Thrust Profile (N)
2.97s Burn WindowEngineered by Cesaroni Technology, the 159G54-12A is a 29mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 159.1 Ns over a 2.97 second burn window.
With an average thrust of 53.6 N and a peak of 119.2 N, it features a dual-peak thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the Red Lightning propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
192.8g 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.