J Class Rocket Motor

Cesaroni 699J145-19A

Cesaroni Technology
Skidmark
Ø 54mm
Total Impulse
699.1Ns
Burn Time
4.87s
Avg Thrust
143.7N
Max Thrust
505.3N

Thrust Profile (N)

4.87s Burn Window

Engineered by Cesaroni Technology, the 699J145-19A is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 699.1 Ns over a 4.87 second burn window.

With an average thrust of 143.7 N and a peak of 505.3 N, it features a regressive thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the Skidmark propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Canadian Association of Rocketry
Diameter 54 mm
Length 236 mm
Hardware Pro54-2G
Delays (s) 9,10,11,12,13,14,15,16,17,18,19
Specific Impulse 170.9 s
Peak Thrust 498.17 N
Peak Time T+ 0.018s
T/W Ratio 17.5
Propellant Skidmark
Profile regressive
Type reload
Sparky Yes

Mass Budget

837g Total
Casing (Dry)
420.0g
50.2%
Propellant
417.0g
49.8%
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...