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SAE ARP907

1966 Edition, October 1, 1966

Complete Document

Missile & Rocket Applications: Hose Assemblies, Flexible Metal, High Pressure And High Temperature

Includes all amendments and changes through Reaffirmation Notice , January 2013


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Product Details:

  • Revision: 1966 Edition, October 1, 1966
  • Published Date: January 2013
  • Status: Active, Most Current
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 8
  • ANSI Approved: No
  • DoD Adopted: No

Description / Abstract:

This recommended practice covers the requirements and qualification tests for two tpes of flexible all-metal hose assemblies intended for hydraulic use on missile and rocket applications at rated pressures of 4000psi.

Type I -65° to +650 °F service temperature range

Type II -65° to +1000 °F service temperature range
AIA/NAS Aerospace Standards