Loading...
Please wait, while we are loading the content...
Similar Documents
Structural heat pipe. [for spacecraft wall thermal insulation system
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1974 |
| Description | A combined structural reinforcing element and heat transfer member is disclosed for placement between a structural wall and an outer insulation blanket. The element comprises a heat pipe, one side of which supports the outer insulation blanket, the opposite side of which is connected to the structural wall. Heat penetrating through the outer insulation blanket directly reaches the heat pipe and is drawn off, thereby reducing thermal gradients in the structural wall. The element, due to its attachment to the structural wall, further functions as a reinforcing member. |
| File Size | 443219 |
| Page Count | 6 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750004150 |
| Archival Resource Key | ark:/13960/t7gr1pj7v |
| Language | English |
| Publisher Date | 1974-11-12 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Wall Temperature Spacecraft Structures Thermal Stability Heat Transfer Heat Pipes Thermal Insulation Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Patent |
