Thrust Profile (N)
7.23s Burn WindowEngineered by Cesaroni Technology, the 14272N1975-P is a 98mm solid rocket motor designed for extreme high-power rocketry. As an official N-class motor, it delivers a total impulse of 14271.6 Ns over a 7.23 second burn window.
With an average thrust of 1974.5 N and a peak of 2567.8 N, it features a dual-peak thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Green3 propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
13247.5g TotalDesign wings in your spreadsheet
AeroSheet loads airfoils directly into Google Sheets. Polars, 3D splines, Fusion 360 export, without leaving your spreadsheet.
WT-98-11000
AMW
10347N10000-P
Cesaroni
10367N1800-P
Cesaroni
GG-98-11000
AMW
N2220DM
AeroTech
N2717WC
Gorilla
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.