N Class Rocket Motor

Cesaroni 13628N5600-P

Cesaroni Technology
White Thunder
Ø 98mm
Total Impulse
13628.0Ns
Burn Time
2.42s
Avg Thrust
5636.0N
Max Thrust
6789.0N

Thrust Profile (N)

2.42s Burn Window

Engineered by Cesaroni Technology, the 13628N5600-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 13628.0 Ns over a 2.42 second burn window.

With an average thrust of 5636.0 N and a peak of 6789.0 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the White Thunder propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Canadian Association of Rocketry
Diameter 98 mm
Length 1010 mm
Hardware Pro98-6G
Delays (s) P
Specific Impulse 218.3 s
Peak Thrust 6750 N
Peak Time T+ 0.019s
T/W Ratio 50.93
Propellant White Thunder
Profile regressive
Type reload
Sparky No

Mass Budget

11280g Total
Casing (Dry)
4917.0g
43.6%
Propellant
6363.0g
56.4%
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.

Google Sheets Install in Google Sheets coming soon
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...