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Standard

FABRICATION OF CARBON FIBER/POLYSULFONE RESIN COMPOSITE STRUCTURES

1994-12-01
HISTORICAL
ARP1643A
This document describes the materials, equipment, and processing techniques used in fabricating high-strength or high-modulus carbon-fiber-reinforced polysulfone laminates for structural applications for service up to 120°C (250°F).
Standard

References, Spacecraft and Spacecraft Servicing, Fluid System Components (Abbreviations, Acronyms, Definitions, Applicable Documents and Environmental Conditions)

2021-04-30
CURRENT
AIR4728A
This SAE Aerospace Information Report (AIR) presents reference information for use in preparing detailed specifications and other documents. The intent is to have a master reference document containing frequently required tabulations of information, such as the meaning of abbreviations, the spelled out wording of acronyms, the definition of terms, etc. so that such tabulations need not be repeated in recommended practice documents describing how to prepare technical documents. This document is intended to provide references in the field of fluid system components for space applications. Space applications include spacecraft, such as satellites, space stations, launch vehicles and space shuttles, and servicing equipment and components used for ground systems and launching and for servicing in space. Fluid system components include couplings, fittings, hose and tubing assemblies.
Standard

References, Spacecraft and Spacecraft Servicing, Fluid System Components (Abbreviations, Acronyms, Definitions, Applicable Documents and Environmental Conditions)

2013-01-02
HISTORICAL
AIR4728
This SAE Aerospace Information Report (AIR) presents reference information for use in preparing detailed specifications and other documents. The intent is to have a master reference document containing frequently required tabulations of information, such as the meaning of abbreviations, the spelled out wording of acronyms, the definition of terms, etc. so that such tabulations need not be repeated in recommended practice documents describing how to prepare technical documents. This document is intended to provide references in the field of fluid system components for space applications. Space applications include spacecraft, such as satellites, space stations, launch vehicles and space shuttles, and servicing equipment and components used for ground systems and launching and for servicing in space. Fluid system components include couplings, fittings, hose and tubing assemblies.
Standard

Impulse Test Equipment

1960-03-01
HISTORICAL
ARP603
This recommended practice covers design schematics of two test machines capable of producing hydraulic impulse pressure cycles with a maximum operating pressure of 5000 psi.
Standard

IMPULSE TESTING OF HYDRAULIC HOSE ASSEMBLIES, TUBING, AND FITTINGS

1977-10-01
HISTORICAL
ARP603D
This recommended practice establishes the requirements and the procedures for impulse testing of hose assemblies, tubing, and fittings for use in aerospace hydraulic systems of 4000 psi nominal operating pressure or less. It also refers to standard impulse test equipment to be used in conducting these impulse tests.
Standard

IMPULSE TESTING OF HYDRAULIC HOSE ASSEMBLIES, TUBING, AND FITTINGS

1979-08-01
HISTORICAL
ARP603E
This Aerospace Recommended Practice (ARP) establishes the requirements and the procedures for impulse testing of hose assemblies, tubing, and fittings for use in aerospace hydraulic systems of 4000 psi nominal operating pressure or less. It also refers to standard impulse test equipment to be used in conducting these impulse tests.
Standard

IMPULSE TESTING OF HYDRAULIC HOSE ASSEMBLIES, TUBING, AND FITTINGS

1975-07-15
HISTORICAL
ARP603C
This recommended practice establishes the requirements and the procedures for impulse testing of hose assemblies, tubing, and fittings for use in aerospace hydraulic systems of 3000 psi nominal operating pressure or less. It also refers to standard impulse test equipment to be used in conducting these impulse tests.
Standard

IMPULSE TESTING OF HYDRAULIC HOSE, TUBING, AND FITTING ASSEMBLIES

2007-01-17
HISTORICAL
ARP603F
This Aerospace Recommended Practice (ARP) establishes the requirements and procedures for impulse testing of hose, tubing, and fitting assemblies for use in aerospace hydraulic systems of 8000 psi nominal operating pressure or less. It also refers to standard impulse test equipment to be used in conducting these impulse tests.
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