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PSAS Cold Gas Thruster Cross Section (22766893915).jpg

From Spacefaring

Original file (3,264 × 2,448 pixels, file size: 1.08 MB, MIME type: image/jpeg)

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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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Image extraction process This image has an extracted file: PSAS Cold Gas Thruster Cross Section (22766893915) (cropped).jpg.
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Licensing

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attribution
This file is licensed under the Creative Commons Attribution 2.0 Generic licence.
You are free:
  • to share – to copy, distribute and transmit the work
  • to remix – to adapt the work
Under the following conditions:
  • attribution – You must give appropriate credit, provide a link to the licence, and indicate if changes were made. You may do so in any reasonable manner, but not in any way that suggests the licensor endorses you or your use.
This image was originally posted to Flickr by Mach 30 at https://flickr.com/photos/63223655@N07/22766893915 (archive). It was reviewed on 3 July 2019 by FlickreviewR 2 and was confirmed to be licensed under the terms of the cc-by-2.0.

3 July 2019

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27 October 2015

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4.15 millimetre

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Date/TimeThumbnailDimensionsUserComment
current17:32, 3 July 2019Thumbnail for version as of 17:32, 3 July 20193,264 × 2,448 (1.08 MB)wikimediacommons>Sense Amid Madness, Wit Amidst FollyTransferred from Flickr via #flickr2commons

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