)
2.23s Burn WindowEngineered by Cesaroni Technology, the 134G60-14A is a 38mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 134.2 Ns over a 2.23 second burn window.
With an average thrust of 60.3 N and a peak of 87.8 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Red Lightning propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
206g 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.