Loading...
Please wait, while we are loading the content...
Similar Documents
Heat pipe technology for advanced rocket thrust chambers (Document No: 19720026294)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Rousar, D. C. |
| Copyright Year | 1971 |
| Description | The application of heat pipe technology to the design of rocket engine thrust chambers is discussed. Subjects presented are: (1) evaporator wick development, (2) specific heat pipe designs and test results, (3) injector design, fabrication, and cold flow testing, and (4) preliminary thrust chamber design. |
| File Size | 9913859 |
| Page Count | 224 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720026294 |
| Archival Resource Key | ark:/13960/t4jm7193m |
| Language | English |
| Publisher Date | 1971-09-15 |
| Access Restriction | Open |
| Subject Keyword | Thermodynamics And Combustion Fabrication Nozzle Design Performance Tests Heat Pipes Product Development Combustion Chambers Thermodynamic Properties Rocket Engine Design Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |