COBHAM AVIATOR 200S - Compact Satellite Data Unit (CSDU)

Compact Satellite Data Unit (CSDU)
C-2 Appendix C: DO-160G specifications 98-145168-A
C.2 Compact Satellite Data Unit (CSDU)
Part Number: SDU-5045
Environmental variable
DO160 G section
(Unless otherwise specified)
Category and
requirements
Temperature and Altitude 4 [(A2F2)Z]
Ground Survival Low Temperature Test -
55°C
4.5.1 A2
Short-Time Operating Low Temperature
Test -40°C
4.5.1 A2
Operating Low Temperature Test -40°C 4.5.2 A2
Ground Survival High Temperature Test
+85°C
4.5.3 A2
Short-Time Operating High Temperature
Test +70°C
4.5.3 A2
Operating High Temperature Test +70°C 4.5.4 A2
In Flight Loss of Cooling 4.5.5 Z
Altitude Test +55.000ft 4.6.1 F2
Decompression Test 4.6.2 A2F2
Overpressure Test 4.6.3 A2
Temperature Variation (-40°C to +70°C) 5 B
Humidity 6 A
Operational Shocks and Crash Safety 7 -
Operational Shocks 7.2 E / B
Crash Safety (Impulse) 7.3.1 E / B
Crash Safety (Sustained) 7.3.3 Aircraft Type 5,
Orientation:
Random
Bench Handling Shocks MIL-STD 810G, Method
516.6, Proc. VI
MIL-STD 810G,
Method 516.6,
Proc. VI
Vibration 8 -
Standard Random Vibration 8.5 S(B3)
Table C-1: Common environmental conditions and tests (DO160G) for CSDU