new icn messageflickr-free-ic3d pan white
17 PSAS Cold Gas Thruster Cross Section | by Mach 30
Back to photostream

17 PSAS Cold Gas Thruster Cross Section

3D printed cross section of a cold gas thruster chamber and nozzle. This nozzle is designed with the following parameters:

 

* Expansion Ratio = 5.4

* Chamber Pressure = 100 psi

* Operational Altitude = 15 km

 

Source STL (github.com/psas/reaction-control/blob/master/3d%20Printin...)

77 views
0 faves
0 comments
Taken on October 27, 2015