AIR795A AIR CONDITIONING OF SUBSONIC AIRCRAFT AT HIGH ALTITUDE
Canceled
03/01/1984
- Features
- Issuing Committee
- Content
- This report is limited to the special problems of air quantity, purity, movement, pressure, temperature, and humidity which arise from the requirements of the human body during high altitude flight, together with the associated aircraft design problems.
- Pages
- 9
- Citation
- SAE International Information Report, AIR CONDITIONING OF SUBSONIC AIRCRAFT AT HIGH ALTITUDE, SAE Standard AIR795A, Revised April 1975, Issued January 1963, https://doi.org/10.4271/AIR795A.