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|  MIL-R-70503A(AR)
2.2 Order of precedence. In the event of a conflict between
the text of this specification and the references cited herein,
the text of this specification shall take precedence.
REQUIREMENTS
3.
3.1 Subsystem definition. The Rocket Management Subsystem
(RMS) shall provide the capability while in flight to select, set
electrical resistance-capacitance (RC) fuzes, and fire single Or
multiple 2.75 inch aerial rockets from four stations consisting of
minimum of five rocket types. Rocket quantities and firing rates
selected shall be variable. The subsystem shall provide a visual
presentation of the number of remaining rockets by type.
3.1.1 Item diagram. Figure 1 shows the general functional
relationship between the components of the RMS and between the RMS
and the helicopter.
Functional Block Diagram
Figure 1.
3
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