Air Conditioning Systems for Subsonic Airplanes
- Aerospace Standard
A supply of outside air with independent control valve(s).
A means for heating.
A means for cooling (air or vapor cycle units and heat exchangers).
A means for removing excess moisture from the air supply.
A ventilation subsystem.
A temperature control subsystem.
A pressure control subsystem.
|Aerospace Standard||SAE Aerospace Applied Thermodynamics Manual Aerothermodynamic Systems Engineering and Design|
|Aerospace Standard||Environmental Control for Civil Supersonic Transport|
|Aerospace Standard||Aerospace Pressurization System Design|
Data Sets - Support Documents
|[Unnamed Dataset 1]|
|[Unnamed Dataset 2]|
|[Unnamed Dataset 3]|
|[Unnamed Dataset 4]|
|[Unnamed Dataset 5]|
|[Unnamed Dataset 6]|
|[Unnamed Dataset 7]|
|Table 1||Outside air requirements|
|Table 2||Airborne contaminants requirements|
|[Unnamed Dataset 10]|
|Table 3||Fuel burn penalties|
Furthers the advancement of technology related to the research, design, test and utilization of aircraft environmental and anti-icing/deicing systems. Develops and updates standards, recommended practices, and information reports contributing to the quality, economy, and safety of commercial and military aircraft.