5000 POUND THRUST H2 F2 REGENERATIVELY COOLED ROCKET ENGINE FOR HEAT TRANSFER STUDIES - ENGINE G-14
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5000 POUND THRUST H2 F2 REGENERATIVELY COOLED ROCKET ENGINE FOR HEAT TRANSFER STUDIES - ENGINE G-14
NASA Identifier: C-1962-63081
| Date Taken: |
08.27.2009 |
| Date Posted: |
02.08.2013 10:41 |
| Photo ID: |
844847 |
| Resolution: |
2400x3000 |
| Size: |
3.25 MB |
| Location: |
WASHINGTON, D.C., US |
| Web Views: |
25 |
| Downloads: |
1 |
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