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PSAS Cold Gas Thruster Cross Section (22766893915) (cropped).jpg

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Summary

Description

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
Date
Source 17 PSAS Cold Gas Thruster Cross Section
Author Mach 30
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27 October 2015

0.03333333333333333333 second

4.15 millimetre

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Date/TimeThumbnailDimensionsUserComment
current17:38, 3 July 2019Thumbnail for version as of 17:38, 3 July 20191,254 × 829 (163 KB)wikimediacommons>Sense Amid Madness, Wit Amidst FollyFile:PSAS Cold Gas Thruster Cross Section (22766893915).jpg cropped 62 % horizontally, 66 % vertically using CropTool with lossless mode.

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