RFP Attachment 3_STATEMENT OF OBJECTIVES.pdf

Statement of Objectives – Common Armament Tester – Fighter (CAT-F)

COMMON ARMAMENT TESTER – FIGHTER (CAT-F)

STATEMENT OF OBJECTIVES (SOO)

Prepared by:

AFMC AFLCMC/ROA ATS Program Office

Robins AFB, Georgia

I. Purpose The Government requires a common armament tester to execute both flightline and backshop requirements prioritizing the F-16 first, followed by F-15 then A-10 fighter fleets. The Government’s primary objective is t h e development, manufacture, deployment, and sustainment of a Common Armament Tester for Fighter (CAT-F). The CAT-F will be used at both Organizational (O-LVL) and Intermediate (I-LVL) Level maintenance. The tester shall be able to execute preload, clean wing, and fault isolation armament requirements and replace, or augment, legacy testers for the F-16, F-15, A10.

The CAT- F shall be cyber secure, nuclear certified and use a Modular Open System Architecture approach. The program will require industry to utilize a CAT-F specific Government Reference Architecture (GRA). The CAT-F acquisition will also be a solution for Diminishing Manufacturing Sources and Materiel Shortages (DMSMS) and Obsolescence Issues across several legacy testers.

The Government is providing industry with the overall solicitation objectives which allow flexibility for each offeror to propose an innovative development approach to achieve the Government’s CAT-F requirements. Offerors shall use the Statement of Objectives (SOO) and attachments with the Request for Proposal (RFP) as a basis for preparing their proposal. Proposals shall include a contractor Statement of Work (SOW) and expected Contract Data Requirements Lists (CDRLs). Proposals shall also include an Integrated Master Schedule (IMS) that indicates their schedule to design, manufacture, and deliver a CAT-F solution for the F-16, F-15, and A-10 platforms.

II. CAT-F Scope The “CAT-F System” is defined as an O-Level (Flightline) an I-Level (Backshop) tester.

The CAT-F System will be comprised of components with each component requiring kitting designed for safe storage and rapid deployment.

The required components are:

• O-Level Handheld tester

• Aircraft Specific O-Level Cable and Adapter Kit

• I-Level Functional and Fault Isolation tester

• Aircraft Specific I-Level Cable and Adapter Kit

III. O-Level Handheld Tester The CAT-F O-Level Handheld tester must be able to execute legacy O-Level Maintenance (Flightline) Pre-load and Clean Wing requirements for the F-16, F-15, and A-10 fighter aircraft. The Handheld Tester must work independently to execute O-Level test requirements and store testing results. The test results shall be compatible with I- Level Functional and Fault Isolation Tester results. The offeror shall propose a prototype plan that details how the offeror will modify a Non-Developmental Item (NDI) to meet a Critical Design Review (CDR) of the O-Level Handheld Tester within 10 months of contract award.

IV. Aircraft Specific O-Level Cable and Adapter Kit The Cable/Adapter Test Program Set (TPS) Kit is expected to be aircraft specific and contain all-appropriate cables and adapters needed to execute pre-load and clean wing testing required at O- Level Maintenance.

V. I-Level Functional and Fault Isolation Tester The CAT-F I-Level Functional and Fault Isolation Tester must be able to execute legacy I-Level (Backshop) requirements for the F-16, F-15, and A-10 fighter aircraft and shall incorporate the O-Level Handheld tester in its design.

VI. Aircraft Specific I-Level Cable and Adapter Kit The Cable/Adapter TPS Kit is expected to be aircraft specific and contain the appropriate cables and adapters needed to execute Fault Isolation requirements at I-Level Maintenance.

VII. CAT-F Component Quantities The expected component quantities listed are based on current fleet status and may be adjusted to meet future Force Structure Changes. This will be an Indefinite Delivery, Indefinite Quantity contract (IDIQ). Table 1.0 indicates the Governments estimated component quantities.

Table 1. CAT-F Estimated Component Quantities

CAT-F Components F-16 F-15 A-10 O-Level Handheld Testers 303 172 68 O-Level Cable and Adapter Kits 303 172 68 I-Level Functional/Fault Isolation Testers 143 80 42 I-Level Cable and Adapter Kits 143 80 42

VIII. Product Support / Logistics Considerations

• The solution considers commercial and equipment that will expedite development, production, and fielding

• Solution that reduces legacy equipment footprint and being able to deploy worldwide

• Provide equipment solutions that deliver a reliable option and minimize the potential for DMSMS

• Describe the Modular Open System Approach (MOSA) approach to deliver CAT-F capability

• Intellectual Property (IP) considerations, to include technical data package deliverables and rights to use the same, must account for the Government’s CAT-F life cycle objectives, including the availability of non-proprietary software code, open and competitive CAT-F enhancements, and approaches for providing unimpeded, innovative, and cost-effective production, operation, maintenance, and upgrades.

IX. Period of Performance (PoP) The period of performance will be a one (1) year Basic with four (4) one-year Options.

X. Contractor Statement of Work (SOW) Offeror shall develop a SOW using the SOW template (SOO Attachment 5). The SOW must clearly indicate the work to complete the CAT-F with detailed tasks, technical requirements, and recommended program deliverables.

XI. Integrated Master Schedule (IMS) The offerors are expected to develop and provide a time-based Integrated Master Schedule (IMS) with the proposal, detailing the tasks, key milestones, phased approach, and delivery dates necessary to ensure successful program/contract execution. The IMS should be traceable to the offer’s developed Contractor SOW. The Offeror’s submitted IMS shall address all 5 contract years. DI-MGMT-81861C, Integrated Program Management Data and Analysis Report (IPMDAR)

XII. Surge Capability Plan The offeror shall propose a Surge capability plan that details its minimum and maximum ability to satisfy a surge production requirement.

STATEMENT OF OBJECTIVES (SOO) Attachments:

Attachment 1: SYSTEM REQUIREMENT DOCUMENT (SRD) Attachment 2: F-16/F-15/A-10 ALTERNATE MISSION EQUIPMENT (AME) Attachment 3: CAT-F AME MAINTENANCE LEVEL REQUIREMENTS Attachment 4: REQUIRED CONTRACT DATA REQUIREMENTS LIST ITEMS Attachment 5: STATEMENT OF WORK (SOW) TEMPLATE

ATTACHMENT 1:

SYSTEM REQUIREMENT DOCUMENT (SRD)

Prepared by:

ATS Engineering Office

AFMC AFLCMC/ROA ATS Program Office Robins AFB, Georgia

The Common Armament Tester for Fighter (CAT-F) System Requirement Document (SRD) defines the system-level functional and performance requirements for a common armament tester for multiple fighter Aircraft. The SRD is derived from the CAT-F Capability Development Document (CDD) and Concept of Operations (CONOPS), system-level performance metrics.

Id Name Description Verification Method SRD_1 System Requirements SRD_1.1 Required States and Modes The Testers non-operational and operational modes are defined below:

a. Non-Operational modes including the tester’s system storage and system transportation, if applicable.

b. Operational modes include Tester Maintenance and Unit Under Test (UUT)/Device Under Test (DUT) Testing. The Tester maintenance modes consist of System Administration activities supporting software updates and approved user access, Tester Self-Test and Tester Calibration.

Demonstration

SRD_1.1.1 Tester Self-Test/Built-In Test The Tester Self-Test/Built in Test (BIT) shall be designed in accordance with MIL-PRF-32070.

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.

Analysis

SRD_1.1.1.1 Power-On Confidence Test The 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 system power-up and shall include running the malware detection defined in

1.10.2.3 of this specification. Power-On Confidence test shall be completed in 10 minutes or less

(T) with an objective of 2 minutes (O).

Threshold: 10 minutes Objective: 2 minutes

Analysis Demonstration

SRD_1.1.1.2 Self-Test The 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. Self-Test may require the use of appropriate cables/accessories from the TPS Kit.

Demonstration

SRD_1.1.1.2.1 Self-Test Data The Tester on-board fault and Self-Test data shall be collected, stored, and provided IAW IEEE 1636, IEEE 1636.1, and IEEE 1636.2 compatible formats to maintenance personnel during and after maintenance operations.

Demonstration

SRD_1.1.1.2.2 Self-Test Execution Time The Tester Self-Test execution time shall be no longer than 10 minutes (T) with an objective of 1 minute (O).

Threshold: 10 minutes Objective: 1 minute

Demonstration

SRD_1.1.1.2.3 Self-Test Fault Detection The 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 function.

Analysis

SRD_1.1.1.2.4 Self-Test Fault Isolation Rate – 1 Component

The 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.)

Threshold: 90% Objective: 95%

Analysis

SRD_1.1.1.2.5 Self-Test Fault Isolation Rate – 2 Components

The 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.)

Threshold: 95% Objective: 100%

Analysis

SRD_1.1.1.2.6 Self-Test Fault Isolation Rate – Components

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

Analysis

SRD_1.1.2 Test Program Set Requirements

All armament UUT TPSs developed for use by the Tester shall be designed IAW MIL-PRF- 32070.

Analysis

SRD_1.1.2.1 Unit Under Test Data Log and

Documentation The Tester software shall collect, store, and provide upon command, the following data in compliance with IEEE-STD-1636.1 for future export:

General Information UUT Serial Number

a. Installed LRU serial numbers if applicable (A UUT for test purposes may contain other subassemblies which are themselves UUTs and separately serial numbered)

b. Tester serial number

c. Operator and date

d. Computer Program Identification Number (CPIN)

e. Checksum/Signature of CPIN to indicate Software unaltered

f. Tester Self-Test Status

g. Total Test Time

h. Overall UUT status (Pass/Fail) For each test sequence in the TPS

i. Upper tolerance value

j. Measured value

k. Lower tolerance value

l. Expected digital data

m. Received digital data word, in both actual state and in “layman’s terms”

n. Power Quality Information in accordance with paragraph 3.3.3.7.

o. Time Stamp

p. Indictments (or callouts) determined through fault isolation to include Failed Connector and Pin and input Connector/Pin(s). Information shall be traceable to the test program.

q. Number of times an individual test sequence was run The Tester shall retain the UUT test data log after an incomplete test or test termination.

Analysis

SRD_1.1.2.2 Real Time Display of Test Results and Status

The Tester shall provide real-time test status to the operator:

a. UUT Serial Number

b. CPIN Number

c. Test Number being executed

d. Upper tolerance value

e. Measured value

f. Lower tolerance value

g. 1553 status

h. External Elapsed Time Indicator

i. Expected digital data

j. Received digital data in both actual state and in “layman’s terms”

k. Recommended Failure Modes e.g. call out most common LRU, Cable etc. Failed Connector and Pin and input Connector/Pin(s)

l. Measurement values for loop back tests and adjustments

Analysis

SRD_1.1.2.3 End of Test Report At the conclusion of TPS execution, the Tester shall display and log a test report for indicating the pass/fail status and certifying the functionality of the UUT.

Analysis

SRD_1.1.2.4 Safe-To-Turn-On Test The UUT TPSs shall perform safe-to-turn-on tests prior to executing the TPS IAW MIL-PRF- 32070A.

Analysis

SRD_1.1.2.5 Test Sequencing The UUT TPSs shall automatically sequence through all test steps pausing only when operator input is required, when operator manually aborts test sequence, when a failure is detected, or until all test steps are successfully completed. Upon failure of a test step or the operator manually aborting the test sequence, the Tester shall display the fault data and allow the operator to retest the failed step, continue testing, or discontinue testing.

Analysis

SRD_1.1.2.6 Test Termination The UUT TPSs shall provide a termination feature to perform an orderly termination of a test in progress (i.e., terminate external interfaces) leaving both the Tester and UUT in a safe state.

SRD_1.1.2.7 Test Entry Points The Tester shall allow the operator to select and run test sequences from operator selectable entry points. At a minimum, entry points shall provide autonomous groups of tests based on UUT functionality. Test Entry Points shall provide the capability for the operator to select and execute testing of specific functional areas of the UUT individually and separate from other functional areas, as well as complete end-to-end testing. UUT certification shall require an end-to-end go chain.

Analysis

SRD_1.1.2.8 Manual Test Sequencing Manual test sequencing shall perform one test step in the sequence and pause for the operator to initiate the next step.

Analysis

SRD_1.1.2.9 Test Control Selection Selection between automatic and manual test control shall be available, except when prohibited due to sequencing and/or timing requirements for tests.

Analysis

SRD_1.1.2.10 Test Data Transfer The Tester shall provide a cyber‐secure compliant capability to transfer test data to an approved external device through an existing secure data port when commanded by the administrator.

Analysis

SRD_1.1.2.11 Clearing Test Data The Tester shall have the capability to clear non‐volatile memory and test data when commanded by an administrator.

Analysis

SRD_1.1.2.12 Pre‐Test External Cable Identification Cable and Cable Testing

The Tester shall verify the external cable configuration/hookup prior to the start of any test. The Tester shall notify the operator of any incorrect cable configurations prior to the start of any test.

The Tester shall prevent test initiation when cables are incorrectly configured. The Tester shall test all Test Program Hardware to include Interface Test Adapters (ITA) and ITA cables as part of the UUT TPS IAW MIL‐PRF‐32070A paragraph 3.3.6.

Analysis

SRD_1.1.2.13 Stray Voltage Test The Tester shall be capable of detecting stray voltage, as required prior to munitions load. Analysis SRD_1.1.2.14 Unit Under Test Fault

Detection The Tester shall detect 100 percent of detectable faults of system LRU failures, based on the available data offered by on‐aircraft or off‐aircraft equipment. A detectable fault is a failure of the UUT that is exhibited at the interface of the UUT and is outside the defined performance parameter or threshold for that particular function.

Analysis

SRD_1.1.2.15 Unit Under Test Cooling UUT cooling carts may be required for some UUT testing. Analysis SRD_1.1.2.16 Interface Test Adapters TPS ITAs shall not utilize active circuit components without prior Government approval. Analysis SRD_1.1.2.17 Functional and Parametric Test

Data Functional and Parametric data for both instruments and test stations should be formatted IAW ATML standards specified in IEEE 1671.2, IEEE 1871.1, as well as IEEE 1671.6 and 1871.2 respectively.

Analysis

SRD_1.1.2.18 Test Configuration Information documenting the test configuration utilized during the testing of any particular UUT (to include information regarding the tested UUT, the test equipment, and the TPS) shall be developed IAW IEEE 1671.4 ATML Test Configuration.

Analysis

SRD_1.1.2.19 Receiver Adapter Interface The Receiver Adapter Interface present within the Tester shall be developed IAW IEEE 1641 Annex K.

Analysis

SRD_1.1.2.20 UUT Test Requirements and Product Design Data

UUT Test Requirements and Product Design Data shall be defined and designed respectively IAW IEEE 1671.1 ATML Test Description, as well as ANSI/EIA 682, Electronic Design Interchange Format (EDIF), and IEEE 1671.3 ATML UUT Description.

Analysis

SRD_1.1.2.21 Digital Test Interchange Format

Interchangeable data present within the Tester shall be formatted IAW IEEE 1445 Digital Test Interchange Format (DTIF).

Analysis

SRD_1.1.2.22 Test Program Documentation All documentation referring to the Test Programs shall be developed IAW IEEE P1671.1 ATML Test Description, and IEEE 1671 Annex C.2 ATML WirelistSchema.

Analysis

SRD_1.1.2.23 Design for Testability Designs for Testability will be created IAW IEEE 1149.1 Test Access Port and Boundary-Scan Architecture, IEEE 1149.4 Mixed Signal Test Bus, and IEEE 1149.6 Boundary-Scan Testing of Advanced Digital Networks.

Analysis

SRD_1.1.2.24 Adapter Functional and Parametric Data

Adapter Functional and Parametric Data shall be IEEE 1671.5 ATML Test Adapter, and IEEE

1871.2 Recommended Practice for Intrinsic Signal Path Information.

SRD_1.1.2.25 Test Duration Total test time using the Common Handheld Tester and the Preload TPS/Kit (O-level MDS specific) shall be less than the current duration of all comparable operational and/or functional testing. The O-LVL 180-day testing time will not exceed 6 Hours and all testing at I-LVL will be under 1 hour per AME.

Threshold: O-LVL 180-day testing time will not exceed 6 hours and all testing at I-LVL will be under 1 hour per AME.

Objective: O-LVL 180-day testing time will not exceed 4.5 hours and all testing at I- LVL will be under 45 minutes per AME.

Test

SRD_1.1.2.26 Software Developer’s Guide The contractor shall develop the CAT-F TPS style guide. Inspection SRD_1.2 Legacy Testing The CAT-F shall be capable of performing all current legacy armament system tests and meet required nuclear certification. The CAT-F will replace multiple current USAF fighter aircraft armament testers and shall execute all legacy inspection and troubleshooting requirements. The tester will be required to conduct armament preload and fault isolation testing on active model versions of the F-16 and F-15 fleets. This tester should be considered as a replacement armament tester for the A-10 fleet and be a future consideration for newer generation fighters. To verify the requirement, the CAT-F will be tested in all operationally representative environments and on all appropriate fighter aircraft. The results will be compared to the appropriate legacy tester.

Test

SRD_1.2.1 A-10 AME The tester shall be able to execute all A-10 AME requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.1.1 Stations 1 and 11 Pylon (with MAU-50 installed)

The tester shall be able to execute all Stations 1 and 11 Pylon (with MAU-50 installed) requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.1.2 Stations 2 and 10 Pylon (with MAU-50 installed)

The tester shall be able to execute all Stations 2 and 10 Pylon (with MAU-50 installed) requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.1.3 Stations 3 & 9 Pylon (with MAU-40 installed

The tester shall be able to execute all Stations 3 & 9 Pylon (with MAU-40 installed requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.1.4 Stations 4 & 8 Pylon (with MAU-40 installed)

The tester shall be able to execute all Stations 4 & 8 Pylon (with MAU-40 installed) requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.1.5 Station 5 Pylon (with MAU-40 installed)

The tester shall be able to execute all Station 5 Pylon (with MAU-40 installed) requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.1.6 Station 6 Pylon (with MAU-40 installed)

The tester shall be able to execute all Station 6 Pylon (with MAU-40 installed) requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.1.7 Station 7 Pylon (with MAU-40 installed)

The tester shall be able to execute all Station 7 Pylon (with MAU-40 installed) requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.1.8 TER-9/A or Variant installed The tester shall be able to execute all TER-9/A or Variant installed requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.1.9 Dual Rail Adaptor (DRA) with LAU-105s and LAU-128 installed

The tester shall be able to execute all Dual Rail Adaptor (DRA) with LAU-105s and GMIU installed requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.1.10 LAU-131 The tester shall be able to execute all LAU-131 requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.1.12 LAU-117 The tester shall be able to execute all LAU-117 requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.1.13 BRU-61 The tester shall be able to execute all BRU-61 requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.1.14 LAU-88 The tester shall be able to execute all LAU-88 requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.1.15 Gun Control Unit The tester shall be able to execute all Gun Control Unit requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.1.16 Pylon SCU-A/SCU-B The tester shall be able to execute all Pylon SCU-A/SCU-B requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.1.17 AN/ALE-47 CMDS The tester shall be able to execute all AN/ALE-47 CMDS requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.1.18 LAU-128 The tester shall be able to execute all LAU-128 requirements IAW the specific MDS Technical

Orders.

Demonstration

SRD_1.2.2 F-15 AME The tester shall be able to execute all F-15 AME requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.2.1 PYLON The tester shall be able to execute all PYLON requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.2.2 BRU-46/47 The tester shall be able to execute all BRU-46/47 requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.2.3 BRU-61 The tester shall be able to execute all BRU-61 requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.2.4 CBU-103, 105, 107, 118

System Check

The tester shall be able to execute all CBU-103, 105, 107, 118 System Check requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.2.5 GBU-31 (JDAM) System Check

The tester shall be able to execute all GBU-31 (JDAM) System Check requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.2.6 GUB-31B UAI System Check The tester shall be able to execute all GUB-31B UAI System Check requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.2.7 M-61A1 The tester shall be able to execute all M-61A1 requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.2.8 AIm-9M Missile System The tester shall be able to execute all AIm-9M Missile System requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.2.9 GBU-38 UAI/GBU-54 UAI

System Check

The tester shall be able to execute all GBU-38 UAI/GBU-54 UAI System Check requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.2.10 AGM-158 UAI System Check The tester shall be able to execute all AGM-158 UAI System Check requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.2.11 AIM-9X/X-2 Missile System The tester shall be able to execute all AIM-9X/X-2 Missile System requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.2.12 AIM-120 LAU-106 Missile System

The tester shall be able to execute all AIM-120 LAU-106 Missile System requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.2.13 AIM-120 LAU-128 Missile System

The tester shall be able to execute all AIM-120 LAU-128 Missile System requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.2.14 Jettison Checks Without Fuel Tanks

The tester shall be able to execute all Jettison Checks Without Fuel Tanks requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.2.15 Jettison Checks With Fuel Tanks

The tester shall be able to execute all Jettison Checks With Fuel Tanks requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.2.16 BRU-46/47 Single Carriage (Pylon)

The tester shall be able to execute all BRU-46/47 Single Carriage (Pylon) requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.2.17 BRU-47 The tester shall be able to execute all BRU-47 requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.2.18 SUU-20 The tester shall be able to execute all SUU-20 requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.2.19 MAU-12 The tester shall be able to execute all MAU-12 requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.2.20 LAU-128 (AIM-9L/M) The tester shall be able to execute all LAU-128 (AIM-9L/M) requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.2.21 LAU-128 (AIM-120) The tester shall be able to execute all LAU-128 (AIM-120) requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.2.22 LAU-120 (AIM-120) The tester shall be able to execute all LAU-120 (AIM-120) requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.2.23 GBU-39 UAI System Check The tester shall be able to execute all GBU-39 UAI System Check requirements IAW the specific MDS Technical orders.

Demonstration

SRD_1.2.2.24 GBU-53 UAI System Check The tester shall be able to execute all GBU-53 UAI System Check requirements IAW the specific MDS Technical orders.

Demonstration

SRD_1.2.2.25 Multipurpose Booster (MPB) UAI System Check

The tester shall be able to execute all MPB UAI System Check requirements IAW the specific MDS Technical orders.

SRD_1.2.2.26 ALE-58A System Check The tester shall be able to execute all ALE-58A System Check requirements IAW the specific

MDS Technical orders.

Demonstration

SRD_1.2.2.27 SUU-60B/A The tester shall be able to execute all SUU-60B/A requirements IAW the specific MDS Technical orders.

Demonstration

SRD_1.2.2.28 SUU-59B/A The tester shall be able to execute all SUU-59B/A requirements IAW the specific MDS Technical orders.

Demonstration

SRD_1.2.2.29 SUU-59C/A The tester shall be able to execute all SUU-59C/A requirements IAW the specific MDS Technical orders.

Demonstration

SRD_1.2.2.30 SUU-73/A The tester shall be able to execute all SUU-73/A System Check requirements IAW the specific MDS Technical orders.

Demonstration

SRD_1.2.2.31 Missile Launcher Auxiliary Relay Panel Check

The tester shall be able to execute all Missile Launcher Auxiliary Relay Panel Check requirements IAW the specific MDS Technical orders.

Demonstration

SRD_1.2.2.32 IRST Pod System Check The tester shall be able to execute all IRST Pod System Check requirements IAW the specific MDS Technical orders.

Demonstration

SRD_1.2.2.33 B61 UAI System Check The tester shall be able to execute all B-61 UAI System Check requirements IAW the specific MDS Technical orders.

Demonstration

SRD_1.2.3 F-16 AME The tester shall be able to execute all F-16 AME requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.1 Preload Functional Checks, 75060 Replacement Tests, Pre-Block Aircraft

The tester shall be able to execute all Preload Functional Checks, 75060 Replacement Tests, Pre-Block Aircraft requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.1.1 MAU-12 on Aircraft The tester shall be able to execute all MAU-12 on Aircraft requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.1.2 External Fuel Tank Pylon on Aircraft

The tester shall be able to execute all External Fuel Tank Pylon on Aircraft requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.1.4 LAU-129 Missile Launcher on Aircraft

The tester shall be able to execute all LAU-129 Missile Launcher on Aircraft requirements IAW the specific MDS Technical Orders, in addition to performing full Mid-body umbilical checkout as defined in the SST Technical Orders.

Demonstration

SRD_1.2.3.1.5 TER-9A on Aircraft The tester shall be able to execute all TER-9A on Aircraft requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.1.6 On Aircraft Launcher Umbilical Only

The tester shall be able to execute all On Aircraft Launcher Umbilical Only requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.1.7 SUU-20 on Aircraft The tester shall be able to execute all SUU-20 on Aircraft requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.1.8 M61A1 20mm Gun System Control Circuits / Gun Control Unit (GCU)

The tester shall be able to execute all M61A1 20mm Gun System Control Circuits / Gun Control Unit (GCU) requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.1.9 On Aircraft WWP 1760 Umbilical Only

The tester shall be able to execute all On Aircraft WWP 1760 Umbilical Only requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.1.10 SCRIU Equipped WWP The tester shall be able to execute all SCRIU Equipped WWP requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.1.11 BRU-57 on Aircraft The tester shall be able to execute all BRU-57 on Aircraft requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.2 Preload Functional Checks- 75060 Replacement Tests, Post-Block Aircraft

The tester shall be able to execute all Preload Functional Checks-75060 Replacement Tests, Post-Block Aircraft requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.2.1 MAU-12 on Aircraft The tester shall be able to execute all MAU-12 on Aircraft requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.2.2 External Fuel Tank Pylon on Aircraft

The tester shall be able to execute all External Fuel Tank Pylon on Aircraft requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.2.3 TER-9A on Aircraft The tester shall be able to execute all TER-9A on Aircraft requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.2.5 LAU-129 Missile Launcher on Aircraft

The tester shall be able to execute all LAU-129 Missile Launcher on Aircraft requirements IAW the specific MDS Technical Orders, in addition to performing full Mid-body umbilical checkout as defined in the SST Technical Orders.

SRD_1.2.3.2.6 LAU-118 Missile Launcher on

Aircraft The tester shall be able to execute all LAU-118 Missile Launcher on Aircraft requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.2.7 On Aircraft Launcher Umbilical Only LAU-117

The tester shall be able to execute all On Aircraft Launcher Umbilical Only LAU-117 requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.2.8 On Aircraft Launcher Umbilical only LAU 118 Launcher

The tester shall be able to execute all On Aircraft Launcher Umbilical only LAU 118 Launcher requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.2.9 On Aircraft Rocket Launcher Umbilical only

The tester shall be able to execute all On Aircraft Rocket Launcher Umbilical only requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.2.10 SUU-20 on Aircraft The tester shall be able to execute all SUU-20 on Aircraft requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.2.11 M61A1 20MM Gun System Control Circuits / Gun Control Unit (GCU)

The tester shall be able to execute all M61A1 20MM Gun System Control Circuits / Gun Control Unit (GCU) requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.2.12 On Aircraft WWP, 1760 Umbilical Only

The tester shall be able to execute all On Aircraft WWP, 1760 Umbilical Only requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.2.13 BRU-57 on Aircraft The tester shall be able to execute all BRU-57 on Aircraft requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.2.14 Under Wing Adapter The tester shall be able to execute all Under Wing Adapter requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.2.15 ALE-50 Pylon on Aircraft The tester shall be able to execute all ALE-50 Pylon on Aircraft requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.2.16 BRU-46 on Aircraft The tester shall be able to execute all BRU-46 on Aircraft requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.2.17 Left Hardpoint Interface The tester shall be able to execute all Left Hardpoint Interface requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.2.18 Right Hardpoint Interface The tester shall be able to execute all Right Hardpoint Interface on Aircraft requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.3 O Level Stores System Tester (SST) - Replacement Tests

The tester shall be able to execute all O Level Stores System Tester (SST) - Replacement Tests requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.3.1 Aircraft station 1, 2, 3A, 7A, 8 and 9 interface connection circuits

The tester shall be able to execute all Aircraft station 1, 2, 3A, 7A, 8 and 9 interface connection circuits requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.3.2 Aircraft station 3, 4, 6 and 7 interface connection circuits

The tester shall be able to execute all Aircraft station 3, 4, 6 and 7 interface connection circuits requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.3.3 Aircraft station 5 (centerline station) interface connection circuits Pre ASQ-236 Modifications

The tester shall be able to execute all Aircraft station 5 (centerline station) interface connection circuits Pre ASQ-236 Modifications requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.3.4 Aircraft station 5 (centerline station) interface connection circuits Post ASQ-236 Modifications

The tester shall be able to execute all Aircraft station 5 (centerline station) interface connection circuits Post ASQ-236 Modifications requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.3.5 ASQ-236 Centerline Pylon on Aircraft, station 5

The tester shall be able to execute all ASQ-236 Centerline Pylon on Aircraft, station 5 requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.3.6 Centerline Pylon on Aircraft, station 5

The tester shall be able to execute all Centerline Pylon on Aircraft, station 5 requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.3.8 LAU-129 Launcher on Aircraft, on stations 1, 2, 3A, 7A, 8, 9

The tester shall be able to execute all LAU-129 Launcher on Aircraft, on stations 1, 2, 3A, 7A, 8, 9 requirements IAW the specific MDS Technical Orders.

SRD_1.2.3.3.9 1760 or non-1760 Wing

Weapon Pylon Equipped with Special Carry Remote Interface Unit (SCRIU) on Aircraft, stations 3, 4, 6, 7

The tester shall be able to execute all 1760 or non-1760 Wing Weapon Pylon Equipped with Special Carry Remote Interface Unit (SCRIU) on Aircraft, stations 3, 4, 6, 7 requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.3.10 Non - 1760 equipped Wing Weapon Pylon on Aircraft, stations 3, 4, 6, 7 (MIL - STD-1760) W20 Check

The tester shall be able to execute all Non-1760 equipped Wing Weapon Pylon on Aircraft, stations 3, 4, 6, 7 (MIL - STD-1760) W20 Check requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.3.11 1760 equipped Wing Weapon Pylon on Aircraft stations 3, 4, 6, 7 (MIL - STD-1760} (W20

Long Check)

The tester shall be able to execute all 1760 equipped Wing Weapon Pylon on Aircraft stations 3, 4, 6, 7 (MIL - STD-1760} (W20 Long Check) requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.3.12 1760 equipped Wing Weapon Pylon on Aircraft, stations 3, 4, 6, 7 (MIL-STD-1760)

(W20 Short Check, 1760 only)

The tester shall be able to execute all 1760 equipped Wing Weapon Pylon on Aircraft, stations 3, 4, 6, 7 (MIL-STD-1760) (W20 Short Check, 1760 only) requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.3.13 Aircraft station 5B interface connection circuits (Right Hardpoint Interface Checkout 5R)

The tester shall be able to execute all Aircraft station 5B interface connection circuits (Right Hardpoint Interface Checkout 5R) requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.3.14 Aircraft station 5L interface connection circuits (Left Hardpoint interface Checkout 5L)

The tester shall be able to execute all Aircraft station 5L interface connection circuits (Left Hardpoint interface Checkout 5L) requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.4 Troubleshooting (94FI) Checks - 75060 ACPTS and

SST

The tester shall be able to execute all Troubleshooting (94FI) Checks - 75060 ACPTS and SST requirements IAW the specific MDS Technical Orders.

Demonstration

SRD_1.2.3.4.1 Gun System Analysis The tester shall be able to execute all M61A1 20mm Gun System Control Circuits IAW the specific MDS Technical Orders (SST).

Demonstration

SRD_1.2.3.4.2 Multiple Release - Procedures The tester shall be able to execute all Multiple Release MAU-12, TER, and External Fuel Tank Pylon on Aircraft procedures (covers inadvertent release) IAW the specific MDS Technical Orders (75060 ACPTS).

Demonstration

SRD_1.2.4 Cables/Adapters Cables/Adapters will be MDS specific. All Cables and Adapter required to execute testing will be provided in MDS specific kits. Each MDS platform will require cable and adapter kits for the O-Level pre-load, O-Level Fault Isolation, and I-level Fault Isolation testing requirements.

Demonstration

SRD_1.3 Future Armament Testing Requirements

The CAT-F design will include the capability to upgrade by using the Computer Program Identification Number (CPIN) management process to sustain tester upgrades and modification during the tester’s life cycle. The developed CAT-F will be built using open system software architecture that allows for future upgrades and modifications. In addition to software upgrades, the CAT-F shall utilize as much as possible Modular Open Systems Approach (MOSA) design for tester hardware and sustainment. Vendor will be required to submit all requested data to gain government engineering acceptance/approval for the MOSA standard and upgrade capability for software and hardware.

Analysis

SRD_1.4 Nuclear Certification Nuclear certification for the Tester and applicable nuclear platform TPSs shall be in accordance with AFI 63‐125 (Nuclear Certification Program), AFI 91-103, AFI 91-107, AFMAN 91-118, AFMAN 91-119, and MIL-STD-1822.

Analysis

SRD_1.4.1 System Safety System safety for the Tester shall be conducted IAW the requirements of MIL‐STD‐882E. The Tester design shall be compliant with requirements defined by AFMAN91‐118 and AFMAN91‐ 119.

SRD_1.4.1.1 Single Failures The Tester 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.

Analysis

SRD_1.4.1.2 Dual Failures The Tester 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.

Analysis

SRD_1.4.1.3 Design Safety – Critical Functions

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

Analysis

SRD_1.4.1.4 Design Safety – Internal Faults The Tester design shall prevent internal faults within the tester that could degrade the nuclear or conventional safety of the equipment to be tested.

Analysis

SRD_1.4.1.5 Design Safety – Unintended Signals

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

Analysis

SRD_1.4.1.6 Design Safety – Unintended Firing

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

Analysis

SRD_1.4.1.7 Test Safety – End of Test The Tester shall ensure any device which has been operated during testing is in a safe or inactivated position when the test ends. A positive indication verifies the safe position of such components.

Analysis

SRD_1.4.1.8 Test Safety – System Failures The Tester failures or shutdowns shall leave the components under test in a safe or inactivated condition. The Tester shall provide a clear indication of UUT failure status.

Analysis

SRD_1.4.1.9 Electromagnetic Environmental Effects Requirements

The Tester 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, as well as MIL-STD-461.

Analysis

SRD_1.5 Systems external interface requirements

The Tester shall accommodate the Unit Under Test (UUT), ancillary equipment, and site interfaces defined below and by reference.

Analysis

SRD_1.5.1 Unit Under Test (UUT) external interface description

The UUT interface shall be used to provide AC power, DC power, analog and digital stimuli to the UUTs and measure AC power, DC power, analog and digital signals from the UUTs through the Tester UUT interface.

Demonstration

SRD_1.5.1.1 UUT communication buses The following communication interfaces shall be provided by the Tester. Demonstration SRD_1.5.1.1.1 MIL‐STD‐1553 The MIL‐STD‐1553 bus interface shall operate as specified in MIL‐STD‐1553A/B and shall provide an interface for both direct and transformer coupled buses. The following modes of operation shall be supported: Bus controller (BC), Remote terminal (RT), and Bus monitor

(BM).

Demonstration

SRD_1.5.1.1.2 MIL-STD-1760 The MIL‐STD‐1760 Aircraft/Store Electrical Interconnection System interface shall operate as specified in MIL‐STD‐1760E and shall provide an interface for the operation and employment of stores on aircraft.

Demonstration

SRD_1.5.1.2 UUT Discrete Interfaces Breach adapter, striker points, etc. Demonstration SRD_1.5.2 Power SRD_1.5.2.1 Operating Power 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 shall comply with the requirements listed in MIL‐ PRF‐28800, MIL‐STD‐704 and MIL‐STD‐1332 where applicable for each tester. If there are discrepancies between the specifications listed, MIL-STD-704 takes precedence.

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

SRD_1.5.2.1.1 Handheld Tester Power The CAT-F Handheld Tester shall be powered by common design batteries which are non-proprietary and replaceable in a minimal amount of time. Preload testing shall utilize battery power for all go/no-go preload and stray voltage testing. When 28VDC is present from the AME side during testing, the handheld tester should leverage that power from the AME to extend battery life. Optionally, users should have the option to use external power (aircraft, Aerospace Ground Equipment (AGE), facility, etc.) power for preload testing. Power adapter cables must be provided for all user power options. The handheld tester internal batteries shall be verified as replaceable in under 2 minutes.

Threshold: Preload testing will utilize battery power for all go/no- go preload and stray voltage testing.

Objective: Preload testing will utilize battery power for all go/no- go preload and stray voltage testing and have the option to use the aircraft/AGE/facility power for preload testing (All power adapter cables must be provided).

Demonstration

SRD_1.5.2.1.2 Fault Isolation Tester Power This equipment shall utilize electric power in accordance with MIL-STD-704 and shall be in accordance with the utilization equipment requirements of MIL-STD-704. As a minimum the primary power source shall operate at 100-240V@50/60/400 Hz (single and multi‐phase) IAW MIL-STD-704, MIL-PRF-28800, and MIL-STD-1332 and include adapters to utilize aircraft, AGE, and Backshop power. If there are discrepancies between the specifications listed, MIL- STD-704 takes precedence.

Test

SRD_1.5.2.2 Unit Under Test Power The Intermediate Tester shall be capable of switching external power as required by the UUT.

The Tester shall control on/off switching of power to the UUT as required by the UUT TPS.

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

Demonstration

SRD_1.5.2.3 Circuit Protection The CAT-F tester will be developed with built in Circuit protection. The design will ensure the users, CAT-F, and Unit Under Test (UUT) are protected from improper voltage or amperage.

Verification will be accomplished by applying enough input power to activate circuit protection in the designed tester, followed by resetting the circuit protection and verifying the tester circuits were not damaged. MIL-STD-704 (Aircraft Electrical Power Characteristics) will be used to ensure power requirements for circuit protection are followed.

Test

SRD_1.5.2.4 Power Monitoring The Intermediate Tester shall measure input power, VRMS for each phase, phase sequence, and frequency information 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 Tester shall detect and respond to the presence of more than 6 VRMS between the Neutral and Chassis Ground as follows:

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

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

Test

SRD_1.5.2.5 Handheld Power Monitoring Handheld Tester shall display handheld battery status

Tester shall display battery status warning at 50%, 25%, and 10%.

Demonstration

SRD_1.5.3 Grounding SRD_1.5.3.1 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‐419.

Inspection

SRD_1.5.3.2 Shock Protection The grounding scheme for the Tester shall provide protection of personnel and equipment from electrical shock hazards during normal operations and under ground fault conditions.

Analysis

SRD_1.5.3.3 Ground Loop Prevention The Tester shall be designed to eliminate ground loops and minimize common ground impedance which can degrade system noise margins.

Analysis

SRD_1.5.3.4 External Safety Ground The Intermediate Tester shall provide an external safety ground stud or bar. Demonstration SRD_1.5.4 Graphical Display SRD_1.5.4.1 I-Level Tester

Graphical Display Size For the I-level tester, the display shall be sized at 9 inches diagonally at a minimum to clearly show all applicable information as defined in specification paragraph 1.1.2.2 (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‐1472, Section 5.2.

Analysis Inspection

SRD_1.5.4.2 Graphical Display Readability The display shall be readable in all lighting conditions, including full daylight ambient conditions; direct sunlight; and nighttime IAW MIL‐STD‐1472G, Section 5.2. The brightness setting shall not allow the display to "blackout".

Demonstration

SRD_1.5.4.3 I-level Graphical User Interface

The Intermediate Tester 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.

Demonstration

SRD_1.5.4.4 User Navigation The Tester shall provide controls to allow the operator to move between pages of display information, between selection options, and selection of a menu item/option.

Demonstration

SRD_1.5.4.5 Handheld Handheld Tester Display shall follow current military standards with sunlight readable graphic display with resolution at least 128 X 64 pixels or better, and different screen background. The handheld tester display will be at a minimum 1.5 inches by 2.5 inches in Viewable Area.

Demonstration

SRD_1.6 Modular Open System Architecture Design

SRD_1.6.1 Modular Design 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.

Analysis

SRD_1.6.1.1 Module Cohesion Module Cohesion – The contractor’s design shall result in modules that are characterized by the singular assignment of…