COMBUSTION AND PERFORMANCE STUDIES OF INJECTION PROCESSES IN A 200 POUND THRUST ROCKET ENGINE LIQUID OXYGEN LOX HEPTANE SYSTEM
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COMBUSTION AND PERFORMANCE STUDIES OF INJECTION PROCESSES IN A 200 POUND THRUST ROCKET ENGINE LIQUID OXYGEN LOX HEPTANE SYSTEM
NASA Identifier: C-1955-38034
| Date Taken: |
08.27.2009 |
| Date Posted: |
02.08.2013 22:06 |
| Photo ID: |
860275 |
| Resolution: |
2100x2700 |
| Size: |
2.04 MB |
| Location: |
WASHINGTON, D.C., US |
| Web Views: |
2 |
| Downloads: |
1 |
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