Thrust Profile (N)
12.52s Burn WindowEngineered by Cesaroni Technology, the 4937L395-P is a 75mm solid rocket motor designed for extreme high-power rocketry. As an official L-class motor, it delivers a total impulse of 4936.8 Ns over a 12.52 second burn window.
With an average thrust of 393.7 N and a peak of 587.5 N, it features a neutral thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Mellow propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
5706g TotalDesign wings in your spreadsheet
AeroSheet loads airfoils directly into Google Sheets. Polars, 3D splines, Fusion 360 export, without leaving your spreadsheet.
BB-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.