 |
|||
|
|
|||
| ||||||||||
|
|  MIL-C-64030(AR)
events occur, a new cavity is substituted, an old cavity reworked,
the material/cycle time changed, a new curing time shall be
established and be approved by the Government.
Note 2: Those features of a part which are subsequently machined
or otherwised worked upon to meet its drawing requirements shall
be inspected in accordance with the classification of defects.
4.5.1 Test methods and procedures. Test methods used for
performance testing parameters described in 4.5.2 including the
radio frequency field generation technique, test vectors and test
acceleration techniques shall be approved prior to use for product
acceptance.
4.5.2 Electronic assembly performance tests. The following
subparagraphs describe the performance tests for the MOPMS Control
Indicator and its subassemblies, the Radio Frequency Receiver and
the Digital Logic Card. Unless otherwise specified, all testing
shall be performed at room ambient temperature? humidity and
atmospheric pressure.
4.5.2.1 Radio frequency receiver performance tests. This
section describes the performance test of the Radio Frequency
Receiver, assembly no. 9333040, a subassembly of the Control
Indicator.
4.5.2.1.1 Test connections. Unless otherwise specified
herein, all test connections, adjustments and manipulations
specified for a test shall be retained throughout subsequent tests.
4.5.2.1.1.1 Power source. Set the output of a O to 6 volt
100 millamp DC power supply to 0 0.1 volts. Connect the
negative terminal to E2 (GND) and E14 (BATGND). Connect the
positive terminal to E1 (VRG). Set the output voltage to 5 0.1
volts l
The initial input
4.5.2.1.1.2 Initial input connections.
connection shall be as listed below.
INPUT
CONNECTED
SIGNAL
TO
TERMINAL
NAME
5 0.2 V
-HWD
E8
0 0.2 v
E9
HWD
5 0.2 V
E11
-CLR
FCL
E7 (DLACK)
E12
open
E15
MCD1
MCD2
open
E16
87
|
|
Privacy Statement - Press Release - Copyright Information. - Contact Us |
Click
here for thousands of PDF manuals