200819219 Rev C Controller Spec.pdf

Refine OS and external keyboard reqs.

CONFIGURATION ITEM PRODUCT FUNCTION

SPECIFICATIONS

FOR THE

GM-LTS PRIMARY COMPUTER

(15090) 3156170 AN/GSM-396 (D,E,F,G,H)

DWN R. M. KELLOGG DATE 02/20/2020

CHK D. L. EMERY DATE 02/20/2020

DWG NO: 200819219

APPLICATION

NEXT ASSY USED ON

DESTRUCTION NOTICE. FOR UNCLASSIFIED, LIMITED

DOCUMENTS, DESTROY BY ANY METHOD THAT WILL

PREVENT DISCLOSURE OF CONTENTS OR

RECONSTRUCTION OF THE DOCUMENTS.

DISTRIBUTION STATEMENT C: DISTRIBUTION

AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND

THEIR CONTRACTORS DUE TO ADMINISTRATIVE OR

OPERATIONAL PURPOSES, DETERMINED ON 19 OCTOBER

2016. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE

REFERRED TO AFLCMC/EBREM, ROBINS AFB, GA.

REVISIONS

REV STATUS OF ALL SHEETS IS: (Rev B)

REV

CONTR GS06K97BND0453

ENGR R. M. KELLOGG DATE 02/20/2020

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CONFIGURATION ITEM PRODUCT FUNCTION

SPECIFICATION, GM-LTS, PRIMARY COMPUTER

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TABLE OF CONTENTS

1. SCOPE

1.1 SPECIFICATION DEFINITION

1.2 CLASSIFICATION

2. APPLICABLE DOCUMENTS

2.1 GOVERNMENT DOCUMENTS

2.2 NON-GOVERNMENT DOCUMENTS

3. REQUIREMENTS

3.1 CRITICAL ITEM DEFINITION

3.1.1 HARDWARE CONFIGURATION

3.1.1.1 PROCESSOR

3.1.1.2 RAM

3.1.1.3 HARD DRIVE

3.1.1.4 INTERFACE EXPANSION BUS

3.1.1.5 PARALLEL PORT

3.1.1.6 SERIAL PORT

3.1.1.7 1553 PORT

3.1.1.8 NETWORK INTERFACE

3.1.1.9 REMOVED

3.1.1.10 UNIVERSAL SERIAL BUS (USB)

3.1.1.11 HEATER PLATES

3.1.1.12 KEYBOARD

3.1.1.13 EXTERNAL KEYBOARD SUPPORT

3.1.1.14 GRAPHICS ADAPTER AND DISPLAY

3.1.1.15 EXTERNAL MONITOR SUPPORT

3.1.1.16 COMPACT DISC READ/WRITE

3.1.1.17 SOFTWARE CONFIGURATION (BIOS)

3.1.1.18 BIOS CMOS MEMORY BACKUP BATTERY

3.1.1.19 SPEAKER

3.1.1.20 EXTERNAL DC POWER SUPPLY

3.2 CHARACTERISTICS

3.2.1 PERFORMANCE

3.2.1.1 SOFTWARE PERFORMANCE

3.2.1.1.1 USER MODIFIABLE BIOS SETTINGS AND DEFAULTS

3.2.1.1.1.1 BOOT ORDER PRIORITY

3.2.1.1.1.2 I/O DEVICE CONFIGURATION

3.2.1.1.1.3 REMOVED

3.2.1.1.1.4 PCI/PNP ISA IRQ RESOURCE EXCLUSION

3.2.1.1.1.5 CUSTOM DRIVES

3.2.1.1.1.6 DISKETTES

3.2.1.1.2 NON-VOLATILE MEMORY

3.2.1.1.3 OPERATING SYSTEM

3.2.1.1.4 APPLICATION SOFTWARE

3.2.1.2 SELF-TEST

3.2.1.3 HARDWARE PERFORMANCE

3.2.1.3.1 POWER

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3.2.1.3.1.1 EXTERNAL POWER SOURCES

3.2.1.3.1.2 PRIMARY COMPUTER POWER UP/POWER DOWN REQUIREMENTS

3.2.1.3.1.3 HEATER INPUT POWER REQUIRMENTS

3.2.1.3.1.4 PRIMARY COMPUTER POWER PASSTHROUGH REQUIREMENTS

3.2.1.3.2 EXPANSION BUS PERFORMANCE

3.2.1.3.3 PARALLEL PORT PERFORMANCE

3.2.1.3.4 SERIAL PORT PERFORMANCE

3.2.1.3.5 1553 PORT PERFORMANCE

3.2.1.3.6 NETWORK INTERFACE

3.2.1.3.7 EXTERNAL KEYBOARD PERFORMANCE

3.2.1.3.8 EXTERNAL VGA PORT PERFORMANCE

3.2.1.3.9 REMOVED

3.2.1.3.10 UNIVERSAL SERIAL BUS (USB)

3.2.1.3.11 COMPACT DISK READ/WRITE (CD R/W)

3.2.1.3.12 POWER-ON TIME

3.2.1.3.13 DISPLAY PERFORMANCE

3.2.2 PHYSICAL CHARACTERISTICS

3.2.2.1 DIMENSIONS

3.2.2.2 WEIGHT

3.2.2.3 FINISH

3.2.2.4 HANDLES

3.2.2.5 RUBBER FEET

3.2.2.6 CHASSIS

3.2.2.7 KEYBOARD

3.2.2.8 DISPLAY

3.2.2.9 CONNECTORS

3.2.2.9.1 POWER I/0 CONNECTOR (J4)

3.2.2.9.2 1553B PORT CONNECTOR (J1)

3.2.2.9.3 PARALLEL INTERFACE CONNECTOR (J5)

3.2.2.9.4 SERIAL INTERFACE CONNECTOR (J3)

3.2.2.9.5 REMOVED

3.2.2.9.6 EXTERNAL DISPLAY CONNECTOR

3.2.2.9.7 UNIVERSAL SERIAL BUS

3.2.2.9.8 NETWORK BUS

3.2.2.10 PLACEMENT OF ENVIRONMENTALLY PROTECTED CONNECTORS

3.2.2.11 PROTECTION OF COMMERCIAL INTERFACES

3.2.2.12 MOUNTING OF CONTROLLER TO GMLTS IAU

3.2.2.13 REPLACEMENT OF BIOS CMOS MEMORY BACKUP BATTERY

3.2.3 RELIABILITY

3.2.3.1 OPERATING RELIABILITY

3.2.4 MAINTAINABILITY

3.2.5 ENVIRONMENTAL CONDITIONS

3.2.6 TRANSPORTABILITY

3.3 DESIGN AND CONSTRUCTION

3.3.1 MATERIALS, PROCESSES, AND PARTS

3.3.1.1 PROCESSES

3.3.2 ELECTROMAGNETIC RADIATION

3.3.2.1 EMC TEST CONFIGURATION

3.3.3 IDENTIFICATION AND MARKING

3.3.3.1 ELECTRICAL WARNING MARKINGS

3.3.4 WORKMANSHIP

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3.3.5 INTERCHANGEABILITY

3.3.6 SAFETY

3.3.6.1 OPERATOR SAFETY

3.3.6.1.1 OPERATION

3.3.6.1.2 MAINTENANCE

3.3.6.1.3 OPEN CIRCUIT VOLTAGE PROTECTION

3.3.6.1.4 LEAKAGE CURRENT PROTECTION

3.3.7 HUMAN PERFORMANCE/HUMAN ENGINEERING

3.3.8 DOCUMENTATION

3.4 QUALIFICATION

3.4.1 LOCATION

3.4.2 SCHEDULE FOR TESTING

4. QUALITY ASSURANCE PROVISIONS

4.1 GENERAL

4.1.1 RESPONSIBILITY FOR INSPECTION

4.1.1.1 QUALITY ASSURANCE TERMS AND DEFINITIONS

4.1.1.2 TEST EQUIPMENT

4.1.1.3 TEST CONDITIONS

4.1.1.4 MEASUREMENT OF TEST CONDITIONS

4.1.1.5 TOLERANCE OF TEST CONDITIONS

4.1.1.6 ACCURACY OF TEST INSTRUMENT CALIBRATION

4.1.2 SPECIAL TESTS AND EXAMINATIONS

4.1.3 PRODUCTION TESTS

4.1.3.1 ACCEPTANCE TEST

4.1.3.2 BURN-IN/VIBRATION ESS

4.2 QUALITY CONFORMATION INSPECTIONS

4.2.1 PREPRODUCTION

4.2.2 QUALIFICATION

5. PREPARATION FOR DELIVERY

5.1 GENERAL

5.2 SPECIFIC REQUIREMENTS

5.3 SHIPPING INFORMATION

6. NOTES

6.1 ORDERING DATA

6.2 DEFINITIONS

6.2.1 ABBREVIATIONS AND ACRONYMS

6.2.2 TERMS

6.2.2.1 ANALYSIS

6.2.2.2 BIT

6.2.2.3 CONFIGURATION

6.2.2.4 DEMONSTRATION

6.2.2.5 DETAIL SPECIFICATION

6.2.2.6 DIMENSIONS

6.2.2.7 FAILURE

6.2.2.8 INSPECTION

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6.2.2.9 INTERMITTENT AND SHORT-TIME OPERATION

6.2.2.10 PC-104

6.2.2.11 PERFORMANCE REQUIREMENTS OF THE TEST EQUIPMENT

6.2.2.12 PROCURING ACTIVITY

6.2.2.13 RUGGEDIZED

6.2.2.14 SELF-TEST

6.2.2.15 TEST

6.2.2.16 WARM-UP TIME

TABLES

TABLE I: ”+VDC OPERATE” INPUT POWER & 28VDC PASSTHROUGH TO J-2

TABLE II: ”+VDC HEATER” POWER REQUIREMENTS & 28VDC PASSTHROUGH TO J-2

TABLE III: PRIMARY COMPUTER ENVIRONMENTAL REQUIREMENTS

TABLE IV: PRIMARY COMPUTER ELECTROMAGNETIC COMPATIBILITY SPECIFICATIONS

TABLE V: REQUIREMENTS FOR QUALIFICATION TESTING

TABLE VI: REQUIRED COMPONENTS OF ACCEPTANCE TEST

TABLE VII: CONFORMANCE VERIFICATION MATRIX

FIGURES

FIGURE 1: LOCATION OF ENVIRONMENTALLY SEALED CONNECTORS

APPENDICES

10. 1 PIN-OUT FOR J1 CONNECTOR

10. 2 PIN-OUT FOR J3 CONNECTOR

10. 3 PIN-OUT FOR J4 CONNECTOR

10. 4 PIN-OUT FOR J5 CONNECTOR

10. 5 REMOVED

10. 6 PIN-OUT FOR EXTERNAL VGA CONNECTOR

10. 7 PIN OUT FOR UNIVERSAL SERIAL BUS

10. 8 PIN OUT FOR NETWORK INTERFACE

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1. SCOPE.

1.1 SPECIFICATION DEFINITION

THIS SPECIFICATION ESTABLISHES THE PERFORMANCE, DESIGN, TEST, MANUFACTURE,

AND ACCEPTANCE REQUIREMENTS FOR THE CRITICAL ITEM HEREAFTER REFERRED TO

AS THE PRIMARY COMPUTER.

1.2 CLASSIFICATION.

THE PRIMARY-COMPUTER SHALL MEET THE REQUIREMENTS SET FORTH IN

MIL-PRF-28800F FOR CLASS 2 TEST EQUIPMENT, UNLESS SUPERSEDED BY THIS

DOCUMENT

2. APPLICABLE DOCUMENTS.

2.1 GOVERNMENT DOCUMENTS.

THE FOLLOWING DOCUMENTS OF THE EXACT ISSUE SHOWN FORM A PART OF THIS

SPECIFICATION TO THE EXTENT SPECIFIED HEREIN. IN THE EVENT OF CONFLICT

BETWEEN THE DOCUMENTS REFERENCED HEREIN AND THE CONTENTS OF THIS

SPECIFICATION, THE CONTENTS OF THIS SPECIFICATION SHALL BE CONSIDERED A

SUPERSEDING REQUIREMENT.

SPECIFICATIONS:

PERFORMANCE SPECIFICATION:

MIL-PRF-28800F TEST EQUIPMENT USE WITH ELECTRICAL AND

24 JUN 96 ELECTRONIC EQUIPMENT, GENERAL SPECIFICATION FOR

STANDARDS/HANDBOOKS:

MILITARY

MIL-STD-461E REQUIREMENTS FOR CONTROL OF ELECTROMAGNETIC

20 AUGUST 99 INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND

EQUIPMENT

MIL-STD-130K IDENTIFICATION MARKING OF U.S.

15 JAN 00 MILITARY PROPERTY

MIL-HDBK-454A GENERAL GUIDELINES FOR

02 NOV 00 ELECTRONIC EQUIPMENT

MIL-STD-810E ENVIRONMENTAL ENGINEERING CONSIDERATIONS

14 JULY 89 AND LABORATORY TESTING

MIL-STD-882D STANDARD PRACTICE FOR SYSTEM SAFETY

10 FEBRUARY 00

MIL-STD-1275B CHARACTERISTICS OF 28-VOLT DC ELECTRICAL

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20 NOV 97 SYSTEMS IN MILITARY VEHICLES

MIL-STD-1472F HUMAN ENGINEERING

23 AUG 99

MIL-STD-1553B DIGITAL TIME DIVISION

15 JAN 96 COMMAND/RESPONSE MULTIPLEX DATA BUS

MIL-HDBK-217F RELIABILITY PREDICTION OF ELECTRONIC EQUIPMENT

28 FEB 95

2.2 NON-GOVERNMENT DOCUMENTS.

THE FOLLOWING DOCUMENTS OF THE EXACT ISSUE SHOWN FORM A PART OF THIS

SPECIFICATION TO THE EXTENT SHOWN HEREIN. UNLESS OTHERWISE INDICATED THE

ISSUE IN EFFECT ON DATE OF INVITATION FOR BIDS OR REQUEST FOR PROPOSAL SHALL

APPLY.

ASQC- A8402-1 QUALITY MANAGEMENT AND QUALITY ASSURANCE

1994 VOCABULARY

ISO-10012-1-97 QUALITY ASSURANCE REQUIREMENTS FOR MEASURING

01 JUN 97 EQUIPMENT

ISO-10012-2-98 PART 2: GUIDELINES FOR CONTROL OF MEASUREMENT

01 SEP 98 PROCESSES

EIA-RS-232C INTERFACE BETWEEN DATA TERMINAL EQUIPMENT AND

DATA COMMUNICATION EQUIPMENT EMPLOYING BINARY

DATA INTERCHANGE IEEE-P996.1, STANDARD FOR

COMPACT EMBEDDED PC MODULES

3. REQUIREMENTS.

3.1 CRITICAL ITEM DEFINITION.

THE PRIME ITEM SHALL BE A RUGGEDIZED, IBM AT COMPATIBLE, COMPACT COMPUTER

SUITABLE FOR CONTROLLING AND MONITORING FIELD TEST EQUIPMENT UNDER

ADVERSE ENVIRONMENTAL CONDITIONS. THE PRIMARY COMPUTER SHALL BE

PORTABLE, LIGHT-WEIGHT, OPERATOR-FRIENDLY, AND CAPABLE OF MEETING THE

PHYSICAL AND OPERATIONAL REQUIREMENTS SPECIFIED IN THE SECTIONS HEREIN AT A

MINIMUM.

3.1.1 HARDWARE CONFIGURATION.

THE MINIMUM HARDWARE SHALL BE AS SPECIFIED HEREIN.

3.1.1.1 PROCESSOR.

THE PRIMARY COMPUTER SHALL BE BASED AROUND AN X86 CLASS MICROPROCESSOR

CAPABLE OF OPERATING AT A CLOCK RATE OF AT LEAST 500 MEGA-HERTZ (MHz).

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3.1.1.2 RAM.

THE PRIMARY COMPUTER SHALL BE CONFIGURED WITH 512 MEGA-BYTES (MB) OF RAM,

WITH EXPANSION CAPABILITY TO AT LEAST 1024 MB.

3.1.1.3 HARD DRIVE.

THE PRIMARY COMPUTER SHALL CONTAIN A USER REMOVABLE INTERNAL HARD DRIVE

WITH A MINIMUM OF 20 GIGABYTES CAPACITY.

3.1.1.4 INTERFACE EXPANSION BUS.

THE COMPUTER SHALL CONTAIN AT LEAST ONE INDUSTRY STANDARD EXPANSION SLOT

TO BE COMPATIBLE WITH DEFINED 1553 EXPANSION CARD.

3.1.1.5 PARALLEL PORT.

THE PRIMARY COMPUTER SHALL CONTAIN ONE INDUSTRY STANDARD PARALLEL

PRINTER PORT. ADDITIONAL REQUIREMENTS FOR THIS PORT ARE DEFINED IN SECTION

3.2.1.3.3.

3.1.1.6 SERIAL PORT.

THE PRIMARY COMPUTER SHALL CONTAIN TWO SERIAL PORTS THAT CONFORM TO THE

EIA-RS-232C INTERFACE STANDARD.

3.1.1.7 1553 PORT.

THE PRIMARY COMPUTER SHALL CONTAIN ONE DUAL REDUNDANT 1553 INTERFACE

CONFORMING TO THE REQUIREMENTS OF MIL-STD-1553B.

3.1.1.8 NETWORK INTERFACE.

THE PRIMARY COMPUTER SHALL CONTAIN ONE 10/100 NETWORK INTERFACE PORT

CONFORMING TO INDUSTRY STANDARDS.

3.1.1.9 REMOVED.

3.1.1.10 UNIVERSAL SERIAL BUS (USB)

THE PRIMARY COMPUTER SHALL CONTAIN ONE USB PORT CONFORMING TO INDUSTRY

STANDARDS.

3.1.1.11 HEATER PLATES.

HEATING ELEMENTS MAY BE INSTALLED INTERNAL TO THE COMPUTER IF REQUIRED TO

ALLOW THE UNIT TO OPERATE ACROSS THE SPECIFIED TEMPERATURE OPERATING

RANGE.

3.1.1.12 KEYBOARD.

THE KEYBOARD SHALL BE A UNITED STATES LAYOUT FULL 87 KEY QWERTY

ELASTOMER KEYBOARD WITH SEPARATE FUNCTION, ALPHA, AND NUMERIC KEYS.

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3.1.1.13 EXTERNAL KEYBOARD SUPPORT.

THE PRIMARY. COMPUTER SHALL BE CAPABLE OF SUPPORTING AN OPTIONAL INDUSTRY

STANDARD 101-KEY KEYBOARD WHEN THE COMPUTER IS UTILIZED IN A LABORATORY

ENVIRONMENT.

3.1.1.14 GRAPHICS ADAPTER AND DISPLAY.

THE GRAPHICS ADAPTER AND DISPLAY, SHALL AT A MINIMUM, BE A SUPER VIDEO

GRAPHICS ADAPTER (SVGA) SUPPORTING A RESOLUTION OF 800 X 600. THE GRAPHICS

ADAPTER SHALL HAVE A MINIMUM OF 4MBYTE OF VIDEO RAM. THE DISPLAY SHALL BE

A HIGH-CONTRAST, ACTIVE MATRIX TFT COLOR DISPLAY DEVICE, WITH A BACKLIGHT

TO AID VISION DURING LOW-LIGHT OPERATION.

3.1.1.15 EXTERNAL MONITOR SUPPORT.

THE PRIMARY COMPUTER SHALL BE CAPABLE OF SUPPORTING AN OPTIONAL EXTERNAL

SVGA COLOR MONITOR WHEN THE COMPUTER IS UTILIZED IN A LABORATORY

3.1.1.16 COMPACT DISC READ/WRITE.

THE PRIMARY COMPUTER SHALL CONTAIN AN INTERNAL COMPACT DISC READ/WRITE

DRIVE (CD R/W).

3.1.1.17 SOFTWARE CONFIGURATION (BIOS).

THE BASIC INPUT/OUTPUT SYSTEM (BIOS) SHALL BE INSTALLED IN THE PRIMARY

COMPUTER AS A PART OF THE DELIVERABLE CONFIGURATION. THE MANUFACTURER

SHALL PROVIDE THE OPERATING SYSTEM AND NECESSARY UTILITIES AS A PART OF THE

PRIMARY COMPUTER'S DELIVERABLE CONFIGURATION.

3.1.1.18 BIOS CMOS MEMORY BACKUP BATTERY.

THE PRIMARY COMPUTER SHALL CONTAIN A USER REPLACEABLE BATTERY BACKUP

FOR THE BIOS CMOS MEMORY .

3.1.1.19 SPEAKER.

THE PRIMARY COMPUTER SHALL CONTAIN AN EXTERNALLY AUDIBLE SPEAKER.

3.1.1.20 EXTERNAL DC POWER SUPPLY.

AN EXTERNAL DC POWER SUPPLY, CAPABLE OF OPERATING THE PRIMARY COMPUTER

SHALL BE DELIVERED WITH EACH PRIMARY COMPUTER.

3.2 CHARACTERISTICS.

THE CHARACTERISTICS OF THE PRIMARY COMPUTER ARE DEFINED BELOW.

3.2.1 PERFORMANCE.

SOFTWARE AND HARDWARE CHARACTERISTICS ARE SPECIFIED IN THE SECTIONS

BELOW.

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3.2.1.1 SOFTWARE PERFORMANCE.

THIS SECTION SPECIFIES THE PERFORMANCE REQUIREMENTS OF THE BIOS,

MANUFACTURER-SUPPLIED SOFTWARE AS WELL AS USER-DEVELOPED APPLICATIONS.

3.2.1.1.1 USER MODIFIABLE BIOS SETTINGS AND DEFAULTS

THE BIOS SHALL PROVIDE THE CAPABILITY FOR THE USER TO MODIFY ALL NECESSARY

SETTINGS. THE BIOS SETTINGS SHALL POWER UP TO A PREDEFINED DEFAULT STATE

WHEN MANUALLY RESET OR THE CMOS BACKUP BATTERY IS CHANGED.

FOLLOWING (AS A MINIMUM), ARE A LIST OF NECESSARY USER MODIFIABLE SETTINGS

AND DEFAULT STATES;

3.2.1.1.1.1 BOOT ORDER PRIORITY.

THE BIOS SHALL CONTAIN A USER MODIFIABLE BOOT ORDER PRIORITY THAT HAS A

MINIMUM OF THREE SELECTABLE DEVICE FIELDS. FIELD 1 SHALL BE DESIGNATED AS

THE FIRST DEVICE ATTEMPTED TO BOOT FROM.

THE FIRST TWO DEVICES OF THE DEFAULT BOOT ORDER PRIORITY FIELDS SHALL BE AS

FOLLOW;

1. CDRW

2. HARD DRIVE

3.2.1.1.1.2 I/O DEVICE CONFIGURATION.

THE BIOS SHALL BE CAPABLE OF ALLOWING THE USER TO MODIFY ALL NECESSARY

PARAMETERS OF THE I/O DEVICES.

THE BIOS SHALL SET THE DEFAULT STATE OF THE I/O DEVICES AS FOLLOWS;

SERIAL PORT A (COM1): ENABLED; IRQ4; 3F8

SERIAL PORT B (COM2): ENABLED; IRQ3; 2F8; MODE: NORMAL

PARALLEL PORT(LPT1): ENABLED; IRQ5; 378; BI-DIRECTIONAL

USB: DISABLED

NETWORK INTERFACE: DISABLED

THE BIOS SHALL ALLOW THE USB AND NETWORK INTERFACE TO BE ENABLED OR

DISABLED;

3.2.1.1.1.3 REMOVED.

3.2.1.1.1.4 REMOVED

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3.2.1.1.1.5 CUSTOM DRIVES

THE DEFAULT BIOS SETTING SHALL DISABLE ALL CUSTOM DRIVES.

3.2.1.1.1.6 DISKETTES

THE DEFAULT BIOS SETTING SHALL DISABLE DISKETTES.

3.2.1.1.2 NON-VOLATILE MEMORY.

OTHER THAN THE BIOS, THE PRIMARY COMPUTER SHALL NOT CONTAIN ANY INTERNAL

NON-VOLATILE MEMORY THAT CAN BE ACCESSED BY THE OPERATING SYSTEM.

3.2.1.1.3 OPERATING SYSTEM.

THE PRIMARY COMPUTER SHALL BE CAPABLE OF OPERATING WITH THE WINDOWS 10

OPERATING SYSTEM.

3.2.1.1.4 APPLICATION SOFTWARE.

THE UNIT SHALL BE CAPABLE OF EXECUTING APPLICATION SOFTWARE PROGRAMS

DEVELOPED FOR THE X86 FAMILY OF MICROPROCESSORS IN THE WINDOWS

3.2.1.2 SELF-TEST.

THE COMPUTER SHALL HAVE SELF-TEST CAPABILITY TO RUN BASIC DIAGNOSTICS. THE

SELF-TEST SHALL BE EXECUTED ON POWER UP AND RESET. ERROR MESSAGES AND

FAILURE CODES SHALL BE GENERATED AND MADE ACCESSIBLE TO BE DISPLAYED TO

OPERATOR FOR ASSIST IN TROUBLESHOOTING THE PRIMARY COMPUTER. THE MINIMUM

COMPONENTS OF THE PRIMARY COMPUTER SELF-TEST ARE AS FOLLOWS:

CENTRAL PROCESSING UNIT CHECK RAM CHECK

INPUT/OUTPUT CHECK

VIDEO CHECK

3.2.1.3 HARDWARE PERFORMANCE.

THE PRIMARY COMPUTER SHALL BE IN ACCORDANCE WITH THE PERFORMANCE

CHARACTERISTICS LISTED IN 3.2.1.3.1 THROUGH 3.2.1.3.12.

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3.2.1.3.1 POWER.

THE PRIMARY COMPUTER SHALL BE CAPABLE OF OPERATING FROM AN EXTERNAL DC

POWER SOURCE(S) APPLIED TO THE J4 CONNECTOR AS DEFINED IN THE FOLLOWING

PARAGRAPHS.

IN ADDITION, THE PRIMARY COMPUTER SHALL ROUTE THE APPLIED INPUT POWER AT

THE J4 CONNECTOR TO THE J5 CONNECTOR TO SUPPLY POWER FOR OTHER ASSEMBLIES.

3.2.1.3.1.1 EXTERNAL POWER SOURCES.

THE EXTERNAL POWER SOURCE(S) APPLIED TO THE J4 CONNECTOR SHALL ORIGINATE

FROM EITHER THE GMLTS IAU OR AN EXTERNAL 60HZ TO DC POWER SUPPLY.

(REFERENCE APPENDIX I, J4 PINOUTS).

3.2.1.3.1.1.1 GMLTS IAU POWER SOURCE.

UNDER NORMAL OPERATING CONDITIONS, THE GMLTS IAU SHALL PROVIDE POWER TO

BOTH THE “+VDC OPERATE” AND “+VDC HEATER” INPUTS AS DEFINED IN TABLE I AND

TABLE II.

3.2.1.3.1.1.2 EXTERNAL DC POWER SOURCE.

THE EXTERNAL DC POWER SUPPLY SHALL BE INCLUDED WITH EACH PRIMARY

COMPUTER. THE INPUT POWER FOR THE EXTERNAL DC POWER SOURCE SHALL BE

60HZ, 120 VAC. AT A MINIMUM, THE EXTERNAL DC POWER SOURCE OUTPUT SHALL BE

CAPABLE OF PROVIDING POWER, AS DEFINED IN TABLE II, TO BOTH “+VDC OPERATE”

AND “+VDC HEATER” INPUTS, AND PROVIDE SHORT CIRCUIT , OVERVOLTAGE, AND

OVERCURRENT PROTECTION WITH AUTOMATIC RECOVERY.

TABLE I:

”+VDC OPERATE” INPUT POWER & 28VDC PASSTHROUGH TO J-2

(+ VDC OPERATE /+VDC RETURN)

REQUIREMENTS LIMITS

INPUT VOLTAGE RANGE 1/ 23 –29 VDC 3/

MAXIMUM RIPPLE AMPLITUDE +/- 1.0 VOLTS MAXIMUM

SURGES NO REQUIREMENT

SPIKES MUST CONFORM TO MIL-STD-1275A

PARAGRAPH 5.2.4

MAXIMUM CURRENT 1.5 AMPS @ 28VDC 2/

1/ UPPER LIMIT IS AN ABSOLUTE MAXIMUM FOR THE SUM OF THE STEADY-STATE AND THE RIPPLE

VOLTAGES BUT DOES NOT INCLUDE THE VOLTAGE SPIKES.

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2/ THIS POWER SOURCE HAS NO INRUSH CAPABILITY.

3/ THIS POWER SOURCE CONTAINS OVERVOLTAGE PROTECTION CIRCUITRY WHICH WILL ENSURE THE

OUTPUT VOLTAGE WILL NOT EXCEED 38V UNDER ANY NORMAL OR ABNORMAL CONDITION OF THE

INPUTS VOLTAGE, THE LOAD CURRENT, OR A POWER SUPPLY FAILURE.

TABLE II:

”+VDC HEATER” POWER REQUIREMENTS & 28VDC PASSTHROUGH TO J-2

(+VDC HEATER/HEATER RETURN)

REQUIREMENTS LIMITS

INPUT VOLTAGE RANGE 1/ 23 – 29 VDC 2/

MAXIMUM RIPPLE AMPLITUDE +/- 1.0 VOLTS MAXIMUM

SURGES NO REQUIREMENT

SPIKES MUST CONFORM TO MIL-STD-1275A

PARAGRAPH 5.2.4

MAXIMUM CURRENT/INRUSH 2.5 AMPS @28VDC/ 5 AMPS MAX INRUSH FOR 350MSEC

1/ UPPER LIMIT IS AN ABSOLUTE MAXIMUM FOR THE SUM OF THE STEADY-STATE AND THE RIPPLE

VOLTAGES BUT DOES NOT INCLUDE THE VOLTAGE SPIKES.

2/ THIS POWER SOURCE CONTAINS OVERVOLTAGE PROTECTION CIRCUITRY WHICH WILL ENSURE THE

OUTPUT VOLTAGE WILL NOT EXCEED 38V UNDER ANY NORMAL OR ABNORMAL CONDITION OF THE

INPUTS VOLTAGE, THE LOAD CURRENT, OR A POWER SUPPLY FAILURE..

3.2.1.3.1.2 PRIMARY COMPUTER POWER UP/POWER DOWN REQUIREMENTS.

THE PRIMARY COMPUTER SHALL BE CAPABLE OF AUTOMATICALLY POWERING UP AND

ACHIEVING STEADY STATE OPERATION ONLY UPON APPLICATION OF “+VDC HEATER”

POWER IN ACCORDANCE WITH THE LIMITS IN TABLE II.

IN THE EVENT THAT THE “+VDC HEATER” POWER SOURCE MOMENTARILY FALLS OUT OF

REGULATION DURING STEADY STATE OPERATION, THE PRIMARY COMPUTER SHALL USE

THE “+VDC OPERATE” POWER SOURCE IN ACCORDANCE WITH THE LIMITS IN TABLE I,

TO SUSTAIN NORMAL OPERATION UNTIL THE “+VDC HEATER” POWER SOURCE RETURNS

TO NORMAL REGULATION.

3.2.1.3.1.3 HEATER INPUT POWER REQUIRMENTS.

ANY OPTIONAL HEATING ELEMENTS REQUIRED TO ALLOW OPERATION IN COLD

ENVIRONMENTS SHALL BE CAPABLE OF OPERATING FROM ONLY THE “+VDC HEATER”

POWER SOURCE AS SPECIFIED IN TABLE II.

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3.2.1.3.1.4 PRIMARY COMPUTER POWER PASSTHROUGH REQUIREMENTS.

POWER AND GROUND FOR BOTH INPUT POWER SOURCES AT THE J4 CONNECTOR SHALL

BE PASSED THROUGH (DIRECTLY CONNECTED) TO THE CORRESPONDING PINS OF THE J5

CONNECTOR. (REFERENCE APPENDIX I, J5 AND J4 PINOUTS)

THE PASSTHOUGH CIRCUITRY OF THE PRIMARY COMPUTER BETWEEN THE J4 AND J5

CONNECTORS SHALL BE ABLE TO WITHSTAND A DIRECT SHORT BETWEEN +28V AND

GROUND OF EITHER POWER SUPPLY AT THE J5 CONNECTOR. A SHORT CIRCUIT OF THE

“+VDC OPERATE” POWER SUPPLY CAN CAUSE A SUSTAINED CURRENT DRAW OF 5 AMPS

BEFORE FOLDBACK OCCURS. A SHORT CIRCUIT OF THE “+VDC HEATER” POWER SUPPLY

CAN CAUSE AN INITIAL INRUSH OF 23.3 AMPS FOR A DURATION OF 750 MSEC AND A

SUSTAINED CURRENT DRAW OF 11.5 AMPS BEFORE FOLDBACK OCCURS.

UNDER NORMAL OPERATING CONDITIONS, THE MAXIMUM CURRENT DRAWN BY ANY

DEVICE CONNECTED TO EITHER OF THE POWER SOURCES AT THE J5 CONNECTOR SHALL

BE LIMITED AS FOLLOWS. (THE PRIMARY COMPUTER IS NOT REQUIRED TO LIMIT THE

CURRENT DRAWN AT THE J5 CONNECTOR)

LIMIT

INRUSH CURRENT 5 AMPS PEAK (MAX 350 MSEC)

STEADYSTATE CURRENT 0.5A CONTINUOUS

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3.2.1.3.2 REMOVED

3.2.1.3.3 PARALLEL PORT PERFORMANCE.

THE PARALLEL PORT PROTOCOL SHALL CONFORM TO THE CENTRONICS INDUSTRY

STANDARD (BIDIRECTIONAL) MODE. THE FOLLOWING STATUS INPUT RECEIVERS AND

ALL DATA LINES SHALL BE INTERNALLY PULLED TO VCC USING A RESISTANCE

BETWEEN 1.2K OHM TO 10K OHM.

~ACK (J5-5)

BUSY (J5-4)

SLCT (J5-1)

~ERROR (J5-12)

PE (J5-15)

3.2.1.3.4 SERIAL PORT PERFORMANCE.

BOTH SERIAL PORTS SHALL CONFORM TO THE EIA-RS-232-C SPECIFICATION. BOTH

PORTS SHALL BE CAPABLE OF SUPPORTING BIDIRECTIONAL FULL DUPLEX DATA

TRANSFER AND HANDSHAKE SIGNALS AND SHALL HAVE MINIMUM OPERATING RANGES

OF 300 TO 38,400 BAUD.

3.2.1.3.5 1553 PORT PERFORMANCE.

THE 1553 PORT SHALL BE IN ACCORDANCE WITH THE OPERATIONAL REQUIREMENTS AS

SPECIFIED IN MIL-STD-1553B. THE 1553 INTERFACE BOARD SHALL BE AN ALTA MPCIE-

1553-1D-E.

3.2.1.3.6 NETWORK INTERFACE.

THE NETWORK INTERFACE PORT SHALL BE IN ACCORDANCE WITH THE INDUSTRY

STANDARD 10BASE-T/100BASE-TX ETHERNET NETWORK INTERFACE AS A MINIMUM.

3.2.1.3.7 EXTERNAL KEYBOARD PERFORMANCE.

THE PRIMARY COMPUTER SHALL BE CAPABLE OF SUPPORTING AN EXTERNAL INDUSTRY

STANDARD 101-KEY KEYBOARD.

3.2.1.3.8 EXTERNAL VGA PORT PERFORMANCE.

AS A MINIMUM, THE PRIMARY COMPUTER SHALL BE CAPABLE OF SUPPORTING AN

EXTERNAL 800 X 600 COLOR SVGA MONITOR.

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3.2.1.3.9 REMOVED.

3.2.1.3.10 UNIVERSAL SERIAL BUS (USB).

THE USB INTERFACE PORT SHALL BE IN ACCORDANCE WITH OR BACKWARD

COMPATIBLE WITH THE INDUSTRY STANDARD 1.0 COMPLIANT, 4 PIN, USB INTERFACE.

3.2.1.3.11 COMPACT DISK READ/WRITE (CD R/W).

THE COMPACT DISK READ/WRITE (CD R/W) DRIVE SHALL CONFORM TO THE ATAPI

INTERFACE WITH A MINIMUM WRITE SPEED OF 4X.

3.2.1.3.12 POWER-ON TIME.

THE PRIMARY COMPUTER SHALL BE CAPABLE OF REACHING OPERATIONAL STATUS,

DEFINED AS COMPLETION OF POWER-ON-SELF-TEST AND START OF EXECUTION OF THE

DISK-BASED OPERATING SYSTEM, WITHIN ONE MINUTE OF POWER-ON AT ANY

OPERATIONALLY REQUIRED TEMPERATURE.

3.2.1.3.13 DISPLAY PERFORMANCE.

THE DISPLAY-SHALL BE VISIBLE IN BOTH DAYLIGHT AND IN LOW-LIGHT APPLICATIONS

WITH THE AID OF AN ADJUSTABLE BACKLIGHT.

3.2.2 PHYSICAL CHARACTERISTICS.

THE REQUIRED PHYSICAL CHARACTERISTICS OF THE PRIMARY COMPUTER SHALL BE AS

SPECIFIED HEREIN.

3.2.2.1 DIMENSIONS.

THE PHYSICAL DIMENSIONS OF THE -PRIMARY COMPUTER SHALL NOT EXCEED 16.5"

(WIDTH) X 14" (DEPTH) X 5.5" (HEIGHT) WITH THE DISPLAY IN THE CLOSED, LATCHED

POSITION FOR TRANSPORT.

3.2.2.2 WEIGHT.

THE MAXIMUM WEIGHT OF THE PRIMARY COMPUTER CONFIGURED AS SPECIFIED

HEREIN SHALL BE NO MORE THAN 22 POUNDS.

3.2.2.3 FINISH.

THE COLOR SHALL BE OLIVE DRAB GREEN OR GREEN CARC (CHEMICAL AGENT

RESISTIVE COATING).

3.2.2.4 HANDLES.

THE PRIMARY COMPUTER SHALL INCLUDE STRAPS OR RECESSED METAL HANDLES TO

AID IN TRANSPORT. IN THE STOWED POSITION, THE HANDLES MAY NOT CAUSE THE

FOOTPRINT OF THE COMPUTER TO EXCEED THE PHYSICAL DIMENSIONS SPECIFIED IN

3.2.2.1.

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3.2.2.5 RUBBER FEET.

RUBBER FEET MAY BE PLACED ON THE EXTERIOR OF THE CASE BUT SHALL NOT CAUSE

THE FOOTPRINT OF THE COMPUTER TO EXCEED THE PHYSICAL DIMENSIONS SPECIFIED

IN 3.2.2.1.

3.2.2.6 CHASSIS.

THE UNIT'S CASE SHALL BE SUFFICIENTLY RUGGEDIZED TO WITHSTAND EXTREME

HANDLING AND TO PROTECT THE INTERIOR ASSEMBLIES FROM THE ENVIRONMENTAL

CONDITIONS SPECIFIED HEREIN. THE CHASSIS OF THE PRIMARY COMPUTER SHALL

PROVIDE ENVIRONMENTAL PROTECTION FOR CONNECTORS AND INPUT/OUTPUT (I/0)

DEVICES. LIDS AND COVERS SHALL LATCH SECURELY FOR TRANSPORT. ALL

DETACHABLE PARTS SHALL BE TETHERED TO THE CHASSIS TO PREVENT BEING LOST OR

SEPARATED FROM THE PRIMARY COMPUTER.

3.2.2.7 KEYBOARD.

THE KEYBOARD SHALL BE MADE AN INTEGRAL PART OF THE CASE. THE KEYBOARD

SHALL BE SEALED TO PROTECT THE INTERIOR IN ADVERSE ENVIRONMENTS. A

BACKLIGHT SHALL BE INSTALLED TO AID VIEWING DURING LOW-LIGHT OPERATION.

3.2.2.8 DISPLAY.

THE DISPLAY SHALL BE MOUNTED IN THE LID OVER THE KEYBOARD. THE LID SHALL BE

ATTACHED TO THE CHASSIS OF THE PRIMARY COMPUTER. THE DISPLAY ANGLE SHALL

BE ADJUSTABLE TO REDUCE GLARE ON THE SCREEN. THE LID SHALL CLOSE WITH THE

DISPLAY IN PLACE. A BACKLIGHT WITH ADJUSTABLE INTENSITY SHALL BE INSTALLED

TO AID IN VISION DURING LOW-LIGHT OPERATION. THE BACKLIGHT SHALL BE

ADJUSTABLE AS REQUIRED TO SET INTENSITY. BACKLIGHT INTENSITY SHALL BE

ADJUSTABLE WITHOUT AFFECTING ANY CONCURRENT PROCESSING BY THE COMPUTER.

3.2.2.9 CONNECTORS.

THE I/0 CONNECTORS MOUNTED IN THE PRIMARY COMPUTER SHALL BE CAPABLE OF

MATING WITH THE CONNECTORS AS SPECIFIED IN SECTION 3.2.2.9.1 THROUGH 3.2.2.9.8.

THE REFERENCE DESIGNATOR FOR EACH CONNECTOR SHALL BE MARKED IN CLOSE

PROXIMITY TO THE RESPECTIVE CONNECTOR.

3.2.2.9.1 POWER I/0 CONNECTOR (J4).

THE POWER I/0 CONNECTOR MOUNTED ON THE PRIMARY COMPUTER THAT PASS

PRIMARY COMPUTER AND HEATER POWER INTO THE PRIMARY COMPUTER SHALL MATE

WITH MILITARY PART NUMBER MS38999/26WB99-SN. THE CONNECTOR SHALL BE

DESIGNATED AS J4. SEE APPENDIX I - 10.3 FOR PIN-OUT.

3.2.2.9.2 1553B PORT CONNECTOR (J1).

THE MIL-STD-1553B INTERFACE CONNECTOR SHALL MATE WITH MILITARY PART

NUMBER MS38999/26WD35PN. THE CONNECTOR SHALL BE DESIGNATED AS J1. SEE

APPENDIX I - 10.1 FOR CONNECTOR PIN-OUT.

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3.2.2.9.3 PARALLEL INTERFACE CONNECTOR (J5).

THE PARALLEL INTERFACE CONNECTOR SHALL MATE WITH MILITARY PART NUMBER

MS38999/26WD35PA. THE CONNECTOR SHALL BE DESIGNATED AS J5. SEE APPENDIX I -

10.4 FOR CONNECTOR PIN-OUT.

3.2.2.9.4 SERIAL INTERFACE CONNECTOR (J3).

THE SERIAL INTERFACE CONNECTOR SHALL MATE WITH MILITARY PART NUMBER

MS38999/26WC35PN. THE CONNECTOR SHALL BE DESIGNATED AS J3. SEE APPENDIX I -

10.2 FOR CONNECTOR PIN-OUT.

3.2.2.9.5 REMOVED.

3.2.2.9.6 EXTERNAL DISPLAY CONNECTOR.

THE EXTERNAL DISPLAY CONNECTOR SHALL MATE WITH THE INDUSTRY STANDARD

HIGH DENSITY 15 PIN D-SUBMINIATURE CONNECTOR. SEE APPENDIX I - 10.6 FOR

CONNECTOR PIN-OUT.

3.2.2.9.7 UNIVERSAL SERIAL BUS.

THE EXTERNAL USB CONNECTOR SHALL MATE WITH THE INDUSTRY STANDARD USB

CONNECTOR. SEE APPENDIX I 10-7 FOR PIN-OUT.

3.2.2.9.8 NETWORK BUS.

THE EXTERNAL NETWORK CONNECTOR SHALL MATE WITH THE INDUSTRY STANDARD

NETWORK CONNECTOR. SEE APPENDIX I 10-8 FOR PIN-OUT.

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3.2.2.10 PLACEMENT OF ENVIRONMENTALLY PROTECTED CONNECTORS.

THE ENVIRONMENTALLY SEALED CONNECTORS (J1, J3,J4, AND J5) SHALL BE LOCATED

ON EITHER THE RIGHT HAND SIDE OR BACK SIDE FROM THE ORIENTATION FACING THE

CONTROLLER SCREEN. THE CONNECTORS SHALL BE EQUALLY DISTRIBUTED TO ALLOW

CONNECTION AND REMOVAL OF MATING CONNECTORS. THE SHELL OF EACH

CONNECTOR SHALL BE GROUNDED.

3.2.2.11 PROTECTION OF COMMERCIAL INTERFACES.

ALL COMMERCIAL INTERFACES AND CONNECTORS SHALL BE LOCATED BEHIND AND

PROTECTED BY A REMOVABLE, BUT TETHERED ENVIRONMENTALLY SEALED ACCESS

COVER PLATE.

3.2.2.12 MOUNTING OF CONTROLLER TO GMLTS IAU.

THE CONTROLLER SHALL BE CAPABLE OF BEING SECURED TO THE EXISTING GMLTS

MOUNTING PLATE. (P/N 96214-3156269) WHEN THE CONTROLLER IS MOUNTED TO THE

PLATE, THE REAR OF THE CONTROLLER SHALL NOT EXTEND BACK MORE THAN 1.75

INCHES PAST THE THUMBSCREWS.

3.2.2.13 REPLACEMENT OF BIOS CMOS MEMORY BACKUP BATTERY.

THE BIOS CMOS MEMORY BACKUP BATTERY SHALL BE FIELD REPLACEABLE.

3.2.3 RELIABILITY.

THE RELIABILITY REQUIREMENTS FOR THE PRIMARY COMPUTER SHALL APPLY DURING

AND AFTER EXPOSURE TO ANY LOGICAL COMBINATION OF ENVIRONMENTAL

CONDITIONS DEFINED IN THIS SPECIFICATION. THIS INCLUDES STORAGE, HANDLING,

AND TRANSPORTATION.

3.2.3.1 OPERATING RELIABILITY.

THE PRIMARY COMPUTER SHALL HAVE A MEAN-TIME BETWEEN FAILURES (MTBF)

DURING OPERATION OF NO LESS THAN 4000 HOURS. THE MTBF SHALL BE CALCULATED

IN ACCORDANCE WITH THE PARTS STRESS ANALYSIS PREDICTION METHOD OF

MIL-HDBK-217E. ITEMS NOT INCLUDED IN THIS SPECIFICATION, AS A PART OF THE

PRIMARY COMPUTER CONFIGURATION SHALL NOT BE INCLUDED IN THE MTBF

CALCULATION.

3.2.4 MAINTAINABILITY.

THE MANUFACTURER SHALL SPECIFY THE MAINTAINABILITY REQUIREMENTS.

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3.2.5 ENVIRONMENTAL CONDITIONS.

UNLESS SPECIFIED OTHERWISE HEREIN, THE PRIMARY COMPUTER SHALL BE IN

ACCORDANCE WITH THE PHYSICAL AND PERFORMANCE CHARACTERISTICS SPECIFIED

HEREIN AFTER BEING SUBJECTED TO THE ENVIRONMENTAL CONDITIONS AS SPECIFIED

IN MIL-PRF-28800F FOR CLASS 2, TEST EQUIPMENT. THE ENVIRONMENTAL

REQUIREMENTS ARE SPECIFIED IN TABLE III.

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TABLE III:

PRIMARY COMPUTER ENVIRONMENTAL REQUIREMENTS

REQUIREMENT MIL-PRF-28800F

PARAGRAPH

COMMENTS

TEMPERATURE, NOT OPERATING 3.8.2.1.1 -51 TO 71 C

TEMPERATURE, OPERATING 3.8.2.2.2 -10 TO 55 C (Note 3)

RELATIVE HUMIDITY 3.8.2.3.2

ALTITUDE, NOT OPERATING 3.8.3

ALTITUDE, OPERATING 3.8.3

VIBRATION, RANDOM - NOT REQUIRED

VIBRATION, SINUSOIDAL 3.8.4.2

BOUNCE, LOOSE CARGO - NOT REQUIRED

SHOCK, FUNCTIONAL 3.8.5.1

TRANSIT DROP 3.8.5.2

BENCH HANDLING 3.8.5.3

SHOCK, HIGH IMPACT - NOT REQUIRED

WATERTIGHT - NOT REQUIRED

SPLASHPROOF (Note 1)

DRIPPROOF - NOT REQUIRED

FUNGUS RESISTANCE 3.8.7

SALT EXPOSURE, ENCLOSURE - NOT REQUIRED

SALT EXPOSURE STRUCTURAL

PARTS

3.8.8.2

EXPLOSIVE ATMOSPHERE - NOT REQUIRED

DUST EXPOSURE (Note 2)

MAGNETIC ENVIRONMENT - NOT REQUIRED

ACOUSTIC NOISE - NOT REQUIRED

SOLAR RADIATION - NOT REQUIRED

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1/ THE PRIMARY COMPUTER SHALL BE DESIGNED TO OPERATE IN ACCORDANCE WITH THE PHYSICAL AND PERFORMANCE CHARACTERISTICS AS SPECIFIED IN THIS DOCUMENT AFTER BEING SUBJECTED TO THE RAIN CONDITIONS SPECIFIED IN MIL-STD-810E, METHOD 506.3, PROCEDURE I, 4 INCHES/HOUR AT

40 MPH.

2/ THE PRIMARY COMPUTER SHALL BE DESIGNED TO OPERATE IN ACCORDANCE WITH THE PHYSICAL AND PERFORMANCE CHARACTERISTICS AS SPECIFIED IN THIS DOCUMENT AFTER BEING SUBJECTED TO THE DUST CONDITIONS SPECIFIED IN MIL-STD-810E, METHOD 510.3, PROCEDURE I, BLOWING DUST

USING 1750 FPM AIR VELOCITY @ 0.3 +/- 0.2 G/FT3 DUST CONCENTRATION.

3/ THE OPERATIONAL TEMPERATURE RANGE THAT THE CD R/W DRIVE IS REQUIRED TO BE CAPABLE TO ACCESS AND WRITE DATA SHALL BE LIMITED TO +5 TO +50 DEGREE C. ATTEMPTING TO ACCESS OR

WRITE DATA OUTSIDE THIS ENVELOPE, BUT WITHIN THE OPERATIONAL TEMPERATURE OF THE

PRIMARY COMPUTER SHALL NOT RESULT IN DAMAGE.

3.2.6 TRANSPORTABILITY.

CHARACTERISTICS AND CONSIDERATIONS RELATED TO PACKAGING, HANDLING AND

TRANSPORTABILITY INCLUDING INDUCED ENVIRONMENTS, SIZE, HAZARDOUS

MATERIALS, WEIGHT AND FRAGILITY SHALL BE CONSIDERED IN THE DESIGN OF THE

PRIMARY COMPUTER.

3.3 DESIGN AND CONSTRUCTION.

3.3.1 MATERIALS, PROCESSES, AND PARTS.

MATERIALS, PROCESSES, AND PARTS SHALL BE USED WHICH ENABLE THE PRIMARY

COMPUTER ASSEMBLY TO MEET THE REQUIREMENTS FOR RELIABILITY,

MAINTAINABILITY, SURVIVABILITY, SAFETY, LOGISTICS, AND SUPPORTABILITY

SPECIFIED HEREIN.

3.3.1.1 PROCESSES.

SOLDERING SHALL BE IN ACCORDANCE GENERALLY ACCEPTED INDUSTRY STANDARDS

FOR ELECTRONIC EQUIPMENT.

3.3.2 ELECTROMAGNETIC RADIATION.

THE PRIMARY COMPUTER SHALL BE DESIGNED TO MEET THE TAILORED -

ELECTROMAGNETIC COMPATIBILITY (EMC) REQUIREMENTS OF MIL-STD-461E FOR

GROUND AIR FORCE AND NAVY CLASS AS SPECIFIED IN TABLE IV.

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TABLE IV:

PRIMARY COMPUTER ELECTROMAGNETIC COMPATIBILITY SPECIFICATIONS

REQUIREMENTS DESCRIPTION

CE102 CONDUCTED EMISSIONS, POWER LEADS

CS101 CONDUCTED SUSCEPTIBILITY, POWER LEADS

CS114 CONDUCTED SUSCEPTIBILITY, BULK CABLE INJECTION

CS116 CONDUCTED SUSCEPTABILITY, DAMPED SINUSOIDAL TRANSIENTS,

CABLES AND POWER LEADS

RE102 RADIATED EMISSIONS, ELECTRICAL FIELD

RS103 RADIATED SUSCEPTIBILITY, ELECTRIC FIELD

3.3.2.1 EMC TEST CONFIGURATION.

EMC TESTING SHALL BE CONDUCTED UNDER THE CONFIGURATION SPECIFIED IN A

THROUGH D.

A. ACCESS COVERS INSTALLED

B. MONITOR EXPOSED

C. POWER CABLE (J4) AND RS-232 (J3) CABLE SHALL BE CONNECTED.

D. J1 AND J5 SHALL BE UNCONNECTED AND SHALL HAVE THE DUST CAPS

INSTALLED.

3.3.3 IDENTIFICATION AND MARKING.

THE PRIMARY COMPUTER AND COMPONENTS THEREOF SHALL BE IDENTIFIED BY

SUITABLE NUMBERING IN ORDER TO PROVIDE CONFIGURATION IDENTIFICATION,

CHANGE CONTROL, AND STATUS ACCOUNTING MARKING SHALL BE IN ACCORDANCE

WITH MIL-STD-130K. ALL PARTS, ASSEMBLIES, OR SUBSYSTEMS, WHICH REQUIRE

SPECIAL CARE DURING HANDLING, SHIPPING, INSTALLATION, OR TEST SHALL BE

IDENTIFIED AND MARKED ACCORDINGLY.

3.3.3.1 ELECTRICAL WARNING MARKINGS.

DANGER, CAUTION, ETC., SIGNS, LABELS AND MARKINGS SHALL BE USED TO WARN OF

SPECIFIC HAZARDS SUCH AS VOLTAGE, CURRENT, THERMAL, OR PHYSICAL. THE SIGNS,

LABELS, AND MARKINGS SHALL BE AS PERMANENT AS THE NORMAL LIFE EXPECTANCY

OF THE EQUIPMENT ON WHICH THEY ARE AFFIXED. GUARDS, BARRIERS, AND ACCESS

DOORS, COVERS OR PLATES SHALL BE MARKED TO INDICATE THE HAZARD WHICH MAY

BE PRESENT UPON REMOVAL OF SUCH DEVICES. ADDITIONALLY, HAZARDS INTERNAL

TO A UNIT SHALL BE MARKED ADJACENT TO HAZARDS IF THEY ARE SIGNIFICANTLY

DIFFERENT FROM THOSE OF SURROUNDING ITEMS. SUCH A CASE WOULD BE A HIGH

VOLTAGE TERMINAL IN A GROUP OF LOW VOLTAGE DEVICES.

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3.3.4 WORKMANSHIP.

WORKMANSHIP IN THE FABRICATION AND ASSEMBLY OF THE PRIMARY COMPUTER

SHALL COMPLY WITH THE REQUIREMENTS OF MIL-STD-454M, REQUIREMENT 9.

3.3.5 INTERCHANGEABILITY.

THE PRIMARY COMPUTER SHALL NOT HAVE ANY UNIQUE CHARACTERISTICS NOT

SPECIFIED IN THIS DOCUMENT THAT WOULD PREVENT BEING REPLACED WITH AN

EQUIVALENT SYSTEM, WHICH CONFORMS TO THIS SPECIFICATION. ALL REPLACEABLE

ITEMS BEARING THE SAME PART NUMBER SHALL BE FUNCTIONALLY AND PHYSICALLY

INTERCHANGEABLE.

3.3.6 SAFETY.

ALL HARDWARE AND ASSOCIATED SOFTWARE SHALL BE DESIGNED SO THAT THE

PROBABILITY OF HARDWARE OR SOFTWARE FAILURE RESULTING IN A CATEGORY I

HAZARD SHALL NOT EXCEED A HAZARD PROBABILITY CATEGORIZATION OF

"IMPROBABLE". MIL-STD-882D SHALL BE USED TO DEFINE CATEGORY I HAZARD AND

HAZARD PROBABILITY CATEGORIZATION OF IMPROBABLE. NO OTHER REQUIREMENTS

FROM MIL-STD-882D ARE IMPLIED. SAFETY SHALL BE IN ACCORDANCE WITH

MIL-STD-454M REQUIREMENT 1 AND AS SPECIFIED HEREIN. A FUSE SHALL NOT BE

REQUIRED INTERNAL TO THE PRIMARY COMPUTER ON THE DC INPUT.

3.3.6.1 OPERATOR SAFETY.

OPERATING AND MAINTENANCE PERSONNEL SHALL BE PROTECTED FROM HAZARDOUS

POTENTIALS BY SHIELDING, MARKING, OR OTHER SUITABLE MEASURES IN

ACCORDANCE WITH 3.3.6.1.1 AND 3.3.6.1.4.

3.3.6.1.1 OPERATION.

WHILE TEST EQUIPMENT IS OPERATING, SHOCK PROTECTION SHALL BE PROVIDED IF

THE OPEN CIRCUIT VOLTAGE BETWEEN ANY ACCESSIBLE PART OF THE TEST

EQUIPMENT AND GROUND OR ANY OTHER SIMULTANEOUSLY ACCESSIBLE PART

EXCEEDS 30 V ROOT-MEAN-SQUARED (42.2 V PEAK) OR 60 VOLTS DIRECT CURRENT

(VDC).

3.3.6.1.2 MAINTENANCE.

SUITABLE MEASURES SHALL BE INCORPORATED TO PROTECT MAINTENANCE

PERSONNEL FROM ALL INTERNAL HAZARDOUS POTENTIALS. CAPACITORS SHALL BE

DISCHARGED TO LESS THAN 42.4 V PEAK WITHIN 2 SECONDS AFTER POWER

INTERRUPTION- UNLESS MARKINGS INDICATE A LONGER DISCHARGE INTERVAL. PARTS

OF EQUIPMENT WHICH BECOME ACCESSIBLE UPON REMOVING A COVER, OPENING A

DOOR, ADJUSTING A CONTROL, SETTING A SUPPLY CIRCUIT VOLTAGE MECHANISM,

REPLACING A FUSE, ATTACHING AND DETACHING AN INTERCONNECTING CABLE

ASSEMBLY, ETC, AND ARE INTENDED FOR ACCESS BY THE OPERATOR DURING NORMAL

USE, SHALL NOT RENDER AN ELECTRIC SHOCK. OPERATOR MAINTENANCE WILL BE

LIMITED TO CLEANING THE DISPLAY AND THE EXTERIOR OF THE CASE.

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3.3.6.1.3 OPEN CIRCUIT VOLTAGE PROTECTION.

THE OPEN CIRCUIT POTENTIAL BETWEEN ANY ACCESSIBLE PART AND EITHER GROUND

OR ANY OTHER SIMULTANEOUSLY ACCESSIBLE PART SHALL NOT EXCEED THE LIMITS

SPECIFIED IN 3.3.6.1.2.

3.3.6.1.4 LEAKAGE CURRENT PROTECTION.

IN THE EVENT THE OPEN CIRCUIT POTENTIAL EXCEEDS LEVELS SPECIFIED IN 3.3.6.1.2,

LEAKAGE CURRENT SHALL BE MEASURED AND SHALL NOT EXCEED 3.5 MA

(MILLIAMPERES).

3.3.7 HUMAN PERFORMANCE/HUMAN ENGINEERING.

MIL-STD-1472F SHALL BE USED AS A DESIGN GUIDE.

3.3.8 DOCUMENTATION.

DOCUMENTATION IN THE FORM OF USER'S MANUALS SHALL BE PROVIDED BY THE

MANUFACTURER AS A PART OF THE PRIMARY COMPUTER.

3.4 QUALIFICATION.

QUALIFICATION TESTING AS SPECIFIED IN 4.1.2 SHALL BE COMPLETED TO VERIFY THE

DESIGN IS IN ACCORDANCE WITH THE REQUIREMENTS SPECIFIED HEREIN. PREVIOUS

ENVIRONMENTAL TESTING BY THE MANUFACTURER OR THE MANUFACTURER'S

REPRESENTATIVE MAY BE SUBSTITUTED FOR THE REQUIRED TESTING WITH

PROCURING ACTIVITY CONCURRENCE. THE ENVIRONMENTAL TEST DATA WILL BE

REVIEWED BY THE PROCURING ACTIVITY TO ENSURE THE PRIMARY COMPUTER DESIGN

ADHERES TO ALL SPECIFIED REQUIREMENTS.

3.4.1 LOCATION.

QUALIFICATION TESTING SHALL TAKE PLACE AT THE MANUFACTURER'S FACILITY OF

CHOICE UNLESS DISAPPROVED BY THE PROCURING ACTIVITY.

3.4.2 SCHEDULE FOR TESTING.

SCHEDULE FOR TESTING SHALL BE ESTABLISHED BY MUTUAL CONSENT OF THE

MANUFACTURER AND THE PROCURING ACTIVITY.

4. QUALITY ASSURANCE PROVISIONS.

4.1 GENERAL.

THIS SECTION SPECIFIES THE QUALIFICATION AND PRODUCTION REQUIREMENTS FOR

INSPECTION AND TEST FOR THE PRIMARY COMPUTER.

4.1.1 RESPONSIBILITY FOR INSPECTION.

THE SUPPLIER SHALL BE RESPONSIBLE FOR THE PERFORMANCE OF ALL INSPECTION

AND TEST REQUIREMENTS SPECIFIED HEREIN. THE SUPPLIER MAY USE HIS OWN OR ANY

OTHER FACILITIES SUITABLE FOR THE PERFORMANCE OF THE TEST REQUIREMENTS

SPECIFIED HEREIN UNLESS DISAPPROVED BY THE PROCURING ACTIVITY. THE

PROCURING ACTIVITY RESERVES THE RIGHT TO PERFORM ANY OF THE TESTS SET

FORTH IN THIS DOCUMENT WHERE SUCH TESTS ARE DEEMED NECESSARY TO ENSURE

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THAT THE EQUIPMENT CONFORMS TO SPECIFIED REQUIREMENTS. INSPECTION

REQUIREMENTS SHALL BE ACCOMPLISHED BY ONE OR MORE OF THE FOLLOWING

METHODS:

A. INSPECTION - VISUAL AND DIMENSIONAL CHECKS.

B. ANALYSIS - REVIEW OF PREVIOUS TEST DATA AND/OR THEORETICAL ANALYSIS.

C. DEMONSTRATION - DEMONSTRATION OF COMPLIANCE WITH THE REQUIREMENT

WITHOUT THE USE OF MEASUREMENT STANDARDS.

D TEST - FIT AND FUNCTIONAL TEST USING MEASUREMENT STANDARDS WHERE

SPECIFIC MEASUREMENTS ARE COMPARED TO ACCEPTANCE CRITERIA.

4.1.1.1 QUALITY ASSURANCE TERMS AND DEFINITIONS.

QUALITY ASSURANCE TERMS USED HEREIN SHALL BE DEFINED IN ASQC A8402-1.

4.1.1.2 TEST EQUIPMENT.

EQUIPMENT USED TO PERFORM TESTS AND INSPECTIONS SPECIFIED HEREIN SHALL BE

CALIBRATED AND MAINTAINED IN ACCORDANCE WITH ISO . THE USE OF TEST

EQUIPMENT WHICH DOES NOT MEET THE REQUIREMENTS OF ISO 10012-1-97 AND 10012-2-

98 SHALL REQUIRE GOVERNMENT APPROVAL.

4.1.1.3 TEST CONDITIONS.

UNLESS OTHERWISE SPECIFIED HEREIN OR IN THE APPROVED TEST PLAN, TESTS AND

INSPECTIONS SHALL BE PERFORMED UNDER THE CONDITIONS OF A THROUGH E.

AMBIENT CONDITIONS WITHIN THE SPECIFIED RANGES NEED NOT BE CONTROLLED.

FOR EQUIPMENT HAVING A SPECIFIED WARM-UP OR STABILIZATION PERIOD AFTER

TURN-ON, FORMAL MEASUREMENTS AND OBSERVATIONS SHALL BE MADE ONLY AFTER

THE SPECIFIED INTERVAL.

A. TEMPERATURE: 25 +/- 10 DEGREES C.

B. HUMIDITY: 20 TO 70 PERCENT RELATIVE HUMIDITY.

C. ALTITUDE: 0 TO 3050 METERS (10,000 FT).

D. POWER: 28.0 +/- 1.0 VOLTS.

E. ATTITUDE: NORMAL OPERATING POSITION.

4.1.1.4 MEASUREMENT OF TEST CONDITIONS.

ALL MEASUREMENTS OF THE TEST CONDITIONS SHALL BE MADE WITH INSTRUMENTS

OF THE ACCURACY SPECIFIED IN 4.1.1.6.

4.1.1.5 TOLERANCE OF TEST CONDITIONS.

THE TOLERANCE OF TEST CONDITIONS SHALL BE AS SPECIFIED IN A THROUGH G:

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A. TEMPERATURE. THE TEST ITEM SHALL BE TOTALLY SURROUNDED BY AN

ENVELOPE OF AIR (EXCEPT AT NECESSARY SUPPORT JOINTS). THE TEMPERATURE

OF THE TEST SECTION MEASUREMENT SYSTEM AND THE TEMPERATURE

GRADIENT THROUGHOUT THIS ENVELOPE, WHICH IS MEASURED CLOSE TO THE

TEST ITEM, SHALL BE WITHIN +/- 2.0 DEGREES C OF THE TEST TEMPERATURE

AND SHALL NOT EXCEED 1 DEGREE C PER METER OR A MAXIMUM OF 2.2

DEGREES C TOTAL (EQUIPMENT NONOPERATING).

B PRESSURE. PRESSURE SHALL BE MEASURED WITH AN ACCURACY OF +/- 5

PERCENT OF MEASURED VALUE.

C. HUMIDITY. RELATIVE HUMIDITY AT THE CHAMBER CONTROL SENSOR SHALL BE

+/- 5 PERCENT RELATIVE HUMIDITY (RH) OF MEASURED VALUE.

D. VIBRATION AMPLITUDE. SINUSOIDAL, +/- 10 PERCENT; RANDOM, AS SPECIFIED

FOR METHOD 514 IN MIL-STD-810E.

E. VIBRATION FREQUENCY. VIBRATION FREQUENCY SHALL BE MEASURED WITH

AN ACCURACY OF +/- 2 PERCENT, +/- 0.5 HZ BELOW 25 HZ.

F. ACCELERATION. ACCELERATION SHALL BE MEASURED TO WITHIN +/- 10

PERCENT.

G. TIME. ELAPSED TIME SHALL BE MEASURED WITH AN ACCURACY-OF +/- 1

PERCENT.

4.1.1.6 ACCURACY OF TEST INSTRUMENT CALIBRATION.

THE ACCURACY OF INSTRUMENTS AND TEST EQUIPMENT USED TO CONTROL OR

MONITOR THE TEST PARAMETERS SHALL BE VERIFIED PRIOR TO AND FOLLOWING EACH

TEST AND THEN CALIBRATED AT PREDETERMINED INTERVALS AND SHALL MEET THE

REQUIREMENTS OF ISO 10012-1-97 AND ISO 10012-2-98.

4.1.2 SPECIAL TESTS AND EXAMINATIONS.

THE QUALIFICATION INSPECTION AND TEST REQUIREMENTS AND CORRESPONDING

METHODS FOR THE CRITICAL ITEM ARE SHOWN IN TABLE V.

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TABLE V:

REQUIREMENTS FOR QUALIFICATION TESTING

EXAMINATION OR TEST REQUIREMENT

REFERENCE

MIL-PRF-28800F

METHOD PARAGRAPH

GROUP A:

PRODUCTION INSPECTION

4.5.3

PREOPERATIONAL INSPECTION 3 4.5.3.1 (a,b)

LEVEL A PERFORMANCE 3.2 4.5.3.2 (Note 1)

OPEN CIRCUIT VOLTAGE 3.3.6.1.3 -

LEAKAGE CURRENT 3.3.6.1.4 4.5.3.2.1

GROUP B:

PRODUCTION CONTROL TESTS

4.5.4

LEVEL B PERFORMANCE AS REQ BY THE PURCHASE SPEC 4.5.4

GROUP C:

ENVIRONMENTAL AND

ELECTRICAL POWER TESTS

TEMPERATURE/HUMIDITY TABLE III 4.5.5.1

ALTITUDE TABLE III 4.5.5.2

VIBRATION, SINUSOIDAL TABLE III 4.5.5.3.2 (Note 2)

SHOCK, FUNCTIONAL TABLE III 4.5.5.4.1 (Note 2)

TRANSIT DROP TABLE III 4.5.5.4.2

BENCH HANDLING TABLE III 4.5.5.4.3

SPLASHPROOF TABLE III MIL-STD-810E Method 506.3 Proc I

VERIFICATION GROUP C 3.2 4.5.5.7 (Note 1)

GROUP D:

ENVIRONMENTAL TESTS

FUNGUS RESISTANCE TABLE III 4.5.6.1

SALT FOG TABLE III 4.5.6.2

DUST TABLE III MIL-STD-810E Method 510.3 Proc I

EMC TABLE VI (Note 3)

VERIFICATION, GROUP D 3.2 4.5.6.7 (Note 1)

GROUP E:

OTHER TESTS

DIMENSIONS 3.2.2.1 4.5.7.3

WEIGHT 3.2.2.2 4.5.7.3

GROUP F:

RELIABILITY

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RELIABILITY TEST 3.2.3.1 4.5.8.1

1/ ACCEPTANCE TEST SHALL BE AS SPECIFIED IN 4.1.3.1 OF THIS SPECIFICATION.

2/ DURING THESE TESTS, THE HARD DRIVE AND CD R/W DRIVES MUST BE POWERED BUT THE DRIVES DO

NOT NEED TO BE ACCESSED.

3/ EQUIPMENT SETUP AND MEASUREMENT SHALL BE TO MIL-STD-461E REQUIREMENTS.

4.1.3 PRODUCTION TESTS.

THE MANUFACTURER SHALL DEVELOP A TEST PLAN TO BE COMPLETED FOR EACH UNIT

AND SHALL SUBMIT IT TO THE PROCURING ACTIVITY FOR CONCURRENCE. THE TEST

PLAN SHALL CONTAIN AT A MINIMUM ACCEPTANCE TESTING AND BURN-IN/VIBRATION

ENVIRONMENTAL STRESS SCREENING (ESS).

4.1.3.1 ACCEPTANCE TEST.

EACH PRIMARY COMPUTER SHALL BE SUBJECTED TO AN ACCEPTANCE TEST

PROCEDURE WITH PROVISIONS FOR DOCUMENTATION TO VERIFY COMPLIANCE WITH

THE REQUIREMENTS OF THIS SPECIFICATION. THE MANUFACTURER SHALL DEVELOP

AND SUBMIT TO THE PROCURING ACTIVITY FOR CONCURRENCE A TEST PROCEDURE

WHICH VERIFIES THE PERFORMANCE CHARACTERISTICS AS SPECIFIED IN TABLE VI AS A

MINIMUM.

TABLE VI:

REQUIRED COMPONENTS OF ACCEPTANCE TEST

REQUIREMENT REQUIREMENT PARAGRAPH

SOFTWARE 3.2.1.1

SELF TEST 3.2.1.2

POWER 3.2.1.3.1

PARALLEL PORT PERFORMANCE 3.2.1.3.3

SERIAL PORT PERFORMANCE (QTY 2) 3.2.1.3.4

1553 PORT PERFORMANCE 3.2.1.3.5

NETWORK INTERFACE 3.2.1.3.6

EXTERNAL KEYBOARD PERFORMANCE 3.2.1.3.7

EXTERNAL VGA PERFORMANCE 3.2.1.3.8

PCMCIA PERFORMANCE (QTY 2) 3.2.1.3.9

UNIVERSAL SERIAL BUS (USB) PERFORMANCE 3.2.1.3.10

COMPACT DISK READ/WRITE 3.2.1.3.11

POWER-ON TIME 3.2.1.3.12

DISPLAY PERFORMANCE 3.2.1.3.13

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4.1.3.2 BURN-IN/VIBRATION ESS.

THE MANUFACTURER SHALL DEVELOP A TEST PROCEDURE FOR ESS TESTING IN

ACCORDANCE WITH THE REQUIREMENTS OF THIS SPECIFICATION AND SHALL SUBMIT

THE ESS TEST PROCEDURE TO THE PROCURING ACTIVITY FOR CONCURRENCE. EACH

UNIT -SHALL BE SUBJECTED TO BOTH OPERATING AND NON-OPERATING TEMPERATURE

RANGES DURING BURN-IN TESTING.

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4.2 QUALITY CONFORMATION INSPECTIONS.

INSPECTION SHALL BE PERFORMED AND DOCUMENTS ON ALL SUBASSEMBLIES DURING

THE ASSEMBLY PROCESS. EACH ITEM SHALL BE INSPECTED BY EXAMINATION FOR THE

FOLLOWING: DIMENSIONS, SOLDERING, WIRING, NAMEPLATES, CORRECT REVISION,

PRODUCT MARKING, AND WORKMANSHIP.

4.2.1 PREPRODUCTION.

VERIFICATION METHODS FOR PREPRODUCTION TEST REQUIREMENTS SHALL BE

CONSISTENT WITH REQUIREMENTS IN MIL-PRF-28800F FOR CLASS 2 TEST EQUIPMENT

UNLESS STATED OTHERWISE HEREIN.

4.2.2 QUALIFICATION.

CONFORMANCE TO THE QUALIFICATION REQUIREMENTS SHALL BE VERIFIED IN

ACCORDANCE WITH TABLE VII.

TABLE VII:

CONFORMANCE VERIFICATION MATRIX

VERIFICATION METHODS

REQUIREMENT PARAGRAPH VERIFICATION

METHOD

METHODOLOGY

I A D T

3. REQUIREMENTS TITLE

3.1 DEFINITION DEFINITION

3.1.1 HARDWARE CONFIGURATION TITLE

3.1.1.1 PROCESSOR X

3.1.1.2 RAM X

3.1.1.3 HARD DRIVE X

3.1.1.4 INTERFACE EXPANSION BUS X

3.1.1.5 PARALLEL PORT X

3.1.1.6 SERIAL PORT X

3.1.1.7 1553 PORT X

3.1.1.8 NETWORK INTERFACE X

3.1.1.9 PCMCIA CARD DRIVES X

3.1.1.10 UNIVERSAL SERIAL BUS (USB) X

3.1.1.11 HEATER PLATES X

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TABLE VII CONFORMANCE VERIFICATION MATRIX - CONTINUED

VERIFICATION METHODS

REQUIREMENT PARAGRAPH VERIFICATION

METHOD

METHODOLOGY

I A D T

3.1.1.12 KEYBOARD X

3.1.1.13 EXTERNAL KEYBOARD SUPPORT X

3.1.1.14 DISPLAY X

3.1.1.15 EXTERNAL MONITOR SUPPORT X

3.1.1.16 COMPACT DISC READ/WRITE X

3.1.1.17 SOFTWARE CONFIGURATION (BIOS) X

3.1.1.18 BIOS CMOS MEMORY BACKUP BATTERY X

3.1.1.19 SPEAKER X

3.1.1.20 EXTERNAL DC POWER SUPPLY X

3.2 CHARACTERISTICS TITLE

3.2.1 PERFORMANCE CHARACTERISTICS DEFINITION

3.2.1.1 SOFTWARE PERFORMANCE TITLE

3.2.1.1.1 USER MODIFIABLE BIOS SETTINGS X

3.2.1.1.1.1 BOOT ORDER PRIORITY X

3.2.1.1.1.2 I/O DEVICE CONFIGURATION X

3.2.1.1.1.3 REMOVED (N/A)

3.2.1.1.1.4 IRQ RESOURCE EXCLUSION X

3.2.1.1.1.5 CUSTOM DRIVES X

3.2.1.1.1.6 DISKETTES X

3.2.1.1.2 NON-VOLATILE MEMORY X

3.2.1.1.3 OPERATING SYSTEM X

3.2.1.1.4 APPLICATION SOFTWARE X

3.2.1.2 SELF-TEST X

3.2.1.3 HARDWARE PERFORMANCE TITLE

3.2.1.3.1 POWER DEFINITION

3.2.1.3.1.1 EXTERNAL POWER SOURCES X

3.2.1.3.1.2 PC POWER UP/POWER DOWN REQ X

3.2.1.3.1.3 HEATER INPUT POWER REQUIREMENT X

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TABLE VII CONFORMANCE VERIFICATION MATRIX – CONTINUED

VERIFICATION METHODS

REQUIREMENT PARAGRAPH VERIFICATION

METHOD

METHODOLOGY

I A D T

3.2.1.3.1.4 PRIM COMP PWR PASSTHROUGH REQ X

3.2.1.3.2 EXPANSION BUS PERFORMANCE X

3.2.1.3.3 PARALLEL PORT PERFORMANCE X

3.2.1.3.4 SERIAL PORT PERFORMANCE X

3.2.1.3.5 1553 PORT PERFORMANCE X

3.2.1.3.6 NETWORK INTERFACE X

3.2.1.3.7 EXTERNAL KEYBOARD PERFORMANCE X

3.2.1.3.8 EXTERNAL VGA PORT PERFORMANCE X

3.2.1.3.9 PCMCIA PERFORMANCE X

3.2.1.3.10 UNIVERSAL SERIAL BUS (USB) X

3.2.1.3.11 COMPACT DISK READ/WRITE X

3.2.1.3.12 POWER-ON TIME X

3.2.1.3.13 DISPLAY PERFORMANCE X

3.2.2 PHYSICAL CHARACTERISTICS TITLE

3.2.2.1 DIMENSIONS X

3.2.2.2 WEIGHT X

3.2.2.3 FINISH X

3.2.2.4 HANDLES X

3.2.2.5 RUBBER FEET X

3.2.2.6 CHASSIS X

3.2.2.7 KEYBOARD X

3.2.2.8 DISPLAY X

3.2.2.9 CONNECTORS DEFINITION

3.2.2.9.1 POWER I/O CONNECTOR (J4) X

3.2.2.9.2 1553B PORT CONNECTOR (J1) X

3.2.2.9.3 PARALLEL INTERFACE CONNECTOR (J5) X

3.2.2.9.4 SERIAL & USB INTERFACE CONNECTOR (J3) X

3.2.2.9.5 EXTERNAL KEYBOARD CONNECTOR X

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TABLE VII CONFORMANCE VERIFICATION MATRIX – CONTINUED

VERIFICATION METHODS

REQUIREMENT PARAGRAPH VERIFICATION

METHOD

METHODOLOGY

I A D T

3.2.2.9.6 EXTERNAL VGA DISPLAY CONNECTOR X

3.2.2.9.7 UNIVERSAL SERIAL BUS X

3.2.2.9.8 NETWORK BUS X

3.2.2.10 PLACEMENT OF ENVIRONMENTALLY

PROTECTED CONNECTORS

X

3.2.2.11 PROTECTION OF COMMERCIAL INTERFACE X

3.2.2.12 MOUNTING OF CONTROLLER TO GMLTS X

3.2.2.13 REPLACEMENT OF CMOS BACKUP BATTERY X

3.2.3 RELIABILITY DEFINITION

3.2.3.1 OPERATING RELIABILITY X

3.2.4 MAINTAINABILITY DEFINITION

3.2.5 ENVIRONMENTAL CONDITIONS DEFINITION

3.2.5 TEMPERATURE X

3.2.5 HUMIDITY X

3.2.5 ALTITUDE X

3.2.5 VIBRATION, SINUSOIDAL X

3.2.5 SHOCK, FUNCTIONAL X

3.2.5 TRANSIT DROP X

3.2.5 BENCH HANDLING X

3.2.5 SPLASHPROOF X

3.2.5 FUNGUS RESISTANCE X

3.2.5 SALT ATMOSPHERE X REVIEW OF PREVIOUS TEST

DATA IS ACCEPTABLE

3.2.5 DUST EXPOSURE X

3.2.6 TRANSPORTABILITY X

3.3 DESIGN AND CONSTRUCTION DEFINITION

3.3.1 MATERIALS, PROCESSES, AND PARTS DEFINITION

3.3.1.1 PROCESSES X

3.3.2 ELECTROMAGNETIC RADIATION X

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TABLE VII CONFORMANCE VERIFICATION MATRIX – CONTINUED

VERIFICATION METHODS

REQUIREMENT PARAGRAPH VERIFICATION

METHOD

METHODOLOGY

I A D T

3.3.2.1 EMC TEST CONFIGURATION X

3.3.3 IDENTIFICATION AND MARKING X

3.3.3.1 ELECTROMAGNETIC WARNING MARKINGS X

3.3.4 WORKMANSHIP X

3.3.5 INTERCHANGEABILITY X

3.3.6 SAFETY DEFINITION

3.3.6.1 OPERATOR SAFETY X

3.3.6.1.1 OPERATION X

3.3.6.1.2 MAINTENANCE X

3.3.6.1.3 OPEN CIRCUIT VOLTAGE PROTECTION X

3.3.6.1.4 LEAKAGE CURRENT PROTECTION X

3.3.7 HUMAN FACTORS X

3.3.8 DOCUMENTATION X

3.4 QUALIFICATION TESTING DEFINITION

3.4.1 LOCATION/WHO DOES THE TESTS DEFINITION

3.4.2 SCHEDULE FOR TESTING DEFINITION

I – INSPECTION

A – ANALYSIS

D – DEMONSTRATION

T – TEST

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5. PREPARATION FOR DELIVERY.

5.1 GENERAL.

THE METHODS OF PRESERVATION, PACKAGING, AND PACKING USED SHALL ASSURE

SAFE DELIVERY AT THE DESTINATION AND PROTECT THE SHIPPED UNITS DURING ALL

PHASES OF HANDLING A LONG TERM STORAGE. THE MANUFACTURER ASSUMES

RESPONSIBILITY FOR ALL DAMAGE, BOTH OBVIOUS AND HIDDEN DAMAGE, WHICH

OCCURS DURING SHIPPING.

5.2 SPECIFIC REQUIREMENTS.

UNLESS OTHERWISE SPECIFIED IN THE CONTRACT OR PURCHASE ORDER, THE

PRESERVATION, PACKING, PACKAGING, AND METHOD OF MARKING SHALL BE AS

DEEMED NECESSARY BY THE MANUFACTURER TO ASSURE SAFE DELIVERY OF THE

PRIMARY COMPUTER.

5.3 SHIPPING INFORMATION.

REQUIRED INFORMATION ON THE PRIMARY COMPUTER INCLUDING DESTINATION

SHALL BE SPECIFIED IN THE CONTRACT OR PURCHASE ORDER.

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6. NOTES.

6.1 ORDERING DATA.

PROCUREMENT DOCUMENTS SHOULD SPECIFY THE FOLLOWING:

A. TITLE OF THIS SPECIFICATION.

B. NUMBER OF THIS SPECIFICATION.

C. DATE OF THIS SPECIFICATION.

6.2 DEFINITIONS.

THE FOLLOWING SECTION DEFINES ACRONYMS AND TERMS USED WITHIN THIS

SPECIFICATION.

6.2.1 ABBREVIATIONS AND ACRONYMS.

THE FOLLOWING ABBREVIATIONS AND ACRONYMS ARE USED IN THIS SPECIFICATION.

A/R AS REQUIRED

BIOS BASIC INPUT/OUTPUT SYSTEM

BIT BUILT-IN TEST

C CENTIGRADE

CARC CHEMICAL AGENT RESISTIVE COATING

EMC ELECTROMAGNETIC COMPATIBILITY

EMI ELECTROMAGNETIC INTERFERENCE

ESS ENVIRONMENTAL STRESS SCREENING

GHz GIGA-HERTZ

HZ HERTZ

I…