SAE ARP1625B-2013 PDF

Scope: This document has been declared ""Stabilized"" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This aerospace recommended practice covers the design, installation, tests and data requirements of stored cold gas blowdown systems or subsystems for use in guided projectiles and tactical missiles. The term system, hereafter, refers to units which function as aerodynamic surface control devices, valve actuated control devices, reaction control devices and sensing/control devices.

SAE ARP1625B-2013 Referenced Document

SAE ARP1231-1973 Gland Design@ Elastomeric O-Ring Seals@ General Considerations
SAE ARP1232 GLAND DESIGN, ELASTOMERIC O-RING SEALS, STATIC RADIAL
SAE ARP1233-1977 Gland Design@ Elastomeric O-Ring Seals@ Dynamic Radial@ 1500 psi Max
SAE AS568 Aerospace Size Standard for O-Rings

2013 SAE ARP1625B-2013 Cold Gas Systems, Missile or Projectiles Design, Installation, Tests and Requirements for
2002 SAE ARP1625A-2002 Cold Gas Systems, Missile or Projectiles Design, Installation, Tests and Requirements For
1994 SAE ARP1625-1994 COLD GAS SYSTEMS, MISSILE OR PROJECTILES DESIGN, INSTALLATION, TESTS AND REQUIREMENTS FOR
1981 SAE ARP1625A-1981 (Noncurrent)Cold Gas Systems, Missile or Projectiles Design, Installation, Tests and Requirements for Reaffirmed Noncurrent May 2002 R(1991)
1981 SAE ARP1625-1981 Cold Gas Systems@ Missile or Projectiles Design@ Installation@ Tests and Requirements for