K Class Rocket Motor

Cesaroni 2285K260-P

Cesaroni Technology
Classic
Ø 54mm
Total Impulse
2285.1Ns
Burn Time
8.68s
Avg Thrust
263.3N
Max Thrust
438.1N

Thrust Profile (N)

8.68s Burn Window

Engineered by Cesaroni Technology, the 2285K260-P is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 2285.1 Ns over a 8.68 second burn window.

With an average thrust of 263.3 N and a peak of 438.1 N, it features a regressive thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Classic propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Canadian Association of Rocketry
Diameter 54 mm
Length 572 mm
Hardware Pro54-6G
Delays (s) P
Specific Impulse 202.7 s
Peak Thrust 430.41 N
Peak Time T+ 0.101s
T/W Ratio 13.11
Propellant Classic
Profile regressive
Type reload
Sparky No

Mass Budget

2047.4999999999998g Total
Casing (Dry)
898.2g
43.9%
Propellant
1149.3g
56.1%
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...