Determination of Hydraulic Pressure Drop
- Aerospace Standard
- ARP24E
- Stabilized
Scope
Rationale
Recommended Content
| Aerospace Standard | Aerospace – Military Type Variable Delivery, Pressure Compensated Hydraulic Pump |
| Aerospace Standard | Aerospace - Accumulator, Hydraulic, Cylindrical, Piston Separated |
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | Sets of Consistent Units | |
| TABLE 2 | Viscosity Conversion Factors |
Issuing Committee
A-6 Aerospace Actuation, Control and Fluid Power Systems
The committee A-6 is a service organization to promote the advancement of actuation, control and fluid power in sciences, technologies, engineering practices, and standards associated with the design, manufacture, operation, and support of aerospace vehicles. The Committee A-6 is comprised of a parent committee, subcommittees, panels, and a Steering Council. The Steering Council may from time to time create or dissolve subcommittees and panels and amend their responsibilities. The current panels include A-6A1, A-6A2, A-6A3, A-6B1, A-6B2, A-6B3, A-6C1, A-6C2, A-6C3, A-6C4 and A-6C5. The Committee A-6 is the approval body for all documents developed by its subcommittees and panels.
Reference
| Number | Title |
|---|---|
| ARP4386 | TERMINOLOGY AND DEFINITIONS FOR AEROSPACE FLUID POWER, ACTUATION, AND CONTROL TECHNOLOGIES |
| AS4395 | FITTING END - FLARED TUBE CONNECTION, DESIGN STANDARD |
| NFPA/T12.12.10 | This document is not part of the subscrption. |
| NFPA/T2.12.1 | This document is not part of the subscrption. |