MIL-STD-2088B
SAE-AMS-T-9047 - Titanium and Titanium Alloy Bars (Rolled or
Forged) and Reforging Stock, Aircraft Quality
SAE-AMS-A-21180 - Aluminum Alloy Castings, High Strength SAE-AMS-A-22771 - Aluminum Alloy Forgings, Heat Treated SAE-AS50881 - Wiring, Aerospace Vehicle
SAE-AMS-H-81200 - Heat Treatment of Titanium and Titanium Alloys
(Copies of these documents are available online at https://www.sae.org or from the Society of
Automotive Engineers, 400 Commonwealth Drive, Warrendale, PA 15090.)
2.4 Order of precedence. In the event of a conflict between the text of this document and the references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained.
3. DEFINITIONS
3.1 Aircraft store. Any device intended for internal or external carriage and mounted on aircraft suspension and release equipment, whether or not the item is intended to be separated in flight from the aircraft. Aircraft stores are classified in two categories as follows:
a. Expendable store. An aircraft store normally separated from the aircraft in flight such as a missile, rocket, bomb, nuclear weapon, mine, torpedo, pyrotechnic device, sonobuoy, signal underwater sound device, cargo drop container, drone, and other similar items.
b. Non-expendable store. An aircraft store that is not normally separated from the aircraft in flight such as a tank (fuel and spray), line source disseminator, pod (refueling, thrust augmentation, gun, electronic-countermeasure, data link), multiple rack, target, and other similar items.
3.2 Bomb Rack Unit (BRU). Suspension equipment used for carrying aircraft store(s) that incorporates a method of separating the aircraft store from the aircraft at the time of commanded release.
3.3 Burst pressure. Design test pressure aimed to verify the structural integrity of the pressure system. Permanent deformation and leakage are permitted when burst pressure is applied, but no sudden ruptures or detachment of parts are allowed.
3.4. Ejections. The number of powered store releases or separations.
3.5 Flight hours. The number of hours accumulated in the airborne condition.
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