DOD-STD-35-71A(YI)
14 January 1983
CHAR
CODE
STANDARD
PARAGRAPH
2448 THE FINAL TEST CHAMBER SHALL HAVE AN AIR VELOCITY OF
NOT LESS THAN 2448 METER(S) PER SECOND.
2450 THE DURATION AT THE FINAL TEMPERATURE SHALL BE NOT
LESS THAN 2450 MINUTE(S).
--
THE REQUIREMENT(S) SHALL BE IN
6228 TEMPERATURE, HIGH.
ACCORDANCE WITH THE BASE DOCUMENT, EXCEPT 6228.
THERE SHALL BE NO EVIDENCE OF PHYSICAL
6229
TEMPERATURE, HIGH.
DAMAGE.
2510 UNITS SHALL CONFORM TO CALIBRATION REQUIREMENTS AFTER
TEST.
THE CHANGE IN SWITCHING POINT SHALL BE NOT GREATER
2512
THAN 2512 DEGREE(S) CELSIUS.
2514 THE CHANGE IN SWITCHING POINT SHALL BE NOT GREATER
THAN 2514 DEGREE(S) FAHRENHEIT.
TESTING SHALL BE PERFORMED IN
6217 TEMPERATURE, HIGH.
ACCORDANCE WITH THE BASE DOCUMENT, EXCEPT 6217.
6218 TEMPERATURE, HIGH.
TESTING SHALL BE PERFORMED IN
ACCORDANCE WITH METHOD 501 OF MILSTD810.
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