| タイトル | A Versatile Rocket Engine Hot Gas Facility |
| 本文（外部サイト） | http://hdl.handle.net/2060/19940029625 |
| 著者（英） | Green, James M. |
| 著者所属（英） | NYMA, Inc. |
| 発行日 | 1993-06-01 |
| 言語 | eng |
| 内容記述 | The capabilities of a versatile rocket engine facility, located in the Rocket Laboratory at the NASA Lewis Research Center, are presented. The gaseous hydrogen/oxygen facility can be used for thermal shock and hot gas testing of materials and structures as well as rocket propulsion testing. Testing over a wide range of operating conditions in both fuel and oxygen rich regimes can be conducted, with cooled or uncooled test specimens. The size and location of the test cell provide the ability to conduct large amounts of testing in short time periods with rapid turnaround between programs. |
| NASA分類 | GROUND SUPPORT SYSTEMS AND FACILITIES (SPACE) |
| レポートNO | 94N34131
NASA-CR-195339
E-8900
NAS 1.26:195339
AIAA PAPER 94-2487 |
| 権利 | Copyright, Distribution under U.S. Government purpose rights |
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