Power Sources for Fluidic Controls
- Aerospace Standard
- AIR1245B
- Stabilized
Scope
Rationale
Recommended Content
Aerospace Standard | Aerospace Design and Installation of Commercial Transport Helicopter Hydraulic Systems |
Aerospace Standard | Hydraulic Systems, Military Aircraft, Design and Installation, Requirements For |
Aerospace Standard | Crashworthy Landing Gear Design |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
TABLE 1 | Candidate Power Sources Power Extraction From Prime Propulsion Engine(s) | |
TABLE 2 | Candidate Power Sources Power Extraction From Secondary Power Sources | |
TABLE 3 | Typical Aerospace Fluidic Control Applications and Typical Power Sources | |
TABLE 4 | Comparison of Gas Versus Liquid Fluidic Systems Factors Comparison of Gas and Fluid Fluidic Systems |
Issuing Committee
A-6A3 Flight Control and Vehicle Management Systems Cmt
The Flight Control and Vehicle Management Systems Panel is responsible for the development of standards and recommended practices related to Commercial Flight Control Systems and the Flight Control functions within Military Vehicle Management Systems (VMS). The Panel is also responsible for developing guidelines for the interface and redundancy required between the VMS and other safety critical systems. The panel provides a forum for Flight Controls and Vehicle Management System engineers, contracting agencies, prime contractors, and suppliers to exchange technical information and discuss regulatory updates, recent technology developments, lessons learned and issues related to system development and in service operation.