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Page Title:
Table I. Major components of Guided Missile Launcher Test Set AN/ASM-464A. |
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|  MIL-G-85299(AS)
3.1.1.1 Missile simulation. The test set shall not test the SIDEWINDER
missile, but shall simulate the missile to test the capability of the aircraft
to supply required launcher inputs, and shall test the launcher capability to
supply required missile inputs. The test results shall be indicated on a
front-panel mounted GO, or NO-GO indicator.
The test set shall indicate a GO condition
3.1.1.2 Stray energy tests.
on the front panel mounted STRAY ENERGY GO indicator as long as safe limits
are not exceeded. The STRAY ENERGY NO-GO indicator lamp shall light when
stray energy is in excess of safe limits.
3.1.1,3 Test set, launcher/p ylon interface. The test set shall connect
to launcher via the igniter contact block of Cable Assembly W1. The W1P1 of
the W1 cable shall connect to the test set. The W1P2 connector interfaces
with adapter W2 for the pylon connection.
Table I lists the major components that comprise
3.1.2 Major components.
the test set.
TABLE I. Major components of Guided Missile Launcher Test Set AN/ASM-464A.
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