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  | ![]() MIL-C-64030(AR) 
3.3 Physical requirements. 
3.3.1 Envelope and dimensions.  The envelope and dimensions 
of the Control Indicator shall conform to the requirements of 
Drawing 9333036. 
3.4 Environmental conditions. 
3.4.1 Operating temperature.  When power-up, the Control 
Indicator Assembly shall activate and perform as specified in Dwg. 
9333026 over a temperature range given therein and when tested as 
specified in 3.5. 
3.4.2 Transportation vibration.  The Control Indicator shall 
show no evidence of internal or external damage that will affect 
the intended functions following Transportation Vibration Test No. 
119, Procedure 2 of MIL-STD-331. 
3.4.3 Shock.  The Control Indicator shall be subject to 
mechanical = per MIL-STD-202, Method 213B, Condition E with a 
5000 g peak and a duration of .05 ms minimum/ 2 ms maximum . 
3.5 Electronic assemblies performance characteristics. 
3.5.1 Radio frequency (RF) receiver.  This section describes 
the performance characteristics of the Radio Frequency (RF) 
Receiver, assembly no. 9333040, a subassembly of-the Control 
Indicator. 
3.5.1.1 Fast clock output.  The signal at E7 (DLACK) shall be 
a 119.5  1 % kHz square wave with a duty cycle of 50  10 %, a 
logic zero level of 0.2  0.2 volt and a logic one level of 5  
0.2 volts when tested as specified in 4.5.2.1.2. 
3.5.1.2 Crystal clock.  The signal at E5 (CLK)  shall have a 
frequency of 478 kHz  1%, a duty cycle of 67  10%, a logic zero 
level of 0.2 +0.2 volt and a logic one level of 5  0.2 volts when 
tested as specified in 4.5.2.1.3. 
3.5.1.3 MCD 
coil. 
With 5  .1 volts applied to E15 (MCD1) and 4 + 0.2 
volts to E16 (MCD2) , the outputs at E17 (L1) and E18 (L2~ shall be 
5  .3 volts and 0  0.2 volts respectively when tested as 
specified in 4.5.2.1.4. 
b.  With 5  .1 volts applied to E16 (MCD1) and 4  0.2 
volts to E15 (MCD1) , the outputs at E18 (L2) and E17 (L1) shall be 
5  .3 volts and 0  0.2 volts respectively when tested in 
4.5.2.14. 
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