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: | 16 |
Downloads: | 1 |