J Class Rocket Motor

SkyR J337B

Sky Ripper Systems
ABS/B, 830cc nitrous
Ø 54mm
Total Impulse
1073.0Ns
Burn Time
3.00s
Avg Thrust
347.0N
Max Thrust
1876.0N

Thrust Profile (N)

3.00s Burn Window

Engineered by Sky Ripper Systems, the J337B is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 1073.0 Ns over a 3.00 second burn window.

With an average thrust of 347.0 N and a peak of 1876.0 N, it features a regressive thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the ABS/B, 830cc nitrous propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Tripoli Rocketry Association, Inc.
Diameter 54 mm
Length 749 mm
Hardware 54/830
Delays (s) P
Specific Impulse 1202 s
Peak Thrust 1521.03 N
Peak Time T+ 0.01s
T/W Ratio 26.44
Propellant ABS/B, 830cc nitrous
Profile regressive
Type hybrid
Sparky No

Mass Budget

1338g Total
Casing (Dry)
1247.0g
93.2%
Propellant
91.0g
6.8%
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.

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...