MIL-STD-2088B
k. Allowable leakage rate of the pressure vessel shall be specified by the procuring activity. l. Any leakage shall not result in pressurization downstream of the pressure vessel.
FIGURE 5. Initiation circuits to activate redundant energy source control devices.
5.1.7.3.1 Pneumatic interface. The pressure vessel charging connection shall be located to enable replenishment when the vessel is installed on the pylon/BRU or aircraft, and shall be compatible with ground support equipment as specified by the procuring activity.
5.1.7.3.2 Pneumatic activated BRUs with removable energy source. A pneumatic activated BRU may be powered by a removable energy source. This vessel may directly interface to the BRU or may be at a remote location in the aircraft and interface to the BRU through appropriate plumbing.
5.1.7.4 Ejection force. Ejection force shall be applied to a store in such a manner as to provide adequate store velocity, pitch attitude, and pitch rate to ensure safe store separation from the aircraft. Unless otherwise specified by the procuring activity, the maximum ejection force applied to a store by the BRU shall be not greater than 22,500 pounds. If multiple ejector pistons are used, the maximum ejection force shall be distributed between the pistons to achieve the desired pitch control. The pressure applied on a store shall be not greater than 15,000 psi. If
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