N Class Rocket Motor

Cesaroni 14263N3400-P

Cesaroni Technology
Skidmark
Ø 98mm
Total Impulse
14263.3Ns
Burn Time
4.19s
Avg Thrust
3403.1N
Max Thrust
3741.6N

Thrust Profile (N)

4.19s Burn Window

Engineered by Cesaroni Technology, the 14263N3400-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 14263.3 Ns over a 4.19 second burn window.

With an average thrust of 3403.1 N and a peak of 3741.6 N, it features a dual-peak thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Skidmark propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Canadian Association of Rocketry
Diameter 98 mm
Length 1239 mm
Hardware Pro98-6GXL
Delays (s) P
Specific Impulse 175.6 s
Peak Thrust 3973.52 N
Peak Time T+ 2.252s
T/W Ratio 24.83
Propellant Skidmark
Profile dual-peak
Type reload
Sparky Yes

Mass Budget

13972g Total
Casing (Dry)
5690.0g
40.7%
Propellant
8282.0g
59.3%
Live Sizing
Flight Envelope

Design wings in your spreadsheet

AeroSheet loads airfoils directly into Google Sheets. Polars, 3D splines, Fusion 360 export, without leaving your spreadsheet.

Veenie Kit

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.

Loading calendar...