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This program is described in detail
in section 6.0, herein. |
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Thespecimens met the requirements
of the specification without exception or deviation. |
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Loadbanks were supplied by Abbott
Electronics. |
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Thistest report represents
Independent Testing Laboratories, Inc. findings and conclusions based upon the conduct of
the test and procedures described herein with respect only to the particular
product(s) or component(s) which were provided to Independent Testing Laboratories, Inc.
by the customer for testing and evaluation proposed per written purchase orders,
procedures or verbal instructions. All findings and conclusions set forth herein are
expressly limited by and are subject to the conditions, exceptions, qualifications,
parameters, and limitations described and noted herein. Independent Testing
Laboratories, Inc. hereby expressly disclaims any responsibility of any nature or type
whatsoever with respect to the applicability of the results set forth hereing to products
or components other than the particular product(s) or component(s) which were
actually physically tested by Independent Testing Laboratories, Inc. for purposes of this
test report. |
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| 6.0 |
REQUIREMENTS,
PROCEDURES AND RESULTS |
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|
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MIL-STD-810E, Method 514.4, Proc. 1 |
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| 6.1 |
VIBRATION |
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| 6.1.1 |
PERFORMANCE CRITERIA |
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Thespecimens shall show proper output voltage during and after this
test. |
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| 6.1.2 |
TEST PROCEDURE |
|
Thetest specimens were subjected to vibration in each of the three (3)
mutually perpendicular axes (X, Y and Z) in the frequency range of 5 to 2000 Hz, one
octave per minute sweeps, 0.06" d.a. from 5 to 99 Hz, 30 G from 99 to 2000 Hz, one
(1) hour per axis. |
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| 6.1.3 |
TEST RESULTS |
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Thespecimens met the requirements of paragraph 6.1.1 above. |
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Datafor this test are presented herein in Appendix A. |
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|
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MIL-STD-810E, Method 507.3, Proc. 1 |
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| 6.2 |
HUMIDITY |
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| 6.2.1 |
PERFORMANCE CRITERIA |
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The specimens shall show proper output voltage after this test. |
| 6.2.2 |
TEST PROCEDURE |
|
The specimens were placed in a humidity chamber and tested in
accordance with Method 507.3, Procedure 1 of Reference 2.2, herein for a period of ten
(10) days.
The specimens were non-operating during the
test. |
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| 6.2.3 |
TEST RESULTS |
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The specimens met the requirements of paragraph 6.2.1 above.
Data for this test are presented herein in
Appendix A. |
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|
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MIL-STD-810E, Method 520.1, Proc. 3 |
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| 6.3 |
TEMPERATURE / ALTITUDE |
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| 6.3.1 |
PERFORMANCE CRITERIA |
|
The specimens
shall show proper output voltage during and after this test. |
|
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| 6.3.2 |
TEST PROCEDURE |
|
The specimens were subjected to Temperature / Altitude testing in
accordance with Method 520.1, Procedure 3, Figure 520-1.5 of Reference 2.2, herein for 40
hours from -55°C to 71°C, 70,000 feet.
The specimens were
operated during this test. |
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| 6.3.3 |
TEST RESULTS |
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The
specimens met the requirements of paragraph 6.3.1 above.
Datafor this test are presented herein in
Appendix A. |
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|
|
MIL-STD-810E, Method 513.4, Proc. 3 |
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| 6.4 |
ACCELERATION |
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| 6.4.1 |
PERFORMANCE CRITERIA |
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The specimens shall show proper output voltage after this test. |
|
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| 6.4.2 |
TEST PROCEDURE |
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The specimens were mounted to a flat aluminum plate and in turn
mounted to the centrifuge arm. Power was applied to the specimens. A constant acceleration
level of 14 G's was applied for a minimum of one (1) minute. The application of 14 G's for
one (1) minute was repeated in both directions of all three (3) mutually perpendicular
axes.
Thespecimens were
non-operating during the test. |
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| 6.4.3 |
TEST RESULTS |
|
The specimens met the requirements of paragraph 6.4.1 above.
Datafor this test are
presented herein in Appendix A. |
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|
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MIL-STD-810E, Method 503.3 |
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| 6.5 |
TEMPERATURE SHOCK |
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| 6.5.1 |
PERFORMANCE CRITERIA |
|
The specimens shall show proper output voltage during and after this
test. |
|
|
| 6.5.2 |
TEST PROCEDURE |
|
The specimens were subjected to Temperature Shock in accordance with
Method 503.3 of Reference 2.2, herein at -55°C to +100°C (non-operating) one (1) hour at
each extreme, 5°C per minute, three (3) cycles.
The specimens were
non-operating during this test. |
|
|
| 6.5.3 |
TEST RESULTS |
|
The specimens met the requirements of paragraph 6.5.1 above.
Data forthis test are
presented herein in Appendix A. |
|
|
|
MIL-S-901C |
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| 6.6 |
HIGH IMPACT SHOCK |
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| 6.6.1 |
PERFORMANCE CRITERIA |
|
The specimens were mounted to a flat aluminum plate and in turn mounted
to the High Impact Light Weight Shock Machine and subjected to six blows as specified in
MIL-S-901, Grade A, Class 1, Type A mounted, as follows:
The specimens were
subjected to shock impacts from hammer drop heights of one, three, and five feet in each
of three (3) directions, back, top, and bottom for a total of nine (9) impacts.
The specimens were
operated at the conclusion of the test. The voltages are listed below.
VOLTAGE AFTER SHOCK: |
|
S/N 7800019 |
14.9 Vdc |
|
|
| 6.6.3 |
TEST RESULTS |
|
The specimens met the requirements of paragraph 6.6.1 above.
Data for thistest are
presented herein in Appendix A. |
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