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LONG-TERM STORAGE OF MISSILE HYDRAULIC SYSTEMS

A-6A Systems Subsystem Integration Steering Group
  • Aerospace Standard
  • AIR974
  • Historical
Published 1994-12-01 by SAE International in United States
Much of the available long-term storage test data has been reviewed and topically separated to enable the independent discussion of storage effects on fluids, seals, hydraulic components, and hydraulic systems. Comments are made in Section 4 concerning the applicability of the test results and regarding design practices for storability. Conclusions are drawn in Section 5 regarding inactive storage of hydraulic systems for at least a 5 year period.
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COLD GAS SYSTEMS, MISSILE OR PROJECTILES DESIGN, INSTALLATION, TESTS AND REQUIREMENTS FOR

A-6A Systems Subsystem Integration Steering Group
  • Aerospace Standard
  • ARP1625
  • Historical
Published 1994-12-01 by SAE International in United States
Systems shall be classified in terms of type, category and class.
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REDUCERS, PNEUMATIC PRESSURE, MISSILE

A-6A Systems Subsystem Integration Steering Group
  • Aerospace Standard
  • AS1297
  • Historical
Published 1994-12-01 by SAE International in United States
The complete specification for a pneumatic pressure reducer for high pressure pneumatic systems used in missiles comprises: (1) this standard, which includes many of the general performance requirements, (2) a detailed procurement specification describing envelope and operating conditions, and (3) the "Pneumatic Components, Aeronautical - General Specification For, MIL-P-8564" which covers general requirements common to all components for use in high pressure pneumatic systems.
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SEALING TECHNIQUES FOR MISSILE APPLICATIONS

A-6A Systems Subsystem Integration Steering Group
  • Aerospace Standard
  • ARP1833
  • Historical
Published 1991-11-01
No Abstract Available.
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