Thrust Profile (N)
2.07s Burn WindowEngineered by Gorilla Rocket Motors, the J535BT is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 1113.8 Ns over a 2.07 second burn window.
With an average thrust of 535.0 N and a peak of 662.4 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Blue Typhoon propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
1225g TotalDesign wings in your spreadsheet
AeroSheet loads airfoils directly into Google Sheets. Polars, 3D splines, Fusion 360 export, without leaving your spreadsheet.
J245-BG
Contrail
440CC076J-J115
Hypertek
J355-BG
Contrail
683J250-15A
Cesaroni
699J145-19A
Cesaroni
J250W
AeroTech
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.