 |
|||
|
Page Title:
Battery Environmental Limitations |
|
||
| ||||||||||
|
|  MIL-N-81497A(AS)
Battery in Use - The Power Supply shall provide
3 .5.6.9
a battery in use signal simultaneously to the Computer, Navigation
and the Control, Gyroscope Assembly during periods when the supply
is operating on its internal battery.
Battery Test - Battery testing shall not be per-
3.5.6.10
formed as part of the inflight fault warning operation but shall
only be performed during the Self Test Submode upon the command of
the Computer, Navigation.
Battery Environmental Limitations - Battery
3.5.6.11
operation shall be limited to the temperature range of -20 to +55
DEG C. Maximum storage temperature shall be 71 DEG C.
The Power Supply shall
Electrical Connectors -
3.5.6.12
have the following electrical connectors.
Function
Type
Designation
Cable to: Gyroscope
MS3112E-22-55SZ
2J1
Assembly
Cable to: Computer,
MS3112E-22-55SN
2J2
Navigation
Cable to: Aircraft
MS3112E-22-55SX
2J3
Aircraft Power
MS3112-E-18-32SN
2J4
Input
Test Connector
M81511/0lE16-55S1
2J5
Color - The Power Supply shall be lusterless
3.5.6.13
gray color 36231 as specified in FED-STD-595.
Mounting - Power Supply Mounting shall be in
3.5.6.14
accordance with MS91403.
Rack , Electrical Equipment MT-3947\ASN-84 - The
3.5.7
Rack, Electrical Equipment shall meet the following requirements.
Function - The Rack, Electrical Equipment shall
3.5.7.1
provide the mechanical interface between the Gyroscope Assembly and
the airframe.
It shall provide the capability of not requiring an
optical realignment of the Gyroscope Assembly after a removal and
replacement in the aircraft.
51
|
|
Privacy Statement - Press Release - Copyright Information. - Contact Us |
Click
here for thousands of PDF manuals