zone rev description date approved · size a cage code dwg. no. 05xq0 28130140 revision b1 scale...

SIZE

A

CAGE CODE

05XQ0 DWG. NO.

28130140 REVISION B1

SCALE N/A SHEET 1 OF 25

REVISIONS

ZONE REV DESCRIPTION DATE APPROVED

A1 ORIGINAL RELEASE 02/13/17 S.PALACIO

B1 STANDARD CLARIFICATIONS 03/01/17 S.PALACIO

PMI CONFIDENTIAL & PROPRIETARY The information contained herein is the property of Planar Monolithics

Industries. Its use or reproductions is prohibited except as provided for by prior written authorization.

Planar Monolithics Industries, Inc. 7311-F GROVE ROAD

FREDERICK, MD 21704

NAME: DATE:

QUALIFICATION TEST PROCEDURE

MODEL: P2T-7G18G-60-T-2W

PART NO: 27330140 NORTHROP GRUMMAN P/N: 567R253H01

CONTRACT NO:

DRAWN: M. Berry 03/01/17

CHECKED:

PROJ ENGR: S. Palacio 03/01/17

PROG MGR:

MFG.ENGR:

QA ENGR: J. Peacher 03/01/17

RELIABILITY:

SIZE

A

CAGE CODE

05XQ0 DWG. NO.



TABLE OF REVISIONS

DESCRIPTION DATE PMI

ORIGINAL RELEASE 02/13/17 M. BERRY

STANDARD CLARIFICATIONS 03/01/17 M. BERRY

SIZE

A

CAGE CODE

05XQ0 DWG. NO.



TABLE OF CONTENTS

1.0 SUMMARY: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 4

1.1 SCOPE: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 4

2.0 GENERAL REQUIREMENTS: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 5

2.1 TEST CONDITIONS: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 5

2.2 TEST FAILURE: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 5

3.0 ELECTRICAL TEST PROCEDURES: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 5

4.0 QUALIFICATION TEST PROCEDURES: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 5

4.1 PRE-ENVIRONMENTAL TESTING ELECTRICAL DATA, OPERATING EXTREMES: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 5

4.2 NON-OPERATING TEMPERATURE CYCLING: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 5

4.3 ALTITUDE: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 6

4.4 MECHANICAL SHOCK, NON-OPERATIONAL: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 6

4.5 VIBRATION: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 6

4.5.1 FULL PERFORMANCE VIBRATION, OPERATIONAL: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 6

4.5.2 FUNCTIONAL VIBRATION: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 6

4.5.3 ENDURANCE VIBRATION, NON-OPERATIONAL: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 6

PERFORMANCE, FUNCTIONAL & ENDURANCE VIBRATION SPECIFICATIONS: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 7

4.6 HUMIDITY: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 10

4.7 RESISTANCE TO SOLVENTS: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 10

4.8 HERMETICITY: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 10

4.9 POST-HERMETIC SEAL ELECTRICAL DATA, OPERATING EXTREMES: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 10

4.10 INTERNAL WATER VAPOR CONTENT (RGA): ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 10

4.11 MECHANICAL/MARKING/WORKMANSHIP/MARKING PERMANENCY INSPECTION: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 10

4.12 STEADY STATE LIFE TEST: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 10

4.13 POST-STEADY STATE ELECTRICAL DATA, OPERATING EXTREMES: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 10

5.0 MEAN TIME BETWEEN FAILURES INTRODUCTION: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 11

5.1 DOCUMENT PRECENDENCE: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 11

5.2 MILITARY STANDARDS: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 11

5.3 OTHER REFERENCED DOCUMENTS: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 11

6.0 EQUIPMENT DESCRIPTION AND OPERATING ENVIROMENT: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 11

6.1 EQUIPMENT DESCRIPTION: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 11

6.2 OPERATING ENVIRONMENT: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 11

6.3 STORAGE ENVIRONMENT & MAINTAINABILITY: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 11

7.0 EQUIPMENT DESCRIPTION AND OPERATING ENVIROMENT: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 12

7.1 RELIABILITY METHODOLOGY: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 12

7.2 GROUND RULES/ASSUMPTIONS: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 12

8.0 RELIABILITY REQUIREMENT: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 12

9.0 RELIABILITY PREDICTION RESULTS: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 12

9.1 MTBF CALCULATIONS: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 12

9.2 RELIABILITY PREDICTION WORKSHEETS: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 13

10.0 PART DERATING: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 13

11.0 CONCLUSIONS: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 13

12.0 LIST OF ABBREVIATIONS AND ACRONYMS: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 13

APPENDIX A – RELIABILITY PREDICTION DETAILS: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 14

APPENDIX B – OPERATING STRESS FACTOR DETAILS: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 17

APPENDIX C – PART DERATING DETAILS: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 19

APPENDIX D – ELECTRICAL DATA, OPERATING EXTREMES REPORTS x3: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 24

APPENDIX E – ENVIRONMENTAL REPORTS: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 25

APPENDIX F – INSPECTION REPORT: ∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙∙ 26

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1.0 SUMMARY Planar Monolithics Industries, Inc. (PMI) has prepared this Qualification Test Procedure Report for the Single Pole Double Throw Switch PN: P2T-7G18G-60-T-2W.

1.1 SCOPE

This report describes the Qualification Tests, Reliability Prediction, and Part Derating created for the design of the Single Pole Double Throw Switch PN: P2T-7G18G-60-T-2W. The analysis includes a part level operational stress analysis in accordance with Task 206 of MIL-STD-785B.

TEST DETAILS

& RESULTS PERFORMED BY

ESTIMATED DURATION

ELECTRICAL, OPERATING EXTREMES 4.1 PMI TBD

NON-OPERATING TEMPERATURE CYCLING 4.2 16 DAYS

ALTITUDE 4.3 2 DAYS

MECHANICAL SHOCK 4.4 2 DAYS

VIBRATION 4.5 2 DAYS

HUMIDITY 4.6 2 DAYS

HERMETIC SEAL 4.8 7 DAYS


INTERNAL WATER VAPOR CONTENT 4.10 2 DAYS

MECHANICAL 4.11

1 DAY MARKING 4.11

WORKMANSHIP 4.11

MARKING PERMANENCY 4.11

STEADY STATE LIFE TEST 4.12 42 DAYS


TOTAL 76+ DAYS

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2.0 GENERAL REQUIREMENTS Evidence supporting successful completion of in-process testing (ESS Testing) and acceptance testing shall be verified prior to formal qualification testing. The Device Under Test, or DUT, shall be closed prior to formal acceptance test to provide a tamper proof seal. At any point during testing a unit does not meet the required specifications, testing shall be manually or automatically (dependent on availability of automated setup) stopped.

2.1 TEST CONDITIONS

Unless specified otherwise, testing shall be performed at an ambient temperature of 25 °C ± 3°C and a relative humidity level not exceeding 90%. The DUT shall be conductively cooled in a manner that maintains the DUT case temperature within the specified ambient temperature window. PMI will test the DUT on a thermal platform to ensure temperature is regulated. The first unit will be characterized at the operating temperature extremes (-40 °C and +85 °C). Initial characterization to include all Section 4.0 test parameters listed on the Acceptance Test Procedure (PMI Document 28030140); the measured values may vary but will meet specifications over the operating temperature range.

2.2 TEST FAILURE

If test failure is indicated, the test program for the DUT shall be stopped by the technician. The cognizant engineering and quality representatives shall be notified. The engineering and quality representatives shall assess the failure to assign cause. A written course of action shall be developed by engineering and quality to determine the root cause of the failure.

3.0 ELECTRICAL TEST PROCEDURES All electrical testing procedure details can be found in PMI Document: 28030140.

4.0 QUALIFICATION TEST PROCEDURES – RESULTS FOUND IN APPENDIX E

4.1 PRE-ENVIRONMENTAL TESTING ELECTRICAL DATA, OPERATING EXTREMES Electrical Testing Results can be found in Appendix D.

4.2 NON-OPERATING TEMPERATURE CYCLING Temperature cycling shall be from -40°C to 95°C and back, see Figure 1 below. The temperature extremes shall be reached by all parts of the equipment and maintained within ±3°C for at least 15 minutes per cycle. Temperature rates of change shall be less than 20°C/min.

FIGURE 1: NON-OPERATING

TEMPERATURE CYCLE

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4.3 ALTITUDE Altitude testing shall be performed in accordance with MIL-STD-202, Method 105, 50,000 feet and temperature range of -30°C to +85°C (operating temperature).

4.4 MECHANICAL SHOCK, NON-OPERATIONAL The shock test shall be performed in accordance with MIL-STD-810, Method 516, Procedure I. Six (6) shocks shall be administered in each of the three (3) orthogonal axes in each direction (+ & -) (36 total) using the SRS curve specified in Figure 2.

FIGURE 2: DESIGN AND SHOCK SPECTRA

4.5 VIBRATION

4.5.1 FULL PERFORMANCE VIBRATION, OPERATIONAL

The part shall be subjected to the full performance vibration levels specified in Figure 3 in each of the three (3) orthogonal axes.

4.5.2 FUNCTIONAL VIBRATION

The part shall be subjected to the functional vibration levels specified in Figure 4 for a minimum of 30 minutes, in each of the three (3) orthogonal axes.

4.5.3 ENDURANCE VIBRATION, NON-OPERATIONAL

The part shall be subjected to the endurance vibration levels specified in Figure 5 for a minimum of 120 minutes, in each of the three (3) orthogonal axes.

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FIGURE 3: SWITCH PERFORMANCE VIBRATION

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FIGURE 4: SWITCH FUNCTIONAL VIBRATION

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FIGURE 5: SWITCH ENDURANCE VIBRATION

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4.6 HUMIDITY The humidity test shall be performed in accordance with MIL-STD-810, Method 507.5, Procedure II for 10 cycles.

4.7 RESISTANCE TO SOLVENTS

Marking permanence shall be in accordance with MIL-STD-883, Method 2105 or MIL-STD-202, Method 215.

4.8 HERMETICITY

Fine and gross leak seal tests shall be performed in accordance with MIL-STD-883, Method 1014, Conditions A & C or MIL-STD-202, Method 112, Condition C & E.

4.9 POST-HERMETIC SEAL ELECTRICAL DATA, OPERATING EXTREMES Electrical Testing Results can be found in Appendix D.

4.10 INTERNAL WATER VAPOR CONTENT (RGA) Internal water vapor shall be measured in accordance with MIL-STD-883, Method 1018.

4.11 MECHANICAL/MARKING/WORKMANSHIP/MARKING PERMENANCY INSPECTION PMI Inspection Form 1092 can be found in Appendix F. 4.12 STEADY STATE LIFE TEST

The part shall meet the full performance when tested in accordance with MIL-STD-883, Method 1005, and as follows:

a) Time: 1000 Hours

b) Temperature: Case temperature shall be such that the minimum junction temperature of all active

parts is 125°C; the burn-in temperature shall be such that the maximum junction temperature of any active part will not be exceeded. The case temperature shall be greater than the maximum operating temperature of the part (85°C).

4.13 POST-STEADY STATE ELECTRICAL DATA, OPERATING EXTREMES Electrical Testing Results can be found in Appendix D.

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5.0 MTBF INTRODUCTION The following analysis consists of the basic reliability prediction performed on the Single Pole Double Throw Switch, to establish analytically the quantitative reliability of the unit’s design.

5.1 DOCUMENT PRECEDENCE

In the event of a conflict between the contents of this report and the referenced Military Standards and Specifications, the contents of this report shall take precedence.

5.2 MILITARY STANDARDS

MIL-STD-785B Reliability Program for Systems and Equipment

Development and Production 15 SEP 1980 Revision B

MIL-HDBK-217F Reliability Prediction of Electronic Equipment (Notice 2) 10 NOV 2010

Revision F

5.3 OTHER REFERENCED DOCUMENTS

PDS36283 Requirements for Component Derating 11 SEP 2010

Revision -

6.0 EQUIPMENT DESCRIPTION AND OPERATING ENVIRONMENT

6.1 EQUIPMENT DESCRIPTION All equipment used to test the Single Pole Double Throw Switch shall be defined on the corresponding Test Report/Certificate of Compliance forms issued by the testing organization.

6.2 OPERATING ENVIRONMENT

The anticipated operating environment for the Single Pole Double Throw Switch is an Airborne, Uninhabited, Fighter (AUF) environment with a temperature range of -40°C to +85°C. The reliability prediction is performed at a part temperature of +75°C. The component derating analysis is performed at a case temperature of +85°C.

6.3 STORAGE ENVIRONMENT & MAINTAINABILITY

There are no deleterious effects from storage due to the nature of the design and the Single Pole Double Throw Switch will exceed a 20 year storage life. The features that contribute to this characteristic are the passivated semiconductor die and design for exposure to MIL-STD-202F humidity. Additionally, the service life of the Single Pole Double Throw Switch will exceed 20 years due to the high MTBF and components selected (or equivalents) are projected to be available well into the service time frame. Both storage life and service life benefit from no limited life items as part of the design and there is no need for scheduled maintenance. While in storage, the unit should remain in an Electrostatic Discharge (ESD) safe and humidity controlled environment at room temperature. The module should remain sealed in the original packaging until operation. The unit’s SMA connectors should be covered by cap lugs to prevent dust or damage while not in use. In the event of damaged connectors, the SPST has field replaceable SMA’s that may be interchanged at any time. To increase ease of testing, see PMI document number 28030140 for details. For any QA related issues or RMA requests, contact [email protected].

mailto:[email protected]

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7.0 RELIABILITY PREDICTION PROCESS

7.1 RELIABILITY METHODOLOGY

The Reliability Prediction of the Single Pole Double Throw Switch was performed, in the AUF environment using the parts count method and part failure rate models of MIL-HDBK-217F Notice 2 as augmented by vendor failure rate data. Each part type failure rate was calculated using the calculated stresses provided by engineering and a computerized Reliability Prediction Program (Windchill Quality Solutions V10.1) then was added to arrive at the unit's serial failure rate. The result of the reliability prediction Process is to obtain the equipment failure rate (λ) in failures per million hours (FPMH) and then calculate the equipment Mean Time Between Failures (MTBF) by reciprocating and converting to hours from million hours.

7.2 GROUND RULES/ASSUMPTIONS

The reliability prediction was performed under the following ground rules/assumptions:

Reliability Model: Serial Environment: AUF (Airborne, Uninhabited, Fighter) Part Temperature: 75 °C Thermal/part stresses: Capacitors: Voltage Stress

Resistors: Voltage Stress Semiconductors: Voltage Stress & Tj Rise

Quality Levels: Capacitors: Pi Q = 0.01

Resistors: Pi Q = 0.3 Diode Semiconductors: Pi Q = 0.7 PIN Diode Semiconductors: Pi Q = 0.5 FETs: Pi Q = 0.7 Microcircuits: Pi Q = 1.0

8.0 RELIABILITY REQUIREMENT The Reliability Requirement for the Mean Time Between Failure (MTBF) of the Single Pole Double Throw Switch is in excess of 1,000,000 operating hours at AUF environmental 75 °C.

9.0 RELIABILITY PREDICTION RESULTS

9.1 MTBF CALCULATIONS

Using the parts lists, calculated stress data and part temperatures for the Environmental Conditions, the MTBF was calculated and is reflected in Table 1.

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TABLE 1 – RELIABILITY PREDICTION SUMMARY

Environment Temperature Required

Failure Rate (FPMH, Max)

Required MTBF (Hours, Min)

Predicted Failure Rate

(FPMH)

Predicted MTBF (Hours)

AUF 75 °C 1.0 1,000,000 0.954938 1,047,188

9.2 RELIABILITY PREDICTION WORKSHEETS The Reliability Prediction Worksheets are contained in Appendix A. The worksheets provide the details of the part stress method reliability prediction. The operating stress factor estimates, including the estimated increase in internal component temperatures, can be found in Appendix B.

10.0 PART DERATING Internal components shall be derated in accordance with the requirements delineated in PDS36283. The derating shall be based upon a case temperature of 85°C. Results can be found in Appendix C.

11.0 CONCLUSIONS Based on the results of the parts count reliability prediction, the reliability of the Single Pole Double Throw Switch is predicted to have a MTBF of 1,047,188 hours when calculated per MIL-HDBK-217F Notice 2 in an airborne uninhabited fighter environment in a 75 °C temperature which meets the reliability requirement of 1,000,000 hours. Additionally, the component derating analysis verified compliance to the requirements delineated in PDS36283 – Requirements for Component Derating.

12.0 LIST OF ABBREVIATIONS AND ACRONYMS AUF Airborne, Uninhabited, Fighter FPMH Failures Per Million Hours MTBF Mean Time Between Failure PMI Planar Monolithics Industries QTP Qualification Test Procedure ESD Electrostatic Discharge RAM Reliability And Maintainability PCB Printed Circuit Board RF Radio Frequency

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APPENDIX A

SINGLE POLE DOUBLE THROW SWITCH RELIABILITY PREDICTION DETAILS

AUF 75 °C PART TEMPERATURE

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APPENDIX B

SINGLE POLE DOUBLE THROW SWITCH OPERATING STRESS FACTOR DETAILS


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APPENDIX C

SINGLE POLE DOUBLE THROW SWITCH PART DERATING DETAILS


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APPENDIX D

SINGLE POLE DOUBLE THROW SWITCH ELECTRICAL REPORTS, OPERATING EXTREMES x3


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APPENDIX E

SINGLE POLE DOUBLE THROW SWITCH ENVIRONMENTAL REPORTS


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APPENDIX F

SINGLE POLE DOUBLE THROW SWITCH INSPECTION REPORT


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