Thrust Profile (N)
3.50s Burn WindowEngineered by AeroTech, the L1365M is a 75mm solid rocket motor designed for extreme high-power rocketry. As an official L-class motor, it delivers a total impulse of 4780.0 Ns over a 3.50 second burn window.
With an average thrust of 1365.0 N and a peak of 1735.0 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Metalstorm propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
4908g 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 soonBB-75-2500
AMW
1685CC098L-L200
Hypertek
2653L585-P
Cesaroni
L695BL
Gorilla
SK-75-3500
AMW
1685CC172L-L475
Hypertek
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.