Abstract
High speed Schlieren imaging, pressure tapping points and optical emission spectroscopy for temperature and heat flux data are essential measurement techniques for analysis of bow shock dispersion, aerodynamic performance or heat transfer of spacecraft in atmospheric re-entry. However, design and manufacturing of a high voltage pulsed-plasma jet for testing in a supersonic counterflow deserves careful examination. High voltage electrification combined with high temperature sparking between electrodes possesses several design difficulties and manufacturing challenges which need to be addressed that form the basis of the design principals and manufacturing methodology of an Apollo capsule pulsed-plasma jet for successful testing and experimentation of the model.
| Original language | English |
|---|---|
| Title of host publication | Machine Design and Manufacturing Engineering III |
| Publisher | Trans Tech Publications Ltd |
| Pages | 139-144 |
| Number of pages | 6 |
| ISBN (Print) | 9783038351801 |
| DOIs | |
| Publication status | Published - 2014 |
| Externally published | Yes |
| Event | 3rd International Conference on Machine Design and Manufacturing Engineering, ICMDME 2014 - Jeju Island, Korea, Republic of Duration: 24 May 2014 → 25 May 2014 |
Publication series
| Name | Applied Mechanics and Materials |
|---|---|
| Volume | 607 |
| ISSN (Print) | 1660-9336 |
| ISSN (Electronic) | 1662-7482 |
Conference
| Conference | 3rd International Conference on Machine Design and Manufacturing Engineering, ICMDME 2014 |
|---|---|
| Country/Territory | Korea, Republic of |
| City | Jeju Island |
| Period | 24/05/14 → 25/05/14 |
UN SDGs
This output contributes to the following UN Sustainable Development Goals (SDGs)
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SDG 9 Industry, Innovation, and Infrastructure
Keywords
- Apollo capsule
- Counterflow
- Manufacturing
- Plasma jet
- Supersonic
ASJC Scopus subject areas
- General Engineering
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