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Deep throttle turbopump technology testing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Guinzburg, A. McGlynn, R. D. Ferguson, T. V. Williams, M. |
| Copyright Year | 2002 |
| Description | The objectives of this viewgraph presentation were to: (1) enhance and demonstrate critical technologies in support of planned RBCC flight test programs; and (2) obtain knowledge of wide flow range as it is applicable to liquid rocket engine turbopumps operating over extreme throttle ranges. This program was set up to demonstrate wide flow range diffuser technologies. The testing phase of the contract to provide data to anchor initial designs was partially successful. Data collected suggest flow phenomena exists at off-design flow rates. |
| File Size | 2116554 |
| Page Count | 36 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20020052456 |
| Archival Resource Key | ark:/13960/t6935sh0d |
| Language | English |
| Publisher Date | 2002-01-01 |
| Access Restriction | Open |
| Subject Keyword | Mechanical Engineering Flight Tests Flow Velocity Turbine Pumps Liquid Propellant Rocket Engines Technology Assessment Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
