DRAFT_BAT_Performance_Specification _dated_26_Jan_16 _Rev_8.pdf

PD15WNAEBAT

DRAFT BAT System Performance Specification, 01/26/16, Rev 8

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DRAFT Bomber Armament Tester (BAT) System Performance Specification

01/26/16, Rev 8

DISTRIBUTION STATEMENT A. Approved for public release: Distribution is unlimited.

(78 ABW/PA Certificate Number 15-05272).

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33T1.033T 33TSCOPE33T

33T1.133T 33TScope33T 33T1.1.133T 33TRequirement Levels33T 33T1.1.233T 33TBomber Armament Tester Definition33T 33T1.2 Unit Under Test 33T1.2.133T 33TB-2A Armament System Units Under Tests33T 33T1.2.233T 33TB-1B Armament System Units Under Tests33T 33T1.2.333T 33TB-52H Armament System Units Under Tests33T

33T2.033T 33TAPPLICABLE DOCUMENTS33T

33T2.1 General 33T2.2 Government Documents 33T2.2.1 Specifications, Standards, and Handbooks 33T2.2.1.133T 33TMilitary Standards33T 33T2.2.1.233T 33TMilitary Specifications 33T 33T2.2.1.333T 33TMilitary Handbooks33T 33T2.2.2 Other Government Documents, Drawings, and Publications 33T2.3 Other Documents 33T2.4 Order of Precedence

33T3.033T 33TREQUIREMENTS33T

33T3.1 General Bomber Armament Tester System Requirements 33T3.1.1 General System Design 33T3.1.2 Applicability 33T3.1.333T 33TModular Open System Architecture33T 33T3.1.433T 33TGovernment Data Rights33T 33T3.1.533T 33TMarkings 33T 33T3.1.633T 33TIdentification Plate33T 33T3.1.733T 33TWorkmanship33T 33T3.1.833T 33TForeign Object Damage Prevention33T 33T3.1.933T 33TEnclosures33T 33T3.1.1033T 33TColor 33T 33T3.1.1133T 33TCable Design33T 33T3.1.11.133T 33TConnector Selection33T 33T3.1.11.233T 33TConnector Finish33T 33T3.1.11.333T 33TConnector Keying33T 33T3.1.11.433T 33TWire Shields 33T 33T3.1.11.533T 33TShield Insulation33T 33T3.1.11.633T 33TShield Bonding33T 33T3.1.11.733T 33TSafety Ground Conductor33T 33T3.1.11.833T 33TCable Crosstalk Mitigation33T 33T3.1.11.933T 33TProtective Caps33T 33T3.1.11.1033T 33TConnector Positioning33T 33T3.1.11.1133T 33TConnector Population33T 33T3.1.1233T 33TPower 33T

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33T3.1.12.133T 33TOperating Power 33T 33T3.1.12.233T 33TMaster Power Switch33T 33T3.1.12.333T 33TPower Cable Length33T 33T3.1.12.433T 33TUnit Under Test Power 33T 33T3.1.12.533T 33TPower Consumption (Key Performance Parameter)33T 33T3.1.12.633T 33TCircuit Breakers 33T 33T3.1.12.733T 33TPower Monitoring33T 33T3.1.1333T 33TGrounding33T 33T3.1.13.133T 33TControlled Grounding Concept 33T 33T3.1.13.233T 33TShock Protection33T 33T3.1.13.333T 33TGround Loop Prevention33T 33T3.1.13.433T 33TExternal Safety Ground33T 33T3.1.1433T 33TGraphical Display 33T 33T3.1.14.133T 33TGraphical Display Size33T 33T3.1.14.233T 33TGraphical Display Readability33T 33T3.1.14.333T 33TGraphical User Interface33T 33T3.1.14.433T 33TUser Navigation33T 33T3.1.1533T 33THuman Factors33T 33T3.1.15.133T 33TOperability with Chemical Warfare Gear33T 33T3.1.15.233T 33TTransportability33T 33T3.1.15.333T 33TEdges and Corners33T 33T3.1.15.433T 33TMoving Parts33T 33T3.1.1633T 33TEnvironmental33T 33T3.1.16.133T 33TSolar Radiation33T 33T3.1.16.233T 33TElectromagneitc Interference33T 33T3.1.16.333T 33TExplosive Atmosphere33T 33T3.1.16.433T 33TAltitude33T 33T3.1.16.533T 33TDrip Proof 33T 33T3.1.16.633T 33TAcoustic Noise33T 33T3.1.16.733T 33TCorrosion Prevention33T 33T3.1.1733T 33TNuclear Certification (Key Performance Parameter)33T 33T3.1.17.133T 33TSystem Safety33T 33T3.1.17.233T 33TSingle Failures33T 33T3.1.17.333T 33TDual Failures33T 33T3.1.17.433T 33TDesign Safety – Critical Functions33T 33T3.1.17.533T 33TDesign Safety – Internal Faults33T 33T3.1.17.633T 33TDesign Safety – Unintended Signals33T 33T3.1.17.733T 33TDesign Safety – Unintended Firing33T 33T3.1.17.833T 33TTest Safety – End of Test 33T 33T3.1.1833T 33TTest Safety – System Failures33T 33T3.1.1933T 33TElectromagnetic Environmental Effects Requirements33T 33T3.1.2033T 33TCyber Security (Key Performance Parameter)33T 33T3.1.20.133T 33TUser Auditing33T 33T3.1.20.233T 33TSoftware Non-Repudiation33T 33T3.1.20.333T 33TEndpoint Security33T 33T3.1.20.433T 33TSystem Administration33T

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33T3.1.20.533T 33TConfiguration Auditing33T 33T3.1.20.633T 33TMalware Alerting33T 33T3.1.20.733T 33TWireless Network33T 33T3.1.20.833T 33TData at Rest Encryption33T 33T3.1.20.933T 33TSystem Recovery33T 33T3.1.2133T 33TBAT Core Tester Self-Test/Built In Test (Key Performance Parameter)33T 33T3.1.21.133T 33TPower-On Confidence Test 33T 33T3.1.21.233T 33TSelf-Test 33T 33T3.1.21.333T 33TSelf-Test Data33T 33T3.1.21.433T 33TSelf-Test Fault Detection33T 33T3.1.21.533T 33TSelf-Test Execution Time33T 33T3.1.21.633T 33TSelf-Test Fault Isolation Rate – 1 Component 33T 33T3.1.21.733T 33TSelf-Test Fault Isolation Rate – 2 Components33T 33T3.1.21.8 Self-Test Fault Isolation Rate – 3 Components 33T3.2 System Capability 33T3.2.1 Modular Open System Architecture 33T3.2.1.1 Open System Architecture Design 33T3.2.1.2 Test Program Set Software Architecture 33T3.2.1.333T 33TOperating System Architecture33T 33T3.2.1.433T 33TTest Executive Software Architecture33T 33T3.2.1.533T 33TMemory Capacity33T 33T3.2.1.633T 33TMemory Usage33T 33T3.2.1.733T 33TProcessor Usage33T 33T3.2.233T 33TSuitability Requirements33T 33T3.2.2.133T 33TMaintainability33T 33T3.2.2.2 Reliability 33T3.3 Test Program Set Requirements 33T3.3.1 Unit Under Test Data Log 33T3.3.2 Real Time Display of Test Results and Status 33T3.3.333T 33TEnd of Test Report 33T 33T3.3.433T 33TSafe-To-Turn-On Test33T 33T3.3.533T 33TTest Sequencing33T 33T3.3.633T 33TTest Termination33T 33T3.3.733T 33TTest Entry Points33T 33T3.3.833T 33TManual Test Sequencing33T 33T3.3.933T 33TTest Control Selection33T 33T3.3.1033T 33TTest Data Transfer 33T 33T3.3.1133T 33TClearing Test Data33T 33T3.3.1233T 33TPre-Test External Cable Identification33T 33T3.3.1333T 33TStray Voltage Test 33T 33T3.3.1433T 33TUnit Under Test Fault Detection33T 33T3.3.1533T 33TUnit Under Test Cooling33T 33T3.3.1633T 33TInterface Test Adapters33T 33T3.4 Aircraft Unique Requirements 33T3.4.1 B-2A Unique Requirements 33T3.4.1.1 Rotary Launcher AssemblyTests (Key Performance Parameter)

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33T3.4.1.233T 33TRotary Launch Assembly Line Replaceable Unit Bench Check33T 33T3.4.1.333T 33TBRU-44 Operational Test Standalone Backshop (Key Performance Parameter)33T 33T3.4.1.433T 33TSmart Bomb Rack Assembly Test Backshop (Key Performance Parameter)33T 33T3.4.1.533T 33TBRU-52 Operational Test Backshop (Key Performance Parameter) 33T 33T3.4.1.633T 33TSmart Bomb Rack Controller Test Backshop33T 33T3.4.1.733T 33TMonitor And Control Equipment and BRU-72 Carriage And Release Equipment Test 33T 33T3.4.1.833T 33TStores Management System Test On Aircraft Only (Key Performance Parameter)33T 33T3.4.233T 33TB-1B Unique Requirements33T 33T3.4.2.133T 33TB-1B Weapon Carriage Systems33T 33T3.4.2.233T 33TB-1B Aircraft Weapons Delivery System (Key Performance Parameter)33T 33T3.4.2.333T 33TFault Isolate to an Line Replaceable Unit 33T 33T3.4.2.433T 33T14 Inch Ejector Rack Backshop Test (Key Performance Parameter)33T 33T3.4.2.533T 33T30 Inch Ejector Rack Backshop Test (Key Performance Parameter)33T 33T3.4.2.633T 33TMAU-12 Ejector Rack Backshop Test (Key Performance Parameter)33T 33T3.4.333T 33TB-52H Unique Requirements33T 33T3.4.3.133T 33TConventional Rotary Launcher Test 33T 33T3.4.3.233T 33TWiring Tests (Key Performance Parameter)33T 33T3.4.3.333T 33TBackshop Tests33T 33T3.4.3.433T 33TMAU-12 Ejector Rack Backshop Test (Key Performance Parameter)33T 33T3.4.3.533T 33TB-52H Unique Testing Times33T

33T4.033T 33TVERIFICATION33T

33T4.1 General Information 33T4.1.1 Responsibility for Verification 33T4.1.2 Verification Methods 33T4.1.3 Final Acceptance 33T4.2 Verification of General System Requirements 33T4.2.1 Verification of General System Design 33T4.2.233T 33TVerification of Applicability 33T 33T4.2.333T 33TVerification of Modular Open System Architecture33T 33T4.2.433T 33TVerification of Markings33T 33T4.2.533T 33TVerification of Identification Plate33T 33T4.2.633T 33TVerification of Workmanship33T 33T4.2.733T 33TVerification of Foreign Object Damage Prevention33T 33T4.2.833T 33TVerification of Enclosures33T 33T4.2.933T 33TVerification of Color 33T 33T4.2.1033T 33TVerification of Cable Design33T 33T4.2.10.133T 33TVerification of Connector Selection33T 33T4.2.10.233T 33TVerification of Connector Finish33T 33T4.2.10.333T 33TVerification of Connector Keying33T 33T4.2.10.433T 33TVerification of Wire Shields 33T 33T4.2.10.533T 33TVerification of Shield Insulation33T 33T4.2.10.633T 33TVerification of Shield Bonding33T

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33T4.2.10.733T 33TVerification of Safety Ground Conductor 33T 33T4.2.10.833T 33TVerification of Cable Crosstalk Mitigation33T 33T4.2.10.933T 33TVerification of Protective Caps33T 33T4.2.10.1033T 33TVerification of Connector Positioning33T 33T4.2.10.1133T 33TVerification of Connector Population33T 33T4.2.1133T 33TVerification of Power 33T 33T4.2.11.133T 33TVerification of Operating Power 33T 33T4.2.11.233T 33TVerification of Master Power Switch33T 33T4.2.11.333T 33TVerification of Power Cable Length33T 33T4.2.11.433T 33TVerification of Unit Under Test Power 33T 33T4.2.11.533T 33TVerification of Power Consumption33T 33T4.2.11.633T 33TVerification of Circuit Breakers 33T 33T4.2.11.733T 33TVerification of Power Monitoring33T 33T4.2.1233T 33TVerification of Grounding33T 33T4.2.12.133T 33TVerification of Controlled Grounding Concept 33T 33T4.2.12.233T 33TVerification of Shock Protection33T 33T4.2.12.333T 33TVerification of Ground Loop Prevention33T 33T4.2.12.433T 33TVerification of External Safety Ground33T 33T4.2.1333T 33TVerification of Graphical Display 33T 33T4.2.13.133T 33TVerification of Graphical Display Size33T 33T4.2.13.233T 33TVerification of Graphical Display Readability33T 33T4.2.13.333T 33TVerification of Graphical User Interface33T 33T4.2.13.433T 33TVerification of User Navigation33T 33T4.2.1433T 33TVerification of Human Factors33T 33T4.2.14.133T 33TVerification of Operability with Chemical Warfare Gear33T 33T4.2.14.233T 33TTransportability33T 33T4.2.14.333T 33TVerification of Edges and Corners33T 33T4.2.14.433T 33TVerification of Moving Parts33T 33T4.2.1533T 33TVerification of Environmental33T 33T4.2.15.133T 33TVerification of Solar Radiation33T 33T4.2.15.233T 33TVerification of Electromagnetic Interference33T 33T4.2.15.333T 33TVerification of Explosive Atmosphere33T 33T4.2.15.433T 33TVerification of Altitude33T 33T4.2.15.533T 33TVerification of Drip Proof 33T 33T4.2.15.633T 33TVerification of Acoustic Noise33T 33T4.2.15.733T 33TVerification of Corrosion Prevention33T 33T4.2.1633T 33TVerification of Nuclear Certification/System Safety 33T 33T4.2.16.133T 33TVerification of System Safety33T 33T4.2.16.233T 33TVerification of Single Failures33T 33T4.2.16.333T 33TVerification of Dual Failures33T 33T4.2.16.433T 33TVerification of Design Safety – Critical Functions33T 33T4.2.16.533T 33TVerification of Design Safety – Internal Faults33T 33T4.2.16.633T 33TVerification of Design Safety – Unintended Signals33T 33T4.2.16.733T 33TVerification of Design Safety – Unintended Firing33T 33T4.2.16.833T 33TVerification of Test Safety – End of Test33T 33T4.2.1733T 33TVerification of Test Safety – System Failures33T

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33T4.2.1833T 33TVerification of Electromagnetic Environmental Effects Requirements33T 33T4.2.1933T 33TVerification of Cyber security33T 33T4.2.19.133T 33TVerification of User Auditing33T 33T4.2.19.233T 33TVerification of Software Non-Repudiation33T 33T4.2.19.333T 33TVerification of Endpoint Security33T 33T4.2.19.433T 33TVerification of System Administration33T 33T4.2.19.533T 33TVerification of Configuration Auditing33T 33T4.2.19.633T 33TVerification of Malware Alerting33T 33T4.2.19.733T 33TVerification of No Wireless Network 33T 33T4.2.19.833T 33TVerification of Data at Rest Encryption33T 33T4.2.19.933T 33TVerification of System Recovery33T 33T4.2.2033T 33TVerification of Tester Self-Test/ Built In Test 33T 33T4.2.20.133T 33TVerification of Power-On Confidence Test 33T 33T4.2.20.233T 33TVerification of Self-Test 33T 33T4.2.20.333T 33TVerification of Self-Test Data33T 33T4.2.20.433T 33TVerification of Self-Test Failure Detection33T 33T4.2.20.533T 33TVerification of Self-Test Execution Time33T 33T4.2.20.633T 33TVerification of Self-Test Fault Isolation Rate – 1 Component 33T 33T4.2.20.733T 33TVerification of Self-Test Fault Isolation Rate – 2 Components33T 33T4.2.20.8 Verification of Self-Test Fault Isolation Rate – 3 Components 33T4.3 System Capability 33T4.3.1 Modular Open System Architecture 33T4.3.1.1 Verification of Open System Architecture Design 33T4.3.1.233T 33TVerification of Test Program Set Software Architecture33T 33T4.3.1.333T 33TVerification of Operating System Architecture33T 33T4.3.1.433T 33TVerification of Test Executive Software Architecture33T 33T4.3.1.533T 33TVerification of Memory Capacity33T 33T4.3.1.633T 33TVerification of Memory Usage33T 33T4.3.1.733T 33TVerification of Processor Usage33T 33T4.3.233T 33TVerification of Suitability Requirements33T 33T4.3.2.133T 33TVerification of Maintainability33T 33T4.3.2.2 Verification of Reliability Requirements 33T4.4 Verification of Test Program Set Requirements 33T4.4.1 Verification of Unit Under Test Data Log 33T4.4.2 Verification of Real Time Display of Test Results and Status 33T4.4.333T 33TVerification of End of Test Report 33T 33T4.4.433T 33TVerification of Safe-To-Turn-On Test 33T 33T4.4.533T 33TVerification of Test Sequencing33T 33T4.4.633T 33TVerification of Test Termination33T 33T4.4.733T 33TVerification of Test Entry Points33T 33T4.4.833T 33TVerification of Manual Test Sequencing33T 33T4.4.933T 33TVerification of Test Control Selection33T 33T4.4.1033T 33TVerification of Test Data Transfer33T 33T4.4.1133T 33TVerification of Clearing of Test Data33T 33T4.4.1233T 33TVerification of Pre-Test External Cable Identification33T 33T4.4.1333T 33TVerification of Stray Voltage Test 33T

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33T4.4.1433T 33TVerification of Unit Under Test Fault Detection33T 33T4.4.15 Verification of Unit Under Test Cooling Cart Interface 33T4.4.16 Verification of Interface Test Adapters 33T4.5 Verification of Aircraft Unique Requirements 33T4.5.1 Verification of B-2A Unique Requirements 33T4.5.2 Verification of B-1B Unique Requirements 33T4.5.333T 33TVerification of B-52H Unique Requirements33T

33T5.033T 33TPACKAGING 33T

33T5.1 Packaging / Handling / Storage / Transportation

33T6.033T 33TNOTES33T

33T6.1 Intended Use 33T6.2 Acquisition Requirements 33T6.3 Acronyms 33TAPPENDIX A: UUT REFERENCE DOCUMENTS33T ........................................................A1

1.0 SCOPE

1.1 Scope

This specification establishes the performance requirements for the Bomber Armament Tester (BAT) System, hereafter referred to as the BAT. This specification shall be used for contractual purposes in the procurement of the BAT and establishes the minimum performance parameters.

This document describes the functional and interface characteristics of the BAT and the verification required to demonstrate the achievement of those specified characteristics and performance parameters.

1.1.1 Requirement Levels

This specification lists two values for certain performance parameters. The threshold (T) is the minimum acceptable level. The objective (O) is the desired level at which performance of the BAT results in an operationally significant increase in capabilities. When only one requirement value is stated, it is the threshold requirement. All Key Performance Parameters (KPPs) must be met for program success.

1.1.2 Bomber Armament Tester Definition

The “BAT System” is hereby defined as: consisting of the common core tester and the Units Under Test (UUT) Test Program Sets (TPSs) required to support respective B-2A, B-1B, or B- 52H weapon systems. The BAT “Core Tester” includes hardware, operating system software, firmware, test executive software, power-on confidence test TPS, user-selectable self-test TPS, and calibration TPS. A UUT TPS includes all cables, Interface Test Adapters (ITAs), software, and technical documentation needed to test a UUT.

The BAT System shall be a versatile, adaptable, common tester featuring modular, open system architecture which can be easily modified and updated to resolve obsolescence or support future requirements. The BAT shall provide organizational level, on and off-equipment capability to support fault detection/isolation and diagnostics of UUTs to identify system or component malfunction to the appropriate faulty Line Replaceable Unit (LRU) for the armament systems UUTs.

The BAT System shall certify the operational readiness of bomber weapon suspension and release equipment, which includes nuclear weapon delivery capability. The BAT shall support B-2A, B-1B, and B-52H organizational level stores station maintenance (on-aircraft) and back-shop armament system component maintenance (off-aircraft).

1.2 Unit Under Test

The following sections provide lists of the B-1B, B-2A, and B-52H armament systems UUTs that shall be supported by the BAT System.

1.2.1 B-2A Armament System Units Under Tests

UUT NAME NIIN PART NO.

Rotary Launcher Assembly (RLA) (Nuclear item; see

MNCL)

01-600-0627 DAA3510A001-101

Nuclear Weapon Control Monitor (NWCM, NWIU) 01-435-0603, 01-435-0141

DAA3383E040-117,

DAA3383E040-119

Bomb Status Relay Assembly (BSRA) 01-435-1816 DAA3383E080-107 Missile Status Relay Assembly (MSRA) 01-435-0605 DAA3383E090-109 Ejector Relay Assembly (ERA) 01-315-6294 DAA3383E100-103 Transformer Rectifier Unit (TRU) 01-315-6293 DAA3383P033-107 Bomb Ejector Rack Unit 44 (BRU-44B/A) 01-511-0578 6127100-02 , Boeing p/n

464-55605-1 Bomb Ejector Rack Unit 52 (BRU-52/A37B-1B5) 01-381-5850 DAA3529A047-001 Smart Bomb Rack Assembly (SBRA) A/A 37B-1B5 01-519-6360 DAA3520A001-011, DAA3520A001-013

Monitor and Control Equipment (MACE) 01-597-1730 DAF3520A500-001 Smart Bomb Rack Controller (SBRC) - part of MACE 01-513-9507, 01-597-3119 70P993000-1013, 70P993000-1017

Bomb Rack Unit 72/B (BRU-72) Carriage and Release Equipment (CARE) - for MOP

01-596-7293 464-95813-9

Junction Box Assembly (JBA), Forward CARE N/A 464-19252-1 Junction Box Assembly (JBA), Aft CARE N/A 464-58563-1 On aircraft tests (SMS harness connectivity test) N/A N/A

Table 1-1 B-2A UUTs

1.2.2 B-1B Armament System Units Under Tests

UUT NAME NIIN PART NO.

Multi-Purpose Rotary Launcher (MPRL) 01-613-2984 L6316202-041/43999 Rack, Bomb Ejector, 30 Inch (BRU-56/A) 01-412-0831 L6410301-081 Conventional Bomb Module (CBM) 28 station 01-323-9577 L6317301-031/43999 Rack, Bomb Ejector, 14 Inch 01-423-8778 L6314201-061, L6314202-041 1760 Enhanced Conventional Bomb Module (SECBM) 10 station

01-592-8399 L6317801-011/43999

Common Weapons Interface Unit (CWIU) 01-488-4261 400-17165-114 Ejector Rack, MAU-12D/A 01-398-7497 69J13060-9 On aircraft test (Weapons Delivery System) N/A N/A

Table 1-2 B-1B UUTs

1.2.3 B-52H Armament System Units Under Tests

UUT NAME NIIN PART NO.

Ejector Rack, MAU-12C/A 01-100-3892 69J13060-7 Ejector Rack, MAU-12D/A 01-398-7497 69J13060-9 Pylon Assy., B-52 Integrated Conventional Weapons NA 398-10652-25, ‘-26, ‘-27, ‘-28 Bomb Release and Arming Control (R/H and L/H) 00-475-2437

00-475-2436 68J34000R-01, 68J34000L-01

Conventional Rotary Launcher (CRL) 1760 N/A 405-22003*

Cluster Bomb Rack (CBR) 00-219-3641 5-69557-1, ‘-505, ‘-507, ‘- 508, ‘-509

On aircraft testing (SMS testing) N/A N/A On aircraft testing (SUU 67 pylon disconnect) N/A N/A *Note: Part number 405-22003-1 for CRL is preliminary and dash number may change.

Table 1-3 B-52H UUTs

2.0 APPLICABLE DOCUMENTS

2.1 General

While every effort has been made to ensure the completeness of this list, users are cautioned that they shall meet all specified requirements of documents cited in section 3 of this specification, whether or not they are listed. The documents listed in sections 2.2 and 2.3 are referenced in section 3 of this specification.

2.2 Government Documents

2.2.1 Specifications, Standards, and Handbooks

The following specifications, standards, and handbooks form a part of this document to the extent specified herein. Unless otherwise specified, the versions of these documents are cited in the solicitation or contract. Documents can be accessed through Defense Logistic Agency ASSIST quick search web application 33TUhttp://quicksearch.dla.mil U33T/.

2.2.1.1 Military Standards

MIL-STD-882 Department of Defense Standard Practice: System Safety Rev. E 11 May 2012

MIL-STD-461 Department of Defense Interface Standard Requirements Rev. F 10 Dec 2007 for the Control of Electromagnetic Interference

MIL-STD-464 Department of Defense Interface Standard Electromagnetic Rev. C 1 Dec 2010 Environmental Effects Requirements For Systems

MIL-STD-1472 Department of Defense Design Criteria Standard Rev. G 11 Jan 2012 Human Engineering

MIL-STD-1553B Department of Defense Interface Standard for Digital Notice 4 15 Jan 1996 Time Division Command/Response Multiplex Data Bus

MIL-STD-1686 Electrostatic Discharge Control Program for the Protection Rev. C 25 Oct 1995 of Electrical and Electronic Parts, Assemblies and

Equipment (Excluding Electrically Initiated Explosive Devices)

MIL-STD-1760E Department of Defense Interface Standard Aircraft/Store Notice 1 24 Oct 2007 Electrical Interconnection System http://quicksearch.dla.mil/

MIL-STD-810G Department of Defense Test Method Standard for Notice 1 15 Apr 2014 Environmental Engineering Considerations and Laboratory Tests

MIL-STD-130N Identification Marking of U.S. Property Change 1 16 Nov 2012

MIL-STD-704F Department Of Defense Interface Standard: Aircraft Notice 2- Validation Electric Power 25 Oct 2013

MIL-STD-1366E Transportability Criteria 31 Oct 2006

MIL-STD-1568C Materials and Processes for Corrosion Prevention and 12 Aug 2014 Control in Aerospace Weapons Systems

MIL-STD-2073-1E(1) Standard Practice for Military Packaging 07-Jan-2011

MIL-STD-3018 Parts Management Change 2 02 June 15

2.2.1.2 Military Specifications

MIL-DTL-38999 Connector, Electrical, Circular, Miniature High Density, Rev. M Supplement 1 Quick Disconnect (Bayonet Threaded and Breech 11 Feb 2015 Coupling), Environment Resistant, Removable Crimp and Hermetic Solder Contracts, General Specification for

MIL-P-15024/5 Plates, Tags and Bands for Identification of Equipment 21 Apr 2014

MIL-PRF-28800 Test Equipment for use with Electrical and Electronic Rev. F 24 Jun 1996 Equipment, General Specification for

MIL-PRF-32070A Performance Specification for Test Program Sets Rev. A 10 Jan 2012

MIL-PRF-39019F Circuit Breakers, Magnetic, Low-Power Sealed, Trip-Free NOTICE 1 General Specification for 13 Feb 2015

MIL-STD-1332B Definitions of Tactical, Prime, Precise, and Utility NOTICE 2 Terminologies for Classification of the DoD Mobile 10 July 2001 Electric Power Engine Generator Set Family

2.2.1.3 Military Handbooks

MIL-HDBK-189 Department of Defense Handbook Reliability Growth Rev. C 14 Jun 2011 Management

MIL-HDBK-217F Reliability Prediction for Electronic Equipment Change Notice 2 28 Feb 1995

MIL-HDBK-419A Grounding, Bonding and Shielding for Electronic Change Notice 1 28 Feb 1995 Equipments and Facilities, (Handbook Contains both Volume I Basic Theory, and Volume II Applications)

MIL-HDBK-454B General Guidelines for Electronic Equipment Notice 1 12 Dec 2012

2.2.2 Other Government Documents, Drawings, and Publications

The following other government documents, drawings, and publications form a part of this document to the extent specified herein. Unless otherwise specified, documents listed in Appendix A UUT Reference Data are provided for reference only. Appendix A Reference Data is provided with no guarantee of completeness, accuracy or currency.

AFMAN 91-118 Safety Design and Evaluation Criteria for Nuclear Weapon 28 July 2015 Systems

AFMAN 91-119 Safety Design and Evaluation Criteria for Nuclear Weapon 05 Jun 2012 Systems Software

AFI 91-107 Design, Evaluation, Troubleshooting, and Maintenance 11 Dec 2012 Criteria for Nuclear Weapon Systems

CNSSI No. 1253 Security Categorization and Control 27 Mar 2014 Selection for National Security Systems

DoDI 8500.01 and .02 Cyber Security 14 Mar 2014

DoDI 8510.01 Risk Management Framework (RMF) for DoD Information 12 Mar 2014 Technology (IT)

FED-STD-595C Colors Used for Government Procurement 595C Change Notice 1 31 Jul 2008

Specification Standard Basic Interface Specification, System 1 No. SYS 1001-02 1 July 2008

Specification Standard System 2 Basic Interface Specification No. SYS 2001-04A

AMAC POG SYS 2

11 Dec 2012

TO 00-25-234 General Shop Practice Requirements for the Repair, Change 1 Maintenance, and Test of Electrical Equipment 23 March 2014

TO 1-1A-14 Installation and Repair Practices Volume 1 Aircraft Electric 15 April 2014 and Electronic Wiring

2.3 Other Documents

IEEE 1636.1-2013 IEEE Standard for Software Interface for Maintenance Information Collection and Analysis (SIMICA):

Exchanging Test Results and Session Information via the eXtensible Markup Language (XML)

ISO 7779:2010 Acoustics -- Measurement of airborne noise emitted by information technology and telecommunications equipment

2.4 Order of Precedence

In the event of a conflict between the text of this specification and the references cited herein the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained.

3.0 REQUIREMENTS

3.1 General Bomber Armament Tester System Requirements

3.1.1 General System Design

The BAT System shall be designed in accordance with (IAW) MIL-PRF-28800F, Test Equipment for use with Electrical and Electronic Equipment, General Specification for Class 1.

3.1.2 Applicability

The BAT System shall be designed to test all of the UUTs listed in Tables 1-1, 1-2, and 1-3. The BAT Core Tester shall contain the functions such as a system controller, analog and digital stimulus, measurement, signal switching, power and Input/Output devices, and software necessary to test the UUTs listed in Tables 1-1, 1-2, and 1-3.

3.1.3 Modular Open System Architecture

The BAT System shall be based on a Modular Open System Architecture (MOSA) design per paragraph 3.2.1.

3.1.4 Government Data Rights

All hardware, software, firmware, software development environments, and technical data items delivered under this contract shall be delivered with Government Purpose Rights at a minimum so that the BAT System can be maintained, sustained, modified, re-used, or re-procured by 3rd parties of the governments’ choosing after this contract is concluded. This includes the rights to use, modify, reproduce, release, perform, display, or disclose technical data within the Government without restriction and to release or disclose technical data outside the Government and authorize persons to whom release or disclosure has been made to use, modify, reproduce, release, perform, display, or disclose that data for United States government purposes.

All software executables and source code developed by the contractor for the BAT System shall be property of the government for unlimited use. This includes BAT Core Tester software, TPS, and qualification software. BAT Core Tester software is defined as the operating system software, firmware, power-on confidence test software, self-test software, calibration software (if calibration required), test executive software, system recovery and/or security software required to meet cybersecurity requirements. The deliverables shall be addressed by Contract Data Requirements Lists (CDRL).

Freeware shall not be used in the design, development, or production of the BAT system, and shall not be incorporated into any of the software deliverables of the BAT system. Freeware is defined as free software which is copyrighted by its developer, who retains the rights to control its distribution, modify it and sell it in the future.

For any and all commercial software used on the BAT System that requires a license, the license “key” shall not be hardware based (i.e. USB-based dongle key). The ability to utilize any and all commercial software shall not require any additional hardware to verify possession of appropriate and corresponding license(s), nor require any recurring license fees for continued use of and reinstallation of the existing software configuration. All licenses shall be “royalty-free,” worldwide, irrevocable and non-exclusive.

3.1.5 Markings

All external devices which require an operational or maintenance interface shall be marked IAW MIL-STD-130. Painted markings shall be 1-inch high block letters unless prohibited by the available space. In such cases the markings shall be the largest size possible but shall not be less than 1/2-inch high. Markings, Information/Caution shall be Lusterless Black Color Number

37038 of FED-STD-595 and Markings, Warning/Danger shall be Lusterless Red Color Number 31136 of FED-STD-595.

3.1.6 Identification Plate

The system end items shall be properly identified IAW MIL-STD-130.

3.1.7 Workmanship

MIL-HDBK 454 Guideline 9 shall be used as a guide to workmanship.

3.1.8 Foreign Object Damage Prevention

All parts and components shall be securely attached to prevent loss and to prevent Foreign Object Damage (FOD) to the B-2A, B-1B, and B-52H aircraft as well as the BAT System or any other equipment.

3.1.9 Enclosures

Enclosures for the BAT System and cables/accessories shall be designed IAW MIL-PRF- 28800F. Accessory enclosures shall prevent cable bends beyond manufacturer specification in storage.

3.1.10 Color

Exterior color shall be color number 26173 (grey) as defined by FED-STD-595.

3.1.11 Cable Design

Cables shall be designed to tolerate 90-degree flexing imposed by the weight of themselves during use, over their service life without damage to the internal wiring, cable exterior, connectors, or connector/cable interface IAW MIL-PRF-32070A. The cable branching limit imposed by MIL-PRF-32070A paragraph 3.4.4.2 is waived. The number of cable branches and connectors shall be minimized while optimizing size, weight, sustainment considerations and TPS run-time.

3.1.11.1 Connector Selection

Connectors shall be selected using MIL-DTL-38999 and shall utilize environmentally sealed connectors with crimp style pins. Connectors that are not MIL-DTL-38999 compliant shall require government approval.

3.1.11.2 Connector Finish

Connectors used to terminate shields shall have a conductive finish.

3.1.11.3 Connector Keying

Connectors shall be keyed to prevent inadvertent application or use unless prevented by UUT.

3.1.11.4 Wire Shields

Except for coaxial cables, wire shields, shall not be used as a return nor shall they be used to conduct power.

3.1.11.5 Shield Insulation

A layer of insulation shall cover all wire shields.

3.1.11.6 Shield Bonding

Overall cable shields shall be terminated at a connector backshell that provides peripheral bonding of the shield.

3.1.11.7 Safety Ground Conductor

All power cables shall have a safety ground conductor IAW MIL-STD-464 and MIL-HDBK- 419A.

3.1.11.8 Cable Crosstalk Mitigation

Cables shall be designed to prevent crosstalk.

3.1.11.9 Protective Caps

Cables shall have a protective end-cap permanently attached by a lanyard and shall be ruggedized.

3.1.11.10 Connector Positioning

Cable connectors shall be positioned to mitigate strain and to facilitate ease of installation and/or removal without incurring ancillary accommodations (e.g., disconnection or removal of adjacent cables).

3.1.11.11 Connector Population

To provide structural integrity when seating connectors, cable connectors shall be completely filled with pins and sockets.

3.1.12 Power

3.1.12.1 Operating Power

The BAT System shall be capable of operating from 28 VDC and 120/240 VRMS 50 Hz, 60 Hz, and 400 Hz AC (single and multi-phase). Operating power shall comply with the requirements listed in MIL-PRF-28800F, MIL-STD-704F and MIL-STD-1332B. Automatic and operator initiated shutdown shall provide an orderly, sequential system shutdown to preclude damage to the Automatic Test Equipment (ATE) or UUT and shall not degrade the ATE hardware or software.

Operating power for the BAT computer/controller shall have the capability of being isolated from the test power being used to power the UUTs.

3.1.12.2 Master Power Switch

The BAT System shall be equipped with a master power On/Off switch with an indicator lamp.

3.1.12.3 Power Cable Length

Power cable length shall be sufficient to enable UUT testing to be performed without repositioning tester, for all test points on a given UUT for on and off aircraft testing.

3.1.12.4 Unit Under Test Power

The BAT System shall be capable of switching external power as required by the UUT. The BAT System shall control on/off switching of power to the UUT as required by the UUT TPS.

Operating power for the BAT computer/controller shall have the capability of being isolated from the test power being used to power the UUTs.

3.1.12.5 Power Consumption (Key Performance Parameter)

The BAT Core Tester, excluding the UUT, shall consume no more than 1.3 kW for operation of internal stimulus and measurement devices.

3.1.12.6 Circuit Breakers

The BAT System shall have circuit breakers with manual reset capability accessible to the maintainer IAW MIL-PRF-39019F. Circuit breakers shall not be capable of being manually over ridden during an over current condition.

3.1.12.7 Power Monitoring

The BAT System shall measure and report input power, VRMS for each phase, phase sequence, and frequency information to the operator as follows:

a. As part of the power up sequence.

b. At the start of all test sequences.

c. During each step while the test load is still connected. Report as part of the data for each failure, or for each step if in manual mode.

The BAT System shall detect and respond to the presence of more than 6 VRMS between the Neutral and Chassis Ground as follows:

a. If during power up, notify the operator of a power fault and prevent the BAT Core Tester power up sequence.

b. If during operation, notify the operator and perform an orderly shutdown.

3.1.13 Grounding

3.1.13.1 Controlled Grounding Concept

A controlled grounding concept shall be used so that grounding will not adversely impact the functional testing/operation of the UUT. This concept shall provide for a single point ATE signal ground as well as a single point safety ground IAW the guidelines of MIL-HDBK-419A.

3.1.13.2 Shock Protection

The grounding scheme for the BAT System shall provide protection of personnel and equipment from electrical shock hazards during normal operations and under ground fault conditions.

3.1.13.3 Ground Loop Prevention

The BAT System shall be designed to eliminate ground loops and minimize common ground impedance which can degrade system noise margins.

3.1.13.4 External Safety Ground

The BAT System shall provide an external safety ground stud or bar.

3.1.14 Graphical Display

3.1.14.1 Graphical Display Size

The display shall be adequately sized to clearly show at a minimum all applicable information as defined in specification paragraph 3.3.2 (e.g., status, menus, test data, fault codes, messages, etc.)

in a manner that is easily readable by the user. The display shall meet the requirements of MIL- STD-1472G section 5.2.

3.1.14.2 Graphical Display Readability

The display shall be readable in all lighting conditions, including full daylight ambient conditions; direct sunlight; and night time IAW MIL-STD-1472G section 5.2. The brightness setting shall not allow the display to "black-out".

3.1.14.3 Graphical User Interface

The BAT System graphical user interface functions shall enable the operator to interact with the test system, to include but not be limited to, enabling TPS diagnostic advancement and/or referral to alternate test instructions, explanations and/or troubleshooting trees; authentication;

test instruction initiation and/or termination; and test result save commands as necessary to achieve UUT test requirements.

3.1.14.4 User Navigation

The BAT System shall provide controls to allow the operator to move between pages of display information, between selection options, and selection of a menu item/option.

3.1.15 Human Factors

3.1.15.1 Operability with Chemical Warfare Gear

The BAT System shall be capable of being operated and decontaminated by personnel in Mission Oriented Protective Posture (MOPP) Level 4 Chemical Warfare Defense Ensemble (CWDE) IAW MIL-STD-1472G section 4.10.

3.1.15.2 Transportability

3.1.15.2.1 Weight

The contractor shall strive to minimize the size, weight and total number of transit cases of the overall system without adversely affecting performance. The BAT system footprint for the B-2A aircraft shall not exceed that of the current legacy tester(s) and cable sets being replaced by the BAT for testing B-2A armament. The BAT system footprint for the B-1B aircraft shall not exceed that of the current legacy tester(s) and cable sets being replaced by the BAT for testing B- 1B armament. The BAT system footprint for the B-52H aircraft shall not exceed that of the current legacy tester(s) and cable sets being replaced by the BAT for testing B-52H armament.

The weight of the BAT Core tester including tester power cables and self-test cables or of any one accessory container for the BAT system shall not exceed a two-person lift to 36 inches as defined for the “Male only” population per MIL-STD-1472G, Section 5.8.6.3.1 (T) with an objective of a two-person lift to 36 inches as defined for the “Male and female” population per MIL-STD-1472G, Section 5.8.6.3.1 or less (O).

The BAT Core tester may be packaged in up to 2 transit cases. If the BAT Core tester is packaged in two transit cases, the weight of each transit case shall not exceed a one person lift to 36 inches as defined for the “Male only” population per MIL-STD-1472G, Section 5.8.6.3.1 (T) with an objective of a one-person lift to 36 inches as defined for the “Male and female” population per MIL-STD-1472G, Section 5.8.6.3.1 or less (O).

3.1.15.2.2 Handles

The system shall be provided with recessed and/or foldable handles or other suitable means for grasping, handling, and carrying IAW MIL-STD-1472G.

3.1.15.3 Edges and Corners

The BAT System shall include provisions for smooth edges/corners, prevent accidental contact with high and low surface temperatures, and provide pinch point prevention, IAW MIL-STD- 1472G.

3.1.15.4 Moving Parts

All moving/mechanical parts shall be inaccessible to the operator during system operation to prevent inadvertent contact (e.g., cooling fan).

3.1.16 Environmental

The BAT System shall conform to the performance specified herein when subjected to the environmental conditions as specified in MIL-PRF-28800F paragraph 3.8 for Class 1 equipment.

Deviations from and clarifications of MIL-PRF-28800F (detail specification references) are specified in the following paragraphs.

3.1.16.1 Solar Radiation

In addition to the temperature requirements specified in MIL-PRF-28800F, the BAT System shall meet High Temperature with Solar Radiation per requirements defined in MIL-STD-810G Method 505.5 Procedure I in a simulated Hot Dry (A1) climate. The BAT shall be in operational configuration and shall be required to successfully pass system self-test as well as a simulation of typical steady state loading and use of stimulus and measurement devices as anticipated for the most strenuous and lengthy B-2A UUT TPS, during the maximum BAT System temperature response period of the exposure cycle.

3.1.16.2 Electromagnetic Interference

The BAT System shall be Electromagnetic Interference (EMI) qualified IAW the following emission and susceptibility requirements from MIL-STD-461F, section 5.3, Table V for Air Force Ground equipment.

TABLE 3-1 EMI REQUIREMENTS

MIL-STD-461F

Requirement

Description

CE102 Conducted Emissions, Power Leads, 10 kHz to 10 MHz CS101 Conducted Susceptibility, Power Leads, 30 Hz to 50 KHz CS114 Conducted Susceptibility, Bulk Cable Injection, tailored to 10 kHz to

200MHz CS115 Conducted Susceptibility, Bulk Cable Injection, impulse excitation CS116 Conducted Susceptibility, Damped Sinusoidal Transients, cables and power leads, 10 kHz to 100 MHz RE102 Radiated Emissions, Electric Field, 10 k Hz to 18 GHz RS103 Radiated Susceptibility, Electric Field, 2 MHz to 40 GHz

3.1.16.3 Explosive Atmosphere

The BAT System shall be designed to be Explosive Atmosphere Qualified per MIL-STD-810G, Method 511.6, Procedure I. The BAT System design shall have the ability to operate in a fuel vapor environment without igniting the environment.

3.1.16.4 Altitude

The BAT System shall conform to the specified performance and accuracy requirements when operated at an altitude 15,000 feet (4,600 meters) or less IAW MIL-STD-810G Method 500.5 Procedure II (operating configuration), and after return from an altitude of 40,000 feet, IAW MIL-STD-810G Method 500.6 Procedure III (storage/transit configuration).

3.1.16.5 Drip Proof

The BAT System shall comply with the drip proof requirements of MIL-PRF-28800F paragraph

3.8.6.3. MIL-PRF-28800F Paragraphs 3.8.6.1 and 3.8.6.2 do not apply to the BAT System.

3.1.16.6 Acoustic Noise

Acoustic noise requirements shall be as specified in MIL-PRF-28800F paragraph 3.8.12. The BAT System shall not generate acoustic noise in excess of 70 dBA sound pressure level (SPL) when measured at the operator and bystander positions, IAW ISO 7779.

3.1.16.7 Corrosion Prevention

The BAT System shall be constructed of parts and materials that are corrosion and deterioration resistant, or coated to resist corrosion and deterioration, IAW MIL-STD-1568C.

3.1.17 Nuclear Certification (Key Performance Parameter)

3.1.17.1 System Safety

System safety for the BAT System shall be conducted IAW the requirements of MIL-STD-882E.

The BAT System design shall be compliant with requirements defined by AFMAN91-118 and

AFMAN91-119.

3.1.17.2 Single Failures

The BAT System shall be designed such that no single component failure, common mode failure, human error, or a design feature shall cause a mishap of Catastrophic or Critical mishap severity categories as defined in MIL-STD-882E.

3.1.17.3 Dual Failures

The BAT System shall be designed such that no dual independent component failures, dual independent human errors, or a combination of a component failure and a human error involving safety critical command and control functions, shall cause a mishap of Catastrophic or Critical mishap severity categories.

3.1.17.4 Design Safety – Critical Functions

The BAT System design shall prevent faults in the test equipment or test circuits that could operate critical functions or apply unintended power to the weapon interface.

3.1.17.5 Design Safety – Internal Faults

The BAT System design shall prevent internal faults within the tester that could degrade the nuclear or conventional safety of the equipment to be tested.

3.1.17.6 Design Safety – Unintended Signals

The BAT System design shall prevent the introduction of signals, voltages, or currents into the weapon system that could degrade nuclear or conventional safety of the equipment to be tested.

3.1.17.7 Design Safety – Unintended Firing

The BAT System shall prevent operation or firing of an item under test, except when specifically designed for that purpose.

3.1.17.8 Test Safety – End of Test

The BAT System shall ensure a weapon system component, which has been operated during testing, is in the safe or inactivated position when the test ends. A positive indication verifies the safe position of such components.

3.1.18 Test Safety – System Failures

The BAT System failures or shutdowns shall leave the components under test in a safe or inactivated condition. The BAT System shall provide a clear indication of UUT failure status.

3.1.19 Electromagnetic Environmental Effects Requirements

The BAT System shall be compatible with ordnance classified as Hazards of Electromagnetic Radiation to Ordnance (HERO) SAFE ORDNANCE IAW the requirements of MIL-STD-464C, section 5.9.3, Table 9.

3.1.20 Cyber Security (Key Performance Parameter)

a. The BAT System shall maintain a mission effective capability in the face of a full spectrum of cyber threats.

b. The BAT System design shall implement cyber security IAW DoDI 8500.01, DoDI 8500.02, DoDI 8510.01, and CNSSI No. 1253. If a commercial operating system is used, the applicable Defense Information Systems Agency (DISA) developed Security Technical Implementation Guide shall be implemented.

c. The requirements listed in 3.1.20.1 through 3.1.20.9 shall be implemented in the design to minimize the impact on operational and maintenance procedures in the flight line environment.

3.1.20.1 User Auditing

The BAT System shall incorporate an electronic auditing trail that unambiguously identifies and records the initiating user of the operational test or any log-on event. This includes auditing the installation of BAT System Software, Test Program Sets, and Firmware as applicable.

3.1.20.2 Software Non-Repudiation

All BAT System Software, TPSs, and firmware created, delivered, and installed shall utilize non-repudiation techniques to guarantee the integrity and origin of the System Software, TPSs and firmware throughout the entire System Software, TPSs and firmware lifecycle.

3.1.20.3 Endpoint Security

The BAT System shall only include necessary and functional information data ports to interface with authorized data-transfer media. Data ports will be disabled when not in use.

3.1.20.4 System Administration

The BAT System shall deny software configuration changes for all but administrator user accounts. The operating system, test executive, and TPS software shall only be capable of being loaded by those users who have administrator privileges. The BAT System shall permit only authorized software code to execute on the system.

3.1.20.5 Configuration Auditing

The BAT System shall perform a configuration audit during system start to identify malware or unauthorized changes to the approved configuration.

3.1.20.6 Malware Alerting

The BAT System shall notify the user of any detected malware or unauthorized changes and not allow activation of the test connections if malware is detected during system start up as defined in 3.1.21.1 of this specification.

3.1.20.7 Wireless Network

Wireless network hardware, software, and firmware shall not be present within the BAT Core Tester.

3.1.20.8 Data at Rest Encryption

The BAT System shall encrypt all data at rest on the nonvolatile storage media used to boot the BAT system as well as store operating system, test executive and Test Program Sets.

3.1.20.9 System Recovery

The BAT Core Tester shall be capable of being recovered to a known clean state by the system administrator from any cyber security incident.

3.1.21 BAT Core Tester Self-Test/Built In Test (Key Performance Parameter) The BAT Core Tester Self-Test/Built in Test (BIT) shall be designed IAW MIL-PRF-32070A.

If faults are discovered, the core tester’s functional status shall be displayed to the user and shall not require the use of external technical manuals to determine functional status.

3.1.21.1 Power-On Confidence Test

The BAT Core Tester shall provide a Power-On Confidence Test to ensure proper operation prior to initiation/stimulation of UUT test. The Power-On Confidence Test shall be automatically performed upon BAT System power-up and shall include running the malware detection defined in 3.1.20.6 of this specification. Power-On Confidence test shall be completed in 10 minutes or less (T) with an objective of 2 minutes (O).

3.1.21.2 Self-Test

The BAT Core Tester shall have an integrated Self-Test capability for failure detection and fault isolation of all system components, and shall provide indications of out of range conditions of the tester. The Self-Test shall ensure that stimulus and measurement devices are operating within tolerance. Self-Test shall run upon system start up and when manually commanded by the user. Self-Test during TPS execution shall not be enabled.

3.1.21.3 Self-Test Data

The BAT Core Tester on-board fault and Self-Test data shall be collected, stored, and provided IAW IEEE 1636.1 compatible formats to maintenance personnel during and after maintenance operations.

3.1.21.4 Self-Test Fault Detection

The BAT Core Tester Self-Test shall detect 100 percent of detectable faults. A detectable fault is a failure of a Tester Replaceable Unit (TRU) that is exhibited at the interface of the TRU and is outside the defined performance parameter or threshold for that particular function.

3.1.21.5 Self-Test Execution Time

The BAT Core Tester Self-Test execution time shall be no longer than 10 minutes (T) with an objective of 1 minute (O).

3.1.21.6 Self-Test Fault Isolation Rate – 1 Component

The BAT Core Tester Self-Test shall isolate at least 90% of detected faults to a single system component (e.g.: tester unit, interface unit, cable number/connector number/pin number, software, etc.)

3.1.21.7 Self-Test Fault Isolation Rate – 2 Components

The BAT Core Tester Self-Test shall isolate at least 95% of detected faults to two system components (e.g.: tester unit, interface unit, cable number/connector number/pin number, software, etc.)

3.1.21.8 Self-Test Fault Isolation Rate – 3 Components

The BAT Core Tester Self-Test shall isolate 100% of detected faults to three system components (e.g.: tester unit, interface unit, cable number/connector number/pin number, software, etc.) or less.

3.2 System Capability

3.2.1 Modular Open System Architecture

3.2.1.1 Open System Architecture Design (MOSA)

The BAT System shall feature a MOSA design. In satisfying the Government’s requirements, the following system architecture design characteristics shall be utilized:

a. Open Architecture – The contractor shall develop and maintain an architecture that incorporates appropriate considerations for re-configurability, portability, maintainability, technology insertion, vendor independence, reusability, scalability, interoperability, upgradeability, and long-term supportability.

b. Modular, Open Design – The contractor shall develop an architecture that is layered and modular and uses standards-based hardware interfaces, operating systems, and middleware that all utilize either non-proprietary or non-vendor-unique key module or component interfaces. The contractor’s design approach shall be applied to all subsystems and components.

i. Module Coupling – The contractor’s design approach shall result in…