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SAE ARP1625B

Действует
Cold Gas Systems, Missile or Projectiles Design, Installation, Tests and Requirements For (Stabilized: Jun 2013)
ОписаниеИзмененияСсылкиВерсии

Ссылочные документы

SAE ARP1231C
Действует
General Gland Design Criteria for Static and Dynamic O-Ring Seal Applications Specifically for Engines and Engine Control Systems
SAE ARP1232C
Действует
Gland Design Criteria and Dimensions for Static Radial O-Ring Seal Applications Without Anti-Extrusion Devices Specifically for Engine and Engine Control Systems
SAE ARP1233B
Действует
Gland Design Criteria and Dimensions for Dynamic Radial O-Ring Seal Applications Specifically for Engine and Engine Control Systems Operating at 1500 psi Max
SAE ARP1234E
Действует
Static Axial O-Ring Seal Applications Without Anti-Extrusion Devices for Engine and Engine Control Systems
SAE AS568F
Действует
Aerospace Size Standard for O-Rings
SAE ARP1625A
Заменен
Cold Gas Systems, Missile or Projectiles Design, Installation, Tests and Requirements For

На этот документ ссылаются

SAE ARP1625A
Заменен
Cold Gas Systems, Missile or Projectiles Design, Installation, Tests and Requirements For
SAE ARP1625
Заменен
COLD GAS SYSTEMS, MISSILE OR PROJECTILES DESIGN, INSTALLATION, TESTS AND REQUIREMENTS FOR (Noncurrent: Dec 1994)