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A versatile rocket engine hot gas facility
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Green, James M. |
| Copyright Year | 1993 |
| Description | 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. |
| File Size | 3335596 |
| Page Count | 9 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19940029625 |
| Archival Resource Key | ark:/13960/t2799391s |
| Language | English |
| Publisher Date | 1993-06-01 |
| Access Restriction | Open |
| Subject Keyword | Ground Support Systems And Facilities (space) Ground Tests Propulsion System Performance Thermal Shock Shock Tests Research Facilities Propulsive Efficiency Rocket Engines High Temperature Gases Engine Tests Spacecraft Propulsion Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
