Thrust Profile (N)
3.34s Burn WindowEngineered by Cesaroni Technology, the 5933M1770-P is a 75mm solid rocket motor designed for extreme high-power rocketry. As an official M-class motor, it delivers a total impulse of 5933.4 Ns over a 3.34 second burn window.
With an average thrust of 1776.8 N and a peak of 2195.2 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Skidmark propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
5993g TotalDesign wings in your spreadsheet
AeroSheet loads airfoils directly into Google Sheets. Polars, 3D splines, Fusion 360 export, without leaving your spreadsheet.
M1200-SF
Loki
2800CC300MFX-M960FX
Hypertek
2800CC200M-M740
Hypertek
M1355RT
Gorilla
M1350W
AeroTech
5198M1101-P
Cesaroni
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.