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Shuttle active thermal control system development testing. volume 5: integrated radiator/expendable cooling system tests
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Scheps, P. B. |
| Copyright Year | 1974 |
| Description | Tests were conducted to gather data on a space shuttle active control system (ATCS) incorporating both radiators and an expendable cooling device to provide vehicle heat removal. Two systems were tested and design information was provided for both nominal and limit conditions. The tests verified the concept that an integrated radiator/expendable cooling system can adequately maintain desired water quantities while responding to variations in heat loads and environments. In addition, the need for duct heating was demonstrated, while exhaust nozzle heating was also shown to be unnecessary. |
| File Size | 11901999 |
| Page Count | 415 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740026232 |
| Archival Resource Key | ark:/13960/t4vj09s25 |
| Language | English |
| Publisher Date | 1974-04-15 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Equipment Specifications Performance Tests Space Shuttles Environmental Tests Cooling Systems Systems Analysis Temperature Control Thermodynamic Properties Heat Transfer 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 |
