J Class Rocket Motor

Contrail J292-SP

Contrail Rockets
Unknown
Ø 54mm
Total Impulse
734.0Ns
Burn Time
2.53s
Avg Thrust
292.0N
Max Thrust
627.8N

Thrust Profile (N)

2.53s Burn Window

Engineered by Contrail Rockets, the J292-SP is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 734.0 Ns over a 2.53 second burn window.

With an average thrust of 292.0 N and a peak of 627.8 N, it features a regressive thrust curve optimal for heavy rockets requiring high off-the-pad acceleration.

Technical Specifications

Tripoli Rocketry Association, Inc.
Diameter 54 mm
Length 719 mm
Hardware Single Use
Delays (s) P
Specific Impulse
Peak Thrust 552.19 N
Peak Time T+ 0.008s
T/W Ratio 19.3
Propellant Standard
Profile regressive
Type hybrid
Sparky Yes
Mass Budget Unavailable
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...