Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download An Investigation Of Leakage Of Large Diameter O Ring Seals On Spacecraft Air Lock Hatches PDF full book. Access full book title An Investigation Of Leakage Of Large Diameter O Ring Seals On Spacecraft Air Lock Hatches.
| Author | : Otto F. Trout |
| Publisher | : |
| Total Pages | : 44 |
| Release | : 1968 |
| Genre | : O-rings |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 472 |
| Release | : 1970 |
| Genre | : |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 700 |
| Release | : 1968 |
| Genre | : Mechanics, Applied |
| ISBN | : |
| Author | : United States. National Aeronautics and Space Administration Scientific and Technical Information Division |
| Publisher | : |
| Total Pages | : 472 |
| Release | : |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division |
| Publisher | : |
| Total Pages | : 470 |
| Release | : 1969 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 1498 |
| Release | : 1968 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : United States. Superintendent of Documents |
| Publisher | : |
| Total Pages | : 1504 |
| Release | : 1979 |
| Genre | : United States |
| ISBN | : |
| Author | : United States. Superintendent of Documents |
| Publisher | : |
| Total Pages | : |
| Release | : 1968 |
| Genre | : Government publications |
| ISBN | : |
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index
| Author | : Otto F. Trout (Jr.) |
| Publisher | : |
| Total Pages | : 50 |
| Release | : 1970 |
| Genre | : Space vehicles |
| ISBN | : |
A lightweight simulated spacecraft air-lock structure was tested under high vacuum to evaluate structural sealing problems and to determine leakage rates. Three different types of hatch configurations and three different seal configurations were tested for a temperature range of from -40° F (-40° C) to 200' F (930 C). Leakage rates of less than 1 x cc/sec or less than 10 (to the power of negative 4) cc/day of helium (standard temperature and pressure) were attained for each hatch.
| Author | : |
| Publisher | : |
| Total Pages | : 768 |
| Release | : 1968 |
| Genre | : Aeronautics |
| ISBN | : |
