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This specification covers the general requirements for the design and installation of fluid anti-icing, de-greasing, and washing systems installed in military aircraft.

This specification covers the requirements for one (1) type of pocket photographic interpretation kit, containing viewing and measuring instruments, for use in the field.

The requirements contained herein are intended for those standards that are promulgated by national standards organizations and used in the aerospace industry. These technical data include narrative text, tables and various graphic data which comprise the standards. Both interface control and interface definitions are covered in this specification. The internal architectures of the computer facilities of either the providers or the users are not constrained by this interchange specification. Rather, neutral formats and transmitting media are defined in order to enable more cost-effective ways to distribute information for computer users than by sending printed documents. This method for digital delivery of aerospace standards is intended to allow the users to display and maintain standards on current computer systems in addition to producing hard copy comparable to existing printed standards.

This specification covers the requirements for disposable self-pressurized kits which utilize a propellant can pressurized with a liquified gas to atomize a product contained in a separate but attached jar (see 6.1).

This specification establishes environmental criteria for designing Aerospace Ground Equipment (AGE) in support of space systems. The test levels in this specification have been elevated to compensate for absence of combined environments during test, and to allow for variations in equipment and operating conditions. Environmental requirements are summarized in Table 1.

This specification covers the requirements for an interval timer for controlling the duration of an electrical pulse to a solenoid valve for use in Rain Repellent systems covered by Specification MIL-R-81589.

This specification established the requirements for a 5 second duration, 4500 pound thrust (when determined at 60°F) solid propellant rocket engine hereinafter specified as 5 S-4500.

This specification covers canisters for shipment and storage of lithium hydroxide (LiOH), to be used in receptacle for CO2 absorbent (see MIL-R-24159).

This specification covers pressure boundary layer control systems of turbo-jet and turbo-prop aircraft for increasing the aerodynamic lift of the wings and flaps during approach, landing, and takeoff.

This specification covers pressure boundary layer control systems of turbo-jet and turbo-prop aircraft for increasing the aerodynamic lift of the wings and flaps during approach, landing, and takeoff.