MIL-C-38418 Revision E:1981
Current
The latest, up-to-date edition.
Control Assembly, Gyroscope, Attitude A/A24G-39
30-07-1981
Important note : Users cannot be edited or removed once added to your Multi user PDF.Describes an Attitude Gyroscope Control Assembly, giving pitch, roll, and heading angular displacements.
| DevelopmentNote |
INACTIVE FOR NEW DESIGN
|
| DocumentType |
Standard
|
| Pages |
111
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
This specification covers the requirements for an Attitude Gyroscope Control Assembly, designated A/A24G-39, which provides pitch, roll, and heading angular displacements.
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