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Environmental Control for Civil Supersonic Transport
- Aerospace Standard
- AIR746C
- Stabilized
Sector:
Issuing Committee:
Language:
English
Scope
This document supplements ARP85, to extend its use in the design of ECS for supersonic transports. The ECS provides an environment controlled within specified operational limits of comfort and safety, for humans, animals, and equipment. These limits include pressure, temperature, humidity, conditioned air velocity, ventilation rate, thermal radiation, wall temperature, audible noise, vibration, and composition (ozone, contaminants, etc.) of the environment. The ECS is comprised of equipment, controls, and indicators that supply and distribute conditioned air to the occupied compartments. This system is defined within the ATA 100 specification, Chapter 21. It interfaces with the pneumatic system (Chapter 36 of ATA 100), at the inlet of the air conditioning system shutoff valves.
Rationale
This document has been determined to contain basic and stable technology which is not dynamic in nature.
Recommended Content
Aerospace Standard | Aerospace Pressurization System Design |
Aerospace Standard | Air Conditioning Systems for Subsonic Airplanes |
Topic
Data Sets - Support Documents
No Datasets Available
Issuing Committee
AC-9 Aircraft Environmental Systems Committee
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.
Reference
Number | Title |
---|---|
AIR910 | OZONE PROBLEMS IN HIGH ALTITUDE AIRCRAFT |
ARP85 | HEATING AND VENTILATING EQUIPMENT, AIRPLANE-GENERAL REQUIREMENTS FOR |
FAA-EQ-78-03 | This document is not part of the subscrption. |
FARPart25 | This document is not part of the subscrption. |
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