Thrust Profile (N)
1.52s Burn WindowEngineered by Loki Research, the G80-LW is a 38mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 122.5 Ns over a 1.52 second burn window.
With an average thrust of 80.5 N and a peak of 129.4 N, it features a neutral thrust curve optimal for general sport flying. It utilizes the Loki White propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
255g 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.