O Class Rocket Motor

Cesaroni 30600O5800-P

Cesaroni Technology
White Thunder
Ø 161mm
Total Impulse
30605.7Ns
Burn Time
5.23s
Avg Thrust
5786.6N
Max Thrust
6338.7N

Thrust Profile (N)

5.23s Burn Window

Engineered by Cesaroni Technology, the 30600O5800-P is a 161mm solid rocket motor designed for extreme high-power rocketry. As an official O-class motor, it delivers a total impulse of 30605.7 Ns over a 5.23 second burn window.

With an average thrust of 5786.6 N and a peak of 6338.7 N, it features a dual-peak thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the White Thunder propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Canadian Association of Rocketry
Diameter 161 mm
Length 754 mm
Hardware Pro150-30K
Delays (s) P
Specific Impulse 223.6 s
Peak Thrust 6395.5 N
Peak Time T+ 2.269s
T/W Ratio 22.37
Propellant White Thunder
Profile dual-peak
Type reload
Sparky No

Mass Budget

26368g Total
Casing (Dry)
12418.0g
47.1%
Propellant
13950.0g
52.9%
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...