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Page Title:
Control Assembly, Gyroscope, Attitude A/A24G-39 |
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|  MIL-C-38418E(AS)
30 July 1981
SUPERSEDING
MIL-C-38418D
4 May 1970
MILITARY SPECIFICATION
CONTROL ASSEMBLY, GYROSCOPE, ATTITUDE
A/A24G-39
This specification has been approved for use
by the Naval Air Systems Command, Department
of the Navy, and is available for use by all
Departments and Agencies of the Department of
Defense.
1.
SCOPE
This specification covers the requirements for an Attitude
1.1
Gyroscope Control Assembly, designated A/A24G-39, which provides pitch,
roll, and heading angular displacements.
Classification - The equipment controlled by this specification
1.2
shall consist of the following components in accordance with 3.2.
Type Designation
Control Assembly, Gyroscope
Attitude A/A24G-39 (see 3.5)
Gyroscope, Displacement (see 3.6)
Amplifier, Electronic Control (see 3.6)
Controller, Compass System (see 3.8)
1.3
Associated Equipment - This equipment shall operate with the
associated equipment listed in 3.2.2.
FSC 6610
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