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PERFORMANCE-BASED WORK STATEMENT (PWS)
for
Rocket Systems Launch Program (RSLP) Aging Surveillance (AS) and Disposal
Solicitation/Contract Number:
FA8818-12-R-0025
11 January 2012
TABLE OF CONTENTS
| 1 | INTRODUCTION | 2 |
| 1.1 Scope | 2 | |
| 2 | APPLICABLE DOCUMENTS | 2 |
| 2.1 Reference Documents | 2 | |
| 2.2 Compliance Documents | 2 | |
| 3 | REQUIREMENTS | 3 |
| 3.1 General Requirements | 3 | |
| 3.2 AS Requirements | 3 | |
| 3.3 Motor Disposition/Disposal Requirements | 6 | |
| 3.4 Special Studies Requirements | 6 | |
| 3.5 Special Requirements/Anomaly Investigations | 6 | |
| 3.6 Materials and Test Equipment (TE) Support | 6 | |
| 3.7 Program Management (PM) Requirements | 7 | |
| 4 | General Considerations | 7 |
| 4.1 Five year Plan | 7 | |
| 4.2 Services Summary | 7 | |
| 4.3 Quality Assurance | 8 | |
| 5 | DELIVERABLES | 9 |
| 6 | contract security requirements | 10 |
| 7 | GOVERNMENT FURNISHED EQUIPMENT/PROPERTY | 10 |
| 8 | Acronyms | 10 |
ANNEXES:
1. RSLP TEST MATRIX
2. RSLP 5 YEAR PLAN
3. GFP LIST
INTRODUCTION
Minuteman (MM) motor and component Aging Surveillance (AS) has been provided by the Rocket Systems Launch Program (RSLP) since 1993 by the original motor manufacturers ATK Launch Systems and Aerojet Corp; Peacekeeper (PK) motor and component AS has been provided for the RSLP since 2006 by ATK Launch Systems; MM and PK motor disposal was previously included in AS contracts and applied mainly to motors and components that had been used in AS processes.
Scope This Performance Work Statement (PWS) delineates the contractor tasks required to perform AS and motor disposal in support of the RSLP on MM and PK rocket motors and related components. These tasks provide motor and component life extension and identify aging trends in the motors which may be a significant indication of motor degradation. Additionally, this new contract will incorporate disassembly and disposal of unusable motors and some components. Required tasks to support AS and motor disposal of these assets include AS analysis, engineering and laboratory tests, motor preparation and static fire/support, support equipment maintenance, disposal, transportation, disassembly and disposition reporting.
APPLICABLE DOCUMENTS
Reference Documents The following documents are to be considered as reference material for the purpose of interpreting the requirements of this PWS but are not contractual documents.
| Document No. | | Title |
| TO 2K-SR118-3 | TECHNICAL MANUAL OVERHAUL AND REPAIR INSTRUCTIONS WITH ILLUSTRATED PARTS BREAKDOWN DEPOT PEACEKEEPER STAGE I MIDEL SR-118, P/N 54576 SERIES THIOKOL CORPORATION FO4704-83-C-0001 | | |
| | FO4704-88-C-0015 | |
TO 21-LG118A-26-1 OPR AND MAINT (DEPOT) -- HANDLING AND RADIOGRAPHIC PREPARATION INSTR FOR PEACEKEEPER SOLID STAGE ROCKET MOTORS AND COMPONENTS, STAGE I, II AND III, PN 54576, 1175641 AND 10529 SERIES (HERCULES INC) LGM118A
AFMAN 91201 EXPLOSIVE SAFETY STANDARDS
12 JAN 11
TO 21-LG118A-2-26CL-1 DEPOT-MISSILE SOLID STAGES TRANSPORTATION AND HANDLING- HILL AFB AND HILL AFB RANGE, UT Compliance Documents The contractor shall comply with the following documents of the exact issue shown to the extent specified in the column entitled "Tailored Application."
| Document No. | Title | | | Tailored Application |
| MILSTD882B | System Safety Program | As specified in the following: | | |
| 30 Mar 84 | Requirements | | All requirements of paragraph 4 and | |
| Notice I | | | | tasks 100 and 106 are applicable. |
I Jul 87
| TO1 IA147 | | Department of Defense | All |
| 5 Jan 98 | Explosives Hazard | | |
| Classification Procedures | | |
REQUIREMENTS
General Requirements Applicable Document Compliance The contractor shall comply with the applicable documents listed in Section 2.0 in performing PWS tasks. The contractor shall use the referenced documents to determine how to accomplish the tasks. The nature of A&AS services designed to facilitate government management and oversight of weapon system activities, however, also requires the contractor to adapt to changing direction, guidance, standards, policies and practices while performing the tasks within this PWS. To ensure both the Government and contractor remain synchronized relative to applicable guidance and documents, the contractor shall perform the PWS using the most current approved version of the applicable documents in section 2.0.
Environmental Compliance The contractor shall perform environmental compliance activities in accordance with federal, state, and local laws and regulations in order to comply with the requirements of this contract. Environmental activities may include one or more of the following: handling of any hazardous materials used or generated in performance of this effort; environmental analysis to demonstrate compliance with applicable federal, state, or local regulations, laws, or other specifications in accordance with this PWS; and preparation/submittal of environmental documentation to proper organizations. These environmental activities will only be in support of tasks covered by this PWS.
AS Requirements The contractor shall provide AS for Safety of Storage (SoS) and Reliability of Flight (RoF) of former MM and PK rocket motors and components. The contractor shall conduct motor and component tests and analyses that result in service life extension and identify aging trends that may affect performance. SoS testing and analysis validates the motors/components are safe to handle and store. RoF testing and analysis validates the motors/components perform to the original specifications. The contractor shall analyze test results and provide a recommendation for continued application/use of the assets. Specific requirements by motor/component are located in Annex 1.
Motor Static Fire Tests The contractor shall provide support for static fire tests of MM and PK rocket motors conducted at the Utah Test and Training Range (UTTR) and conduct/support motor static fire tests at the contractor’s proposed facility.
UTTR Static Fire Tests The contractor shall provide data analysis, including post-fire analysis and post-fire inspections. Ballistics analysis will be conducted by the contractor. The contractor shall provide a report on the post-fire analyses and inspections data. Results of these tests and inspections shall be provided for inclusion in the annual report. (CDRL A001, CDRL A002, CDRL A003) Contractor Facility Static Fire Tests The contractor shall provide static fire capability including but not limited to planning, preparation, execution and data analysis, including post-fire analysis and post-fire inspections. Ballistics analysis will be conducted by the contractor. The contractor shall provide a report on the post-fire analysis and inspections. The contractor shall maintain the static fire capability, regardless of static fire schedule. Results of these tests and inspections shall be included in an annual report. (CDRL A001, CDRL A002, CDRL A003) Component Static Fire Tests The contractor shall provide static fire tests of igniters and Gas Generators (GG) conducted at the contractor’s proposed facility, which may include Government range facilities.
Igniter Static Fire Tests The contractor shall plan, prepare, and execute the static fire tests of igniters, and data analysis. Pre-test environments (temperature cycling/transport and handling) shall be imposed by the Government. The contractor shall perform all necessary planning to delineate pre-test inspections and instrumentation requirements. The contractor shall prepare a final report for each test to include but not limited to data resulting from pre-fire testing, post-fire inspections and comparison to historical data. (CDRL A001, CDRL A002, CDRL A003) GG Static Fire Tests The contractor shall plan, prepare, execute of Thrust Vector Actuated (TVA), Extendable Nozzle Exit Cone (ENEC), Deployment Actuation System (DAS) GG and analyze the data. Pre-test environments (temperature cycling/transportation and handling) will be imposed by the Government. The contractor shall prepare a test plan (TP) detailing test conditions, pre-test inspections, and instrumentation. The contractor shall prepare a final report for each test to include but not limited to data resulting from pre-fire inspections, post-fire inspections, ballistics, and comparison to historical data. (CDRL A001, CDRL A002, CDRL A003) Nozzle Inspections and Tests Nozzle inspection and Static Fire tests are performed to determine effects of aging and provide service life extension of MM and PK nozzles. The contractor shall support the planning, preparation, execution, and data analysis of the testing of flexseal, TVA, and nozzles to identify aging trends. The contractor shall prepare a test plan detailing test conditions and instrumentation. The contractor shall prepare a final report for each test to include but not limited to data resulting from the testing, and comparison to historical data. (CDRL A001, CDRL A002, CDRL A003) Propellant Tests These tests are performed to determine effects of aging on motor and component propellant. The contractor shall perform/support the testing and analysis. Quantity and location of samples and test conditions shall be commensurate with previous test programs.
The contractor may assess the effects of changes in mechanical properties on structural margins of safety.
Loaded Motor Propellant Material Properties Test & Analysis The contractor shall plan, prepare, execute and provide data analysis to identify any age related trends and provide a recommendation for continued application/use of the assets. The contractor shall prepare a final report for each test to include but not limited to data resulting from the testing, and comparison to historical data. (CDRL A001, CDRL A002, CDRL A003) Motor Dissection The contractor shall conduct motor dissection periodically to ensure samples for conducting propellant material properties test. The timing and test required shall be approved by the Government according to the approved TP. The contractor shall support this planning and provide analysis of the propellant and bondline mechanical property data to support the trend analysis and useful life estimates. (CDRL A001, CDRL A002, CDRL A003) Loaded Motor Plugging/Excise Sampling The intent of this test series is to provide insight and assess the condition of the liner and propellant along the longitudinal axis of the case. The contractor shall plug and remove excise samples from the loaded motor case. This effort includes motor plugging, and test and analysis of samples. Quantities and locations of samples and testing conditions shall be consistent with previous test programs. (CDRL A001, CDRL A002, CDRL A003) Propellant Hazards Sensitivity Tests The contractor shall conduct propellant hazards sensitivity tests on motor propellants. These are primarily follow-on tests to the previous operational AS programs. The contractor shall support test planning and provide analysis of the propellant to support the trend analysis and useful life estimates with comparison to historical data base. (CDRL A001, CDRL A002, CDRL A003) Component Laboratory Tests Loaded Igniter Dissection The contractor shall dissect propellant loaded and unloaded igniters. Tests and inspections shall be comparable to previous test programs. This effort includes igniter dissection, analysis, test, storage and disposal. (CDRL A001, CDRL A002, CDRL A003) GG Dissection The contractor shall dissect Roll Control (RC), TVA and Nozzle GGs to obtain propellant chemical and mechanical properties. Tests and inspections shall be comparable to previous test programs. This effort includes GG dissection, storage, propellant testing and analysis. (CDRL A001, CDRL A002, CDRL A003) Ordnance Tests
3.2.5.1 Interstage Ordnance
The contractor shall provide IO Functional Testing, including RSLP unique items and legacy hardware. A test report (TR) will be issued to document the test results from functional tests as well as all the plots of the various environmental testing. Tests and inspections shall be comparable to previous test programs. (CDRL A001, CDRL A002, CDRL A003)
3.2.5.2 Ordnance Initiation Set
The contractor shall evaluate the hardware used to initiate igniters, gas generators and separation ordnance. This hardware consists of the through bulk-head initiator (TBI), and the type I and III ordnance transfer assemblies (OTA). The contractor shall prepare a test plan detailing test conditions and instrumentation. The contractor shall prepare a final report for each test to include results of the testing, and comparison to the historical database. (CDRL A001, CDRL A002, CDRL A003)
0. Ordnance/Range Certification Test Requirements The Government will provide Flight Termination (FTS) and Ordnance test per Range Commanders Council (RCC) 319-07 using Government Range personnel and test facilities to the maximum extent possible. The contractor shall support FTS and ordnance test as requested by the Government.
Motor Disposition/Disposal Requirements The contractor shall be responsible for the disposal of motors/components and related assets as necessary to support RSLP requirements.
AS Related Disposal The contractor shall disposition and dispose of residual material resulting from AS for assets tested/consumed at the contractor’s facility. This shall include, but is not be limited to, residual propellant from dissections/plugging operations, and motor/component static fire. Motors subject to the Strategic Arms Reduction Treaty (START) will be disposed per treaty requirements.
Excess Motor/Component Disposal The contractors shall disassemble and dispose of unusable motors/components per Government plan, through proven and effective methods, including but not limited to, wash out, motor/component fire or detonation. The contractor will provide a final report of motor disposition. (CDRL A005) Storage of Assets The contractor shall store selected assets required for AS and disposal to ensure availability when needed or as directed by the Government. Tasks required for this storage shall include the monitoring of the temperature to ensure proper environmental control.
Special Studies Requirements The contractor shall conduct special studies, which may be required due to changing AS or motor disposal requirements. The contractor shall provide engineering, technical and analysis support for system engineering and safety related issues of the motors/components. The contractor shall perform AS and disposal testing and analyses related to transportation, maintenance, safety, processing, test, long term storage and use. Special studies may result in either a recommendation or solution to an identified need, and/or procure support equipment as requested by the Government. (CDRL A001, CDRL A002, CDRL A003, CDRL A004) Special Requirements/Anomaly Investigations The contractor shall conduct special requirements studies/investigations related to motors/ components and disposal requirements, as directed by the Government. This includes activities such as failure investigations, anomaly investigations, and modification or development of tooling to support unique program requirements. The contractor shall also conduct other special requirements studies related to requirements in this PWS when, due to the uncertain nature of the effort involved, it is not practical to establish a firm fixed price. Special Requirements/Anomaly Investigations could result in recommendations or solutions to an identified need. (CDRL A001, CDRL A002, CDRL A003, CDRL A004) Materials and Test Equipment (TE) Support The offeror shall provide motor/component unique materials necessary for the refurbishment, testing, and maintenance as required by the Government to support RSLP.
Materials Provide materials including chemicals, soft goods, lubricants, hardware, ordnance, and other components as requested by the Government.
Electrical TE Maintenance Provide periodic maintenance of electrical TE to include minor repairs and labor.
Pressure Transducer Calibration Provide calibration of pressure transducers as requested by the Government. (CDRL A001, CDRL A002) Program Management (PM) Requirements PM & Engineering Support The contractor shall manage the overall schedule and annual report. The contractor shall provide an annual report that summarizes all contract activities, testing and recommendations. The contractor shall develop, maintain, and deliver to the Government an electronic monthly program schedule which details required activities, progress achieved, and required dates for Government Furnished Property (GFP) delivery. The contractor shall provide a monthly Contract Funds Status Report (CFSR) report that identifies actual and projected commitments, expenditures, billings, and Government invoices for all CLINs on this contract. The CFSR shall be submitted by the 10th day of each month, with data accurate to the previous month. (CDRL A002, CDRL A007, CDRL A008) Meetings The contractor shall support four Technical Interchange/Technical Direction (TI/TD) meetings per year for AS support and two Technical Interchange meetings (TIM) for disposal to be conducted in or near the contractor’s facility. At the Government’s discretion, these meetings can support other mission integration activities. One of these meetings may be held at Kirtland AFB. (CDRL A006) Data The contractor will provide a copy of all TPs and TRs to the Government for motor and component testing and motor/component disposition provided under this contract. (CDRL A001, CDRL A002, CDRL A003)
GENERAL CONSIDERATIONS
Five year Plan The Government has developed a 5 year plan, located at Annex 2, forecasting requirements for AS and disposal activities anticipated for this contract.
Services Summary
| SS # |
| Performance Category |
| PWS Paragraph |
| Performance Threshold |
| 1 |
| Motor Static Fire Tests |
| 1.1.1 |
| Contractor support to motor static fire tests shall be capable of inclusion into Annual AS Reports with less than two (2) recommendations/solutions per year requiring significant change for reasons within contractor control. |
| 2 |
| Component Static Fire Tests |
| 1.1.2 |
| Contractor support to component static fire tests shall be capable of inclusion into Annual AS Reports with less than two (2) recommendations/solutions per year requiring significant change for reasons within contractor control. |
| 3 |
| Propellant Tests |
| 1.1.3 |
| Contractor support to propellant tests shall be capable of inclusion into Annual AS Reports with less than two (2) recommendations/ solutions per year requiring significant change for reasons within contractor control. |
| 4 |
| Component Laboratory Tests |
| 1.1.4 |
| Contractor support to component laboratory tests shall be capable of inclusion into Annual AS Reports with less than two (2) recommendations/solutions per year requiring significant change for reasons within contractor control. |
| 5 |
| Ordnance Tests |
| 1.1.5 |
| Contractor support to Ordnance tests shall be capable of inclusion into Annual AS Reports with less than two (2) recommendations/ solutions per year requiring significant change for reasons within contractor control. |
| 6 |
| Excess Motor/ Component Disposal |
| 1.2.2 |
| Contractor motor and component disposal shall conform to all AFCANs guidelines with less than two (2) disposal actions per year requiring Government action for reasons within contractor control. |
| 7 |
| Materials & TE Support |
| 1.5 |
| Contractor support for materials and TE support shall conform to Government stated needs with less than two (2) per year impacting baseline schedules for reasons within contractor control. |
| 8 |
| PM & Engineering Support |
| 1.6.1 |
| Program schedules and reports are accurate and provided on time with less than 3 schedules/reports per year requiring significant change for reasons within contractor control. |
| 9 |
| Data |
| 1.6.2 |
| Test and Disposition Reports will be accurate and complete with less than 2 significant changes required per document for reasons within contractor control. |
Quality Assurance In compliance with Federal Acquisition Regulation (FAR) 52.246-4 “Inspection of Services—Fixed Price” the Contractor shall provide and maintain an inspection system acceptable to the Government covering the services under this contract. Complete records of all inspection work performed by the Contractor shall be maintained and made available to the Government during contract performance and for as long afterwards as the contract requires.
The Government has the right to inspect and test all services called for by the contract, to the extent practicable at all places and times during the term of the contract. The Government shall perform inspections and tests in a manner that will not unduly delay the work.
If any of the services performed do not conform with the contract requirements, the Government may require the Contractor to perform the services again in conformity with contract requirements, at no increase to contract price or for no additional fee. When the defects in services cannot be corrected by re-performance, the Government may --
· Require the Contractor to take necessary action to ensure that future performance conforms to contract requirements; and
· Reduce the contract price or any fee payable under the contract to reflect the reduced value of the services performed.
If the Contractor fails to promptly perform the services again or take the action necessary to ensure future performance in conformity with contract requirements, the Government may --
· By contract or otherwise, charge to the Contractor any cost incurred by the Government that is directly related to the performance of such service or
· Terminate the contract for default.
Government Inspection The Government will evaluate the contractor's performance under this contract in accordance with the Quality Assurance Surveillance Plan. Government methods of inspection other than those listed in the PWS (such as provided for by the Inspection of Services clause) may occur during the performance period of this contract. Such surveillance will be done according to standard inspection procedures or other contract provisions. Any action taken by the Contracting Officer (CO) as a result of inspections will be according to the terms of this contract.
Contracting Officer’s Representative (COR) CORs are representatives of the contracting officer and will participate in the administration of this contract. Subsequent to contract award, the contractor will be provided with a letter identifying CORs and setting forth their duties and authorities.
Scope Changes Any matter concerning a change to the scope, prices, terms or conditions of this contract shall be referred to the CO.
Administrative Records All records, documents, and associated papers provided by the Government and generated during the period of this contract become Government property and will remain in place upon contract termination or completion. During the period of the contract, records, documents, and associated papers shall be available for review.
DELIVERABLES
Contract Deliverables Requirements List (CDRL):
| CDRL# |
| TITLE: SUB-TITLE |
| DID |
| A001 |
| TEST/INSPECTION REPORT: INDIVIDUAL TEST REPORT |
| DI-NDTI-80809B |
| A002 |
| TEST/INSPECTION REPORT: ANNUAL SUMMARY REPORT |
| DI-NDTI-80809B |
| A003 |
| TEST PLAN |
| DI-NDTI-80566A |
| A004 |
| TECHNICAL REPORT-STUDY/SERVICES: SPECIAL STUDIES |
| DI-MISC-80508B |
| A005 |
| HAZARDOUS WASTE (HW) REPORT: MOTOR DISPOSAL CERTIFICATE |
| DI-NDTI-80899 |
| A006 |
| REPORT, RECORD OF MEETING/MINUTES |
| DI-ADMN-81505 |
| A007 |
| INTEGRATED MASTER SCHEDULE (IMS) |
| DI-MGMT-81650 |
| A008 |
| CONTRACT FUNDS STATUS REPORT (CFSR) |
| DI-MGMT-81468 |
CONTRACT SECURITY REQUIREMENTS
This contract will follow the DoD 5200.22M, National Industrial Security Operating Manual (NISPOM). To accomplish this work the contractor will require access to For Official Use Only (FOUO) Information and the Government Local Area Network. Additionally the contractor will receive and generate classified material at the SECRET level, be authorized to use the services of Defense Technical Information Center (DTIC) or other secondary distribution center, have TEMPEST and Operations Security (OPSEC) requirements, and have access to DoD Space System Protection Guide Information. Contract security requirements are defined in the contract DD 254, Contract Security Classification Specification.
GOVERNMENT FURNISHED EQUIPMENT/PROPERTY
The Contractor shall be responsible and accountable for all Government property provided under this contract and shall comply with FAR Subpart 45.5 Records of Government property. The Contractor shall create and maintain records of all Government property accountable to the contract, including Government-furnished and Contractor-acquired property. GFP available for this contract are included in Annex 3.
ACRONYMS
| CDRL |
| Contrat Deliverables Requirements Document |
CFSR
CO
Contract Funds Status Report Contracting Officer
| COR |
| Contracting Officer’s Representative |
| DAS |
| Deployment Actuation System |
| ENEC |
| Extendable Nozzle Exit Cone |
| FAR |
| Federal Acquisition Regulation |
| FTS |
| Flight Termination System |
| GFP |
| Government Furnished Property |
| IMS |
| Integrated Master Schedule |
| LEA |
| Linear Explosive Assemblies |
| PWS |
| Performance Work Statement |
| RCC |
| Range Commander’s Council |
| RSLP |
| Rocket Systems Launch Program |
| START |
| STrategic Arms Reduction Treaty |
| TI/TD |
| Technical Interchange/Technical Direction |
| TIM |
| Technical Integration Meeting |
| TVA |
| Thrust Vector Actuated |
| UTTR |
| Utah Test and Training Range |
RSLP AS AND DISPOSAL PWS
ANNEX 1: RSLP TEST MATRIX
| Test Type |
| System/Component |
| Peacekeeper |
| Minuteman |
| SR118 |
| SR119 |
| SR120 |
| M55 |
| SR19 |
| M57 |
| Peformance Test (Static Fire) |
| Motor |
| X |
| X |
| X |
| G1 |
| G1 |
| G1 |
X
RC Gas Generator
X
Nozzle Gas Generator
| Dissect/Plugging & Material Testing |
| Igniter |
| X |
| X |
| X |
| X |
| X |
| X |
X
RC Gas Generator
X
Nozzle Gas Generator
X
Motor
| Propellant Properties |
| X |
| X |
| X |
| X |
| X |
| X |
| Propellant Hazards |
| X |
| X |
| X |
| X |
| X |
| X |
| Other Testing (Non-ordance) |
| Nozzle Flexseal |
| X |
| X |
| X |
X
Unfired Nozzle Test
Fire Nozzle Test
| Flight Termination System and Other Ordnance |
| LSC Testing |
| X |
| X |
| X |
| Interstage Ordnance Test |
| X |
| X |
| X |
| X |
| X |
| X |
| Ordnance Initiation |
| X |
| X |
| X |
Safe and Arm (1)
Arm/Disarm Switch (1)
TT Port Frangible Sector
G2
TVA Gas Generator Igniter
G2
Sounding Rocket Destruct System
Mechanical Modular Ordnance System (1)
X
Greases
X
O-rings
Gaskets (Metal)
X
Liner Kits
X
Notes:
(1) - Common for all MM applications; tested at Gov facility X - Tested at contractor facility G1 - Testing performed at government facility. Contractor responsible for post-test disassembly/ inspections G2 - For information only. Testing performed at Government facility. No contractor involvement currently required.
RSLP AS AND DISPOSAL PWS
ANNEX 2: GOVERNMENT 5 YEAR PLAN
Minuteman M55A1
Calendar Year
| Activity Name |
| 2012 |
| 2013 |
| 2014 |
| 2015 |
| 2016 |
| 2017 |
Static Fire Test
| Insulation Erosion |
| 1 |
| 1 |
| 1 |
| 1 |
| 1 |
| 1 |
Loaded Motor Plugging
Prop. & Bondline Testing
| Unfired Nozzle Test |
| 1 |
| 1 |
| 1 |
| 1 |
| 1 |
| 1 |
Igniters
Static Test with Environments
Dissection/Propellant Testing
| Motor Disposal |
| 12 |
| 12 |
| * |
| * |
| * |
| * |
Minuteman SR19-AJ-1
Calendar Year
| Activity Name |
| 2012 |
| 2013 |
| 2014 |
| 2015 |
| 2016 |
| 2017 |
Static Fire Test
| Post Fire Inspections |
| 1 |
| 1 |
| 1 |
| 1 |
| 1 |
| 1 |
| Insulation Erosion |
| 1 |
| 1 |
| 1 |
| 1 |
| 1 |
| 1 |
Loaded Motor Plugging
Prop. & Bondline Testing
| Unfired Nozzle Inspections |
| 1 |
| 1 |
| 1 |
| 1 |
| 1 |
| 1 |
Igniters
| Static Test with Environments |
| 1 |
Dissection/Propellant Testing
RC Gas Generator
| Static Test with Environments |
| 2 |
Dissection/Propellant Testing
TVA Gas Generator
Static Test with Environments
Dissection/Propellant Testing
Flexseal
Full-Scale Unit
Flexseal Removal From Full-Scale Motor
| Motor Disposal |
| 2 |
| 4 |
| * |
| * |
| * |
| * |
Minuteman M57A1
Calander Year
| Activity Name |
| 2012 |
| 2013 |
| 2014 |
| 2015 |
| 2016 |
| 2017 |
Static Fire Test
| Post Fire Nozzle Inspections |
| 2 |
| 2 |
| 2 |
| 2 |
| 2 |
| 2 |
Loaded Motor Plugging
Prop. & Bondline Testing
| Unfired Nozzle Inspections |
| 2 |
| 2 |
| 2 |
| 2 |
| 2 |
| 2 |
Igniters
| Static Test with Environments |
| 2 |
Dissection/Propellant Testing
Post Fire Burst Test
| Motor Disposal |
| 30 |
| 34 |
| * |
| * |
| * |
| * |
| * 0 unless directed otherwise by the Government; |
| No component disposal is planned |
Peacekeeper SR118
Calendar Year
| Activity Name |
| 2012 |
| 2013 |
| 2014 |
| 2015 |
| 2016 |
| 2017 |
Static Fire Test
Fired Nozzle
Insulation Erosion
Prop. & Bondline Testing Analysis
Propellant Hazards Testing
Dissection/Propellant Testing
Igniters
Static Test with Environments
Dissection/Propellant Testing
TVA Gas Generator
Static Test
Dissection/Propellant Testing
TVA System
Flexseal
Full-Scale Unit
Flexseal Removal From Full-Scale Motor
| Motor Disposal |
| * |
| * |
| * |
| * |
| * |
| * |
Peacekeeper SR119
Calendar Year
| Activity Name |
| 2012 |
| 2013 |
| 2014 |
| 2015 |
| 2016 |
| 2017 |
Static Fire Test
Post Fire Inspections
Insulation Erosion
Prop. & Bondline Testing Analysis
Propellant Hazards Testing
Nozzles
| Unfired Nozzle Inspections |
| 1 |
Igniters
| Static Test with Environments |
| 2 |
Dissection/Propellant Testing
ENEC Gas Generator
| Static Test with Environments |
| 2 |
Dissection/Propellant Testing
TVA Gas Generator
| Static Test with Environments |
| 2 |
Dissection/Propellant Testing
Flexseal
Full-Scale Unit
Flexseal Removal From Full-Scale Motor
| Motor Disposal |
| * |
| * |
| * |
| * |
| * |
| * |
| * 0 unless directed otherwise by the Government; |
| No component disposal is planned |
Peacekeeper SR120
Calendar Year
| Activity Name |
| 2012 |
| 2013 |
| 2014 |
| 2015 |
| 2016 |
| 2017 |
Static Fire Test
Post Fire Inspections
Insulation Erosion
Loaded Case
Dissection
Prop. & Bondline Testing and Analysis
Propellant Hazards Testing
Igniters
Static Test with Environments
Dissection/Propellant Testing
DAS Gas Generator
Static Test with Environments
TVA Gas Generator
Static Test with Environments
TVA System
Flexseal
Full-Scale Unit
Flexseal Removal From Full-Scale Motor
| Motor Disposal |
| * |
| * |
| * |
| * |
| * |
| * |
| * 0 unless directed otherwise by the Government; |
| No component disposal is planned |
ORDNANCE
Calendar Year
| Activity Name |
| 2012 |
| 2013 |
| 2014 |
| 2015 |
| 2016 |
| 2017 |
PK FTOS LSCA (Range Safety)
SR118/SR119
SR120
PK Ordnance Initiation Set
Thru-Bulk Head Initiator
Type I OTA
Type III OTA
PK Interstage
ASE/SR118
SR118/SR119
SR119/SR120
MM Interstage
| Delay Booster (16 sec) |
| 10 |
Explosive Assembly (Longitudnal)
Exploosive (H) Booster
Mechanical S/A
Pellet Assembly
Page of 3
RSLP AS AND DISPOSAL PWS
ANNEX 3: GOVERNMENT FURNISHED PROPERTY
| PART NUMBER |
| DESCRIPTION |
| QTY |
| UOM |
| COST |
| EXT. COST |
| 1103136-3 |
| SPACER, SKIRT |
| 2 |
| EA |
| $29.94 |
| $59.88 |
| 1103136-3 |
| SPACER, SKIRT |
| 2 |
| EA |
| $29.94 |
| $59.88 |
| 1103138-1 |
| GASKET |
| 1 |
| EA |
| $0.60 |
| $0.60 |
| 1103138-1 |
| GASKET |
| 1 |
| EA |
| $0.60 |
| $0.60 |
| 1103138-1 |
| GASKET |
| 2 |
| EA |
| $0.60 |
| $1.20 |
| 1103138-1 |
| GASKET |
| 2 |
| EA |
| $0.60 |
| $1.20 |
| 1103138-1 |
| GASKET |
| 2 |
| EA |
| $0.60 |
| $1.20 |
| 1103138-1 |
| GASKET |
| 1 |
| EA |
| $0.60 |
| $0.60 |
| 1103370-5 |
| INSERT, CLAMP |
| 6 |
| EA |
| $8.14 |
| $48.84 |
| 1103370-7 |
| INSERT |
| 10 |
| EA |
| $8.14 |
| $81.40 |
| 1105320-1 |
| BRACKET, RELIEF VALVE |
| 1 |
| EA |
| $64.14 |
| $64.14 |
| 1105354-1 |
| BRACKET, RELIEF VALVE |
| 1 |
| EA |
| $52.99 |
| $52.99 |
| 1105354-1 |
| BRACKET, RELIEF VALVE |
| 1 |
| EA |
| $52.99 |
| $52.99 |
| 1105354-1 |
| BRACKET, RELIEF VALVE |
| 1 |
| EA |
| $52.99 |
| $52.99 |
| 1105354-1 |
| BRACKET, RELIEF VALVE |
| 1 |
| EA |
| $52.99 |
| $52.99 |
| 1105354-1 |
| BRACKET, RELIEF VALVE |
| 1 |
| EA |
| $52.99 |
| $52.99 |
| 1105354-1 |
| BRACKET, RELIEF VALVE |
| 1 |
| EA |
| $52.99 |
| $52.99 |
| 1105354-1 |
| BRACKET, RELIEF VALVE |
| 1 |
| EA |
| $52.99 |
| $52.99 |
| 1105913-1 |
| INSULATOR |
| 1 |
| EA |
| $26.65 |
| $26.65 |
| 1105914-1 |
| INSULATOR |
| 1 |
| EA |
| $26.65 |
| $26.65 |
| 383728-9 |
| CLIP |
| 2 |
| EA |
| $34.16 |
| $68.32 |
| 383728-9 |
| CLIP |
| 2 |
| EA |
| $34.16 |
| $68.32 |
| 383728-9 |
| CLIP |
| 2 |
| EA |
| $34.16 |
| $68.32 |
| 383728-9 |
| CLIP |
| 2 |
| EA |
| $34.16 |
| $68.32 |
| 383905-1 |
| GROMMET |
| 1 |
| EA |
| $5.69 |
| $5.69 |
| 383905-1 |
| GROMMET |
| 1 |
| EA |
| $5.69 |
| $5.69 |
| 383905-1 |
| GROMMET |
| 1 |
| EA |
| $5.69 |
| $5.69 |
| 383905-1 |
| GROMMET |
| 1 |
| EA |
| $5.69 |
| $5.69 |
| 383905-1 |
| GROMMET |
| 1 |
| EA |
| $5.69 |
| $5.69 |
| 383905-1 |
| GROMMET |
| 1 |
| EA |
| $5.69 |
| $5.69 |
| 383914-1 |
| GROMMET |
| 1 |
| EA |
| $7.42 |
| $7.42 |
| 384020-1 |
| GROMMET |
| 2 |
| EA |
| $5.26 |
| $10.52 |
| 384020-1 |
| GROMMET |
| 2 |
| EA |
| $5.26 |
| $10.52 |
| 384020-1 |
| GROMMET |
| 2 |
| EA |
| $5.26 |
| $10.52 |
| 384020-1 |
| GROMMET |
| 2 |
| EA |
| $5.26 |
| $10.52 |
| 384020-1 |
| GROMMET |
| 2 |
| EA |
| $5.26 |
| $10.52 |
| 384020-1 |
| GROMMET |
| 1 |
| EA |
| $5.26 |
| $5.26 |
| 384020-1 |
| GROMMET |
| 3 |
| EA |
| $5.26 |
| $15.78 |
| 384020-1 |
| GROMMET |
| 2 |
| EA |
| $5.26 |
| $10.52 |
| 384020-1 |
| GROMMET |
| 2 |
| EA |
| $5.26 |
| $10.52 |
| 384020-1 |
| GROMMET |
| 2 |
| EA |
| $5.26 |
| $10.52 |
| PART NUMBER |
| DESCRIPTION |
| QTY |
| UOM |
| COST |
| EXT. COST |
| 384020-1 |
| GROMMET |
| 2 |
| EA |
| $5.26 |
| $10.52 |
| 384020-1 |
| GROMMET |
| 2 |
| EA |
| $5.26 |
| $10.52 |
| 384020-3 |
| GROMMET |
| 2 |
| EA |
| $5.32 |
| $10.64 |
| 384020-3 |
| GROMMET |
| 2 |
| EA |
| $5.32 |
| $10.64 |
| 384020-3 |
| GROMMET |
| 1 |
| EA |
| $5.32 |
| $5.32 |
| 384020-3 |
| GROMMET |
| 1 |
| EA |
| $5.32 |
| $5.32 |
| 384020-3 |
| GROMMET |
| 2 |
| EA |
| $5.32 |
| $10.64 |
| 384020-3 |
| GROMMET |
| 2 |
| EA |
| $5.32 |
| $10.64 |
| 384020-3 |
| GROMMET |
| 2 |
| EA |
| $5.32 |
| $10.64 |
| 369884-49-FRD |
| CHAMBER MINUTEMAN (FIRED) |
| 1 |
| EA |
| $500,000.00 |
| $500,000.00 |
| 369884-49-FRD |
| CHAMBER MINUTEMAN (FIRED) |
| 1 |
| EA |
| $500,000.00 |
| $500,000.00 |
| 383617-409-REP |
| IGNITER, ROCKET MOTOR |
| 2 |
| EA |
| $500.00 |
| $1,000.00 |
| 1216845-9-FRD |
| LITVC SYSTEM, FIRED |
| 1 |
| EA |
| $3,000.00 |
| $3,000.00 |
| GEN-1024 |
| NOZZLE, FIRED, DISSECT |
| 1 |
| EA |
| $80,000.00 |
| $80,000.00 |
| 1213706-98553 |
| EXIT CONE ASSY, TRUNCATED |
| 1 |
| EA |
| $7,000.00 |
| $7,000.00 |
| 367950-1 |
| BOLT |
| 3 |
| EA |
| $0.92 |
| $2.76 |
| 1153803-1 |
| WEATHERSEAL |
| 1 |
| EA |
| $23.92 |
| $23.92 |
| 384744-9-AGING |
| ROCKET MOTOR, AGING |
| 1 |
| EA |
| $500,000.00 |
| $500,000.00 |
| 384023-9-REP |
| NOZZLE ASSEMBLY |
| 1 |
| EA |
| $80,000.00 |
| $80,000.00 |
| 1208682-59 |
| MOTOR ASSEMBLY |
| 1 |
| EA |
| $20,000.00 |
| $20,000.00 |
| 382100-FRM-903 |
| ROCKET MOTOR DISASSEMBLED |
| 1 |
| EA |
| $500,000.00 |
| $500,000.00 |
| 384744-9-AGING |
| ROCKET MOTOR, AGING |
| 1 |
| EA |
| $500,000.00 |
| $500,000.00 |
| 384744-9-AGING |
| ROCKET MOTOR, AGING |
| 1 |
| EA |
| $500,000.00 |
| $500,000.00 |
| NAS1057T6-012 |
| SPACER (WASHER) |
| 4 |
| EA |
| $2.60 |
| $10.40 |
| 1369925 |
| IGNITER GAS GEN |
| 1 |
| EA |
| $1,300.00 |
| $1,300.00 |
| 1369925 |
| IGNITER GAS GEN |
| 1 |
| EA |
| $1,300.00 |
| $1,300.00 |
| 1369925 |
| IGNITER GAS GEN |
| 1 |
| EA |
| $1,300.00 |
| $1,300.00 |
| 1369925 |
| IGNITER GAS GEN |
| 1 |
| EA |
| $1,300.00 |
| $1,300.00 |
| 1369925 |
| IGNITER GAS GEN |
| 1 |
| EA |
| $1,300.00 |
| $1,300.00 |
| 1369925 |
| IGNITER GAS GEN |
| 1 |
| EA |
| $1,300.00 |
| $1,300.00 |
| 1369925 |
| IGNITER GAS GEN |
| 1 |
| EA |
| $1,300.00 |
| $1,300.00 |
| 7300-11 |
| SWITCH, ARM/DISARM |
| 1 |
| EA |
| $1,217.60 |
| $1,217.60 |
| 7300-11 |
| SWITCH, ARM/DISARM |
| 1 |
| EA |
| $1,217.60 |
| $1,217.60 |
| 7300-11 |
| SWITCH, ARM/DISARM |
| 1 |
| EA |
| $1,217.60 |
| $1,217.60 |
| 1106909 |
| GAS GENERATOR PRESSURE |
| 1 |
| EA |
| $900.00 |
| $900.00 |
| 1106909 |
| GAS GENERATOR PRESSURE |
| 1 |
| EA |
| $900.00 |
| $900.00 |
| 1106909 |
| GAS GENERATOR PRESSURE |
| 1 |
| EA |
| $900.00 |
| $900.00 |
| 1106909 |
| GAS GENERATOR PRESSURE |
| 1 |
| EA |
| $900.00 |
| $900.00 |
| 1106909 |
| GAS GENERATOR PRESSURE |
| 1 |
| EA |
| $900.00 |
| $900.00 |
| 1106909 |
| GAS GENERATOR PRESSURE |
| 1 |
| EA |
| $900.00 |
| $900.00 |
| 383618-17213 |
| IGNITER, AGING |
| 1 |
| EA |
| $6,240.00 |
| $6,240.00 |
| 383618-209 |
| IGNITER, REHABED |
| 1 |
| EA |
| $6,240.00 |
| $6,240.00 |
| 1106909 |
| GAS GENERATOR PRESSURE |
| 1 |
| EA |
| $900.00 |
| $900.00 |
| 1107216 |
| GAS GENERATOR, AGED TVC |
| 1 |
| EA |
| $900.00 |
| $900.00 |
| PART NUMBER |
| DESCRIPTION |
| QTY |
| UOM |
| COST |
| EXT. COST |
| 1107216 |
| GAS GENERATOR, AGED TVC |
| 1 |
| EA |
| $900.00 |
| $900.00 |
| 1107216 |
| GAS GENERATOR, AGED TVC |
| 1 |
| EA |
| $900.00 |
| $900.00 |
| 1107216 |
| GAS GENERATOR, AGED TVC |
| 1 |
| EA |
| $900.00 |
| $900.00 |
| 1106909 |
| GAS GENERATOR PRESSURE |
| 1 |
| EA |
| $21,550.00 |
| $21,550.00 |
| 383618-209 |
| IGNITER, REHABED |
| 1 |
| EA |
| $6,240.00 |
| $6,240.00 |
| 383618-209-REP |
| IGNITER M/M FIELD RETURN |
| 1 |
| EA |
| $3,200.00 |
| $3,200.00 |
| 383618-209-REP |
| IGNITER M/M FIELD RETURN |
| 1 |
| EA |
| $3,200.00 |
| $3,200.00 |
| 1209682-9 |
| ORDNANCE SUBASSEMBLY |
| 1 |
| EA |
| $5,000.00 |
| $5,000.00 |
| 1106909 |
| GAS GENERATOR PRESSURE |
| 1 |
| EA |
| $900.00 |
| $900.00 |
| 1106909 |
| GAS GENERATOR PRESSURE |
| 1 |
| EA |
| $900.00 |
| $900.00 |
| 1106909 |
| GAS GENERATOR PRESSURE |
| 1 |
| EA |
| $900.00 |
| $900.00 |
| 383618-209-REP |
| IGNITER M/M FIELD RETURN |
| 1 |
| EA |
| $3,200.00 |
| $3,200.00 |
| 1107216 |
| GAS GENERATOR, AGED TVC |
| 1 |
| EA |
| $900.00 |
| $900.00 |
| 1107216 |
| GAS GENERATOR, AGED TVC |
| 1 |
| EA |
| $900.00 |
| $900.00 |
| 1107216 |
| GAS GENERATOR, AGED TVC |
| 1 |
| EA |
| $900.00 |
| $900.00 |
| 1107216 |
| GAS GENERATOR, AGED TVC |
| 1 |
| EA |
| $900.00 |
| $900.00 |
| 1107216 |
| GAS GENERATOR, AGED TVC |
| 1 |
| EA |
| $900.00 |
| $900.00 |
| 1107216 |
| GAS GENERATOR, AGED TVC |
| 1 |
| EA |
| $900.00 |
| $900.00 |
| 1106909 |
| GAS GENERATOR PRESSURE |
| 1 |
| EA |
| $900.00 |
| $900.00 |
| 1106909 |
| GAS GENERATOR PRESSURE |
| 1 |
| EA |
| $900.00 |
| $900.00 |
| 1106909 |
| GAS GENERATOR PRESSURE |
| 1 |
| EA |
| $900.00 |
| $900.00 |
| 1106909-REP |
| GAS GEN ROLL CONTROL |
| 1 |
| EA |
| $25,863.00 |
| $25,863.00 |
| 1107216-REP |
| GAS GENERATOR |
| 1 |
| EA |
| $20,185.00 |
| $20,185.00 |
| 1106909-REP |
| GAS GEN ROLL CONTROL |
| 1 |
| EA |
| $25,863.00 |
| $25,863.00 |
| 1107216-REP |
| GAS GENERATOR |
| 1 |
| EA |
| $20,185.00 |
| $20,185.00 |
| 1106909 |
| GAS GENERATOR PRESSURE |
| 1 |
| EA |
| $21,550.00 |
| $21,550.00 |
| 1106909-REP |
| GAS GEN ROLL CONTROL |
| 1 |
| EA |
| $25,863.00 |
| $25,863.00 |
| 1107216-REP |
| GAS GENERATOR |
| 1 |
| EA |
| $20,185.00 |
| $20,185.00 |
| 383617-99/112 |
| IGNITER, M/M, AGED |
| 1 |
| EA |
| $600.00 |
| $600.00 |
| 383617-99/112 |
| IGNITER, M/M, AGED |
| 1 |
| EA |
| $600.00 |
| $600.00 |
| 383617-99/112 |
| IGNITER, M/M, AGED |
| 1 |
| EA |
| $600.00 |
| $600.00 |
| 383617-99/112 |
| IGNITER, M/M, AGED |
| 1 |
| EA |
| $600.00 |
| $600.00 |
| 383617-99/112 |
| IGNITER, M/M, AGED |
| 1 |
| EA |
| $600.00 |
| $600.00 |
| 383617-99/112 |
| IGNITER, M/M, AGED |
| 1 |
| EA |
| $600.00 |
| $600.00 |
| 383617-99/112 |
| IGNITER, M/M, AGED |
| 1 |
| EA |
| $600.00 |
| $600.00 |
| 383617-99/112 |
| IGNITER, M/M, AGED |
| 1 |
| EA |
| $600.00 |
| $600.00 |
| 1178400-1 |
| ADAPTER FIRING |
| 1 |
| EA |
| $500.00 |
| $500.00 |
| LUM383617-99 |
| IGNITER AGING W/O S AND A |
| 1 |
| EA |
| $600.00 |
| $600.00 |
| LUM383617-99 |
| IGNITER AGING W/O S AND A |
| 1 |
| EA |
| $900.00 |
| $900.00 |
| LUM383617-99 |
| IGNITER AGING W/O S AND A |
| 1 |
| EA |
| $900.00 |
| $900.00 |
| LUM383617-99 |
| IGNITER AGING W/O S AND A |
| 1 |
| EA |
| $600.00 |
| $600.00 |
| LUM383617-99 |
| IGNITER AGING W/O S AND A |
| 1 |
| EA |
| $900.00 |
| $900.00 |
| LUM383617-99 |
| IGNITER AGING W/O S AND A |
| 1 |
| EA |
| $600.00 |
| $600.00 |
| 1106909-REP |
| GAS GEN ROLL CONTROL |
| 1 |
| EA |
| $25,863.00 |
| $25,863.00 |
| PART NUMBER |
| DESCRIPTION |
| QTY |
| UOM |
| COST |
| EXT. COST |
| 1107216 |
| GAS GENERATOR, AGED TVC |
| 1 |
| EA |
| $20,185.00 |
| $20,185.00 |
| 1107216-REP |
| GAS GENERATOR |
| 1 |
| EA |
| $20,185.00 |
| $20,185.00 |
| 1107216 |
| GAS GENERATOR, AGED TVC |
| 1 |
| EA |
| $20,185.00 |
| $20,185.00 |
| 1107216 |
| GAS GENERATOR, AGED TVC |
| 1 |
| EA |
| $20,185.00 |
| $20,185.00 |
| 1107216 |
| GAS GENERATOR, AGED TVC |
| 1 |
| EA |
| $20,185.00 |
| $20,185.00 |
| 1107216 |
| GAS GENERATOR, AGED TVC |
| 1 |
| EA |
| $20,185.00 |
| $20,185.00 |
| 1107216 |
| GAS GENERATOR, AGED TVC |
| 1 |
| EA |
| $20,185.00 |
| $20,185.00 |
| 1107216 |
| GAS GENERATOR, AGED TVC |
| 1 |
| EA |
| $20,185.00 |
| $20,185.00 |
| 1107216 |
| GAS GENERATOR, AGED TVC |
| 1 |
| EA |
| $20,185.00 |
| $20,185.00 |
| 1107216 |
| GAS GENERATOR, AGED TVC |
| 1 |
| EA |
| $20,185.00 |
| $20,185.00 |
| 1107216 |
| GAS GENERATOR, AGED TVC |
| 1 |
| EA |
| $20,185.00 |
| $20,185.00 |
| 1107216 |
| GAS GENERATOR, AGED TVC |
| 1 |
| EA |
| $20,185.00 |
| $20,185.00 |
| 1106909-REP |
| GAS GEN ROLL CONTROL |
| 1 |
| EA |
| $25,863.00 |
| $25,863.00 |
| 1106909-REP |
| GAS GEN ROLL CONTROL |
| 1 |
| EA |
| $25,863.00 |
| $25,863.00 |
| 1107216-REP |
| GAS GENERATOR |
| 1 |
| EA |
| $20,185.00 |
| $20,185.00 |
| 1107216-REP |
| GAS GENERATOR |
| 1 |
| EA |
| $20,185.00 |
| $20,185.00 |
| 1107216 |
| GAS GENERATOR, AGED TVC |
| 1 |
| EA |
| $20,185.00 |
| $20,185.00 |
| 1107216 |
| GAS GENERATOR, AGED TVC |
| 1 |
| EA |
| $20,185.00 |
| $20,185.00 |
| 1107216 |
| GAS GENERATOR, AGED TVC |
| 1 |
| EA |
| $20,185.00 |
| $20,185.00 |
| 1107216 |
| GAS GENERATOR, AGED TVC |
| 1 |
| EA |
| $20,185.00 |
| $20,185.00 |
| 1106909 |
| GAS GENERATOR PRESSURE |
| 1 |
| EA |
| $25,863.00 |
| $25,863.00 |
| 1106909 |
| GAS GENERATOR PRESSURE |
| 1 |
| EA |
| $25,865.00 |
| $25,865.00 |
| 1106909 |
| GAS GENERATOR PRESSURE |
| 1 |
| EA |
| $25,863.00 |
| $25,863.00 |
| 1106909 |
| GAS GENERATOR PRESSURE |
| 1 |
| EA |
| $25,863.00 |
| $25,863.00 |
| 1106909 |
| GAS GENERATOR PRESSURE |
| 1 |
| EA |
| $25,863.00 |
| $25,863.00 |
| 1106909 |
| GAS GENERATOR PRESSURE |
| 1 |
| EA |
| $25,863.00 |
| $25,863.00 |
| 383617-17214 |
| IGNITER, AGING |
| 1 |
| EA |
| $6,000.00 |
| $6,000.00 |
| 384517-29-REP |
| EXTENSION ASSY EXIT |
| 1 |
| EA |
| $7,756.00 |
| $7,756.00 |
| 1208693-9 |
| NOZZLE ASSEMBLY, MODIFIED |
| 1 |
| EA |
| $80,000.00 |
| $80,000.00 |
| 1110067-1-REP |
| TUBE ASSY EXHAUST RH TVC |
| 1 |
| EA |
| $4,000.00 |
| $4,000.00 |
| 1110067-1-REP |
| TUBE ASSY EXHAUST RH TVC |
| 1 |
| EA |
| $4,000.00 |
| $4,000.00 |
| 1110067-3-REP |
| TUBE ASSEMBLY, RIGHT HAND |
| 1 |
| EA |
| $4,000.00 |
| $4,000.00 |
| 384023-9-REP |
| NOZZLE ASSEMBLY |
| 1 |
| EA |
| $80,000.00 |
| $80,000.00 |
| 383767-9-REP |
| SHIELD, BASE HEAT |
| 1 |
| EA |
| $7,600.00 |
| $7,600.00 |
| 383767-9-REP |
| SHIELD, BASE HEAT |
| 1 |
| EA |
| $7,600.00 |
| $7,600.00 |
| 384517-29-REP |
| EXTENSION ASSY EXIT |
| 1 |
| EA |
| $7,756.00 |
| $7,756.00 |
| 1110067-1 |
| TUBE ASSY EXHAUST R/H TVC |
| 1 |
| EA |
| $3,500.00 |
| $3,500.00 |
| 1110067-1 |
| TUBE ASSY EXHAUST R/H TVC |
| 1 |
| EA |
| $1,200.00 |
| $1,200.00 |
| 1110067-1 |
| TUBE ASSY EXHAUST R/H TVC |
| 1 |
| EA |
| $1,200.00 |
| $1,200.00 |
| 1110067-1-REP |
| TUBE ASSY EXHAUST RH TVC |
| 1 |
| EA |
| $4,000.00 |
| $4,000.00 |
| 1110067-1-REP |
| TUBE ASSY EXHAUST RH TVC |
| 1 |
| EA |
| $4,000.00 |
| $4,000.00 |
| 1208693-9 |
| NOZZLE ASSEMBLY, MODIFIED |
| 1 |
| EA |
| $80,000.00 |
| $80,000.00 |
| 384023-9-REP |
| NOZZLE ASSEMBLY |
| 1 |
| EA |
| $80,000.00 |
| $80,000.00 |
| 384517-29-REP |
| EXTENSION ASSY EXIT |
| 1 |
| EA |
| $7,756.00 |
| $7,756.00 |
| 384517-29-REP |
| EXTENSION ASSY EXIT |
| 1 |
| EA |
| $7,756.00 |
| $7,756.00 |
| PART NUMBER |
| DESCRIPTION |
| QTY |
| UOM |
| COST |
| EXT. COST |
| 1109992-5-REP |
| MANIFOLD GAS GEN TVC |
| 1 |
| EA |
| $4,000.00 |
| $4,000.00 |
| 1110067-1-REP |
| TUBE ASSY EXHAUST RH TVC |
| 1 |
| EA |
| $4,000.00 |
| $4,000.00 |
| 384517-29-REP |
| EXTENSION ASSY EXIT |
| 1 |
| EA |
| $7,756.00 |
| $7,756.00 |
| 1213706-19 |
| EXIT CONE ASSY, TRUNCATED |
| 1 |
| EA |
| $1.00 |
| $1.00 |
| 1213706-39 |
| EXIT CONE ASSY, TRUNCATED |
| 1 |
| EA |
| $1.50 |
| $1.50 |
| 384023-9-REP |
| NOZZLE ASSEMBLY |
| 1 |
| EA |
| $80,000.00 |
| $80,000.00 |
| 384023-9-REP |
| NOZZLE ASSEMBLY |
| 1 |
| EA |
| $80,000.00 |
| $80,000.00 |
| 384517-29 |
| EXTENSION ASSY EXIT CONE |
| 1 |
| EA |
| $6,000.00 |
| $6,000.00 |
| 384517-29-REP |
| EXTENSION ASSY EXIT |
| 1 |
| EA |
| $7,756.00 |
| $7,756.00 |
| 1111915-1 |
| SPACER |
| 1 |
| EA |
| $13.25 |
| $13.25 |
| 383725-9 |
| CLIP |
| 1 |
| EA |
| $58.56 |
| $58.56 |
| 1149638-1 |
| COVER |
| 2 |
| EA |
| $56.56 |
| $113.12 |
| 384024-5-REP |
| COVER, PROTECTIVE |
| 1 |
| EA |
| $10.00 |
| $10.00 |
| 384024-5-REP |
| COVER, PROTECTIVE |
| 1 |
| EA |
| $10.00 |
| $10.00 |
| 1111915-1 |
| SPACER |
| 1 |
| EA |
| $13.25 |
| $13.25 |
| 383725-9 |
| CLIP |
| 1 |
| EA |
| $58.56 |
| $58.56 |
| 1149625-19-REP |
| J-BOX HARD VALVE M/M |
| 1 |
| EA |
| $500.00 |
| $500.00 |
| 1149625-9-REP |
| J-B0X SOFT VALVE M/M |
| 1 |
| EA |
| $500.00 |
| $500.00 |
| 384024-5-REP |
| COVER, PROTECTIVE |
| 1 |
| EA |
| $10.00 |
| $10.00 |
| 1208694-1 |
| BRACKET, ACTUATOR |
| 1 |
| EA |
| $210.00 |
| $210.00 |
| 383725-49 |
| CLIP, MOUNTING |
| 2 |
| EA |
| $23.71 |
| $47.42 |
| 384024-5 |
| COVER, PROTECTIVE |
| 1 |
| EA |
| $10.00 |
| $10.00 |
| 384024-5 |
| COVER, PROTECTIVE |
| 1 |
| EA |
| $10.00 |
| $10.00 |
| 367950-1 |
| BOLT |
| 108 |
| EA |
| $0.92 |
| $99.36 |
| 4075KF |
| CLAMP, PRESSURE VESSLE |
| 1 |
| EA |
| $245.00 |
| $245.00 |
| 1107536-1 |
| SLEEVE |
| 8 |
| EA |
| $78.50 |
| $628.00 |
| 1107537-1 |
| INSULATOR |
| 16 |
| EA |
| $373.00 |
| $5,968.00 |
| 367950-1 |
| BOLT |
| 220 |
| EA |
| $0.92 |
| $202.40 |
| 1107055-1 |
| SUPPORT |
| 2 |
| EA |
| $30.00 |
| $60.00 |
| 1209678-1 |
| PLATE |
| 1 |
| EA |
| $45.00 |
| $45.00 |
| 1107055-1 |
| SUPPORT |
| 6 |
| EA |
| $30.00 |
| $180.00 |
| 1110544-5 |
| INSULATOR |
| 6 |
| EA |
| $100.00 |
| $600.00 |
| 1148350-9 |
| SUPPORT |
| 1 |
| EA |
| $64.00 |
| $64.00 |
| NAS1351-6-32P |
| SCREW, SOCKET HEAD CAP |
| 13 |
| EA |
| $9.00 |
| $117.00 |
| TSR1AB04B |
| SPLICE, TINEL LOCK |
| 79 |
| EA |
| $23.00 |
| $1,817.00 |
| 384024-5-REP |
| COVER, PROTECTIVE |
| 1 |
| EA |
| $10.00 |
| $10.00 |
| 383725-49 |
| CLIP, MOUNTING |
| 2 |
| EA |
| $23.71 |
| $47.42 |
| 383725-49 |
| CLIP, MOUNTING |
| 2 |
| EA |
| $23.71 |
| $47.42 |
| 384024-5-REP |
| COVER, PROTECTIVE |
| 1 |
| EA |
| $10.00 |
| $10.00 |
| TMS-3/4-1.5-9 |
| MARKING, MIL-I-81531 |
| 40 |
| EA |
| $1.52 |
| $60.80 |
| TMS-3/8-1.5-9 |
| MARKING, MIL-I-81531 |
| 40 |
| EA |
| $0.81 |
| $32.40 |
| 383725-49 |
| CLIP, MOUNTING |
| 4 |
| EA |
| $25.00 |
| $100.00 |
| 1149625-9-REP |
| J-B0X SOFT VALVE M/M |
| 1 |
| EA |
| $500.00 |
| $500.00 |
| 1149638-1 |
| COVER |
| 2 |
| EA |
| $56.56 |
| $113.12 |
| 384024-5-REP |
| COVER, PROTECTIVE |
| 1 |
| EA |
| $10.00 |
| $10.00 |
| PART NUMBER |
| DESCRIPTION |
| QTY |
| UOM |
| COST |
| EXT. COST |
| 384024-5-REP |
| COVER, PROTECTIVE |
| 1 |
| EA |
| $10.00 |
| $10.00 |
| 1109965-1 |
| SUPPORT |
| 1 |
| EA |
| $31.00 |
| $31.00 |
| NAS1352N3-10 |
| SCREW |
| 29 |
| EA |
| $4.00 |
| $116.00 |
| 1110470-3 |
| INSERT |
| 1 |
| EA |
| $300.00 |
| $300.00 |
| NAS1595-12 |
| O-RING |
| 1 |
| EA |
| $2.60 |
| $2.60 |
| 1149625-19 |
| JUNCTION BOX |
| 1 |
| EA |
| $500.00 |
| $500.00 |
| 1149638-1 |
| COVER |
| 2 |
| EA |
| $56.56 |
| $113.12 |
| 383905-1 |
| GROMMET |
| 1 |
| EA |
| $5.69 |
| $5.69 |
| AS7014A04A06 |
| BOLT |
| 55 |
| EA |
| $83.99 |
| $4,619.45 |
| AS7014A04A06 |
| BOLT |
| 21 |
| EA |
| $83.99 |
| $1,763.79 |
| 1178952-2 |
| GASKET, FLEXITALLIC |
| 2 |
| EA |
| $28.73 |
| $57.46 |
| AS7014A05A06 |
| BOLT, TENSION, HIGH TEMP |
| 3 |
| EA |
| $342.00 |
| $1,026.00 |
| AS7014A05A06 |
| BOLT, TENSION, HIGH TEMP |
| 98 |
| EA |
| $83.99 |
| $8,231.02 |
| AS7014A05A07 |
| BOLT |
| 100 |
| EA |
| $83.99 |
| $8,399.00 |
| SPC-S7025A1B66A |
| CLAMP |
| 1 |
| EA |
| $6.50 |
| $6.50 |
| 384024-5-REP |
| COVER, PROTECTIVE |
| 1 |
| EA |
| $10.00 |
| $10.00 |
| 1149638-1 |
| COVER |
| 2 |
| EA |
| $56.00 |
| $112.00 |
| 384024-5-REP |
| COVER, PROTECTIVE |
| 1 |
| EA |
| $10.00 |
| $10.00 |
| 14E00652517 |
| ADAPTER OFR MOTOR SE |
| 1 |
| 01E00804 |
| HARNESS, FWD STAND |
| 1 |
| 01E00800 |
| CRADLE SECTION |
| 1 |
| 01E00800 |
| CRADLE SECTION |
| 1 |
| 01E00804 |
| HARNESS, FWD STAND |
| 1 |
| 01E00800 |
| CRADLE SECTION |
| 1 |
| 01E00800 |
| CRADLE SECTION |
| 1 |
| 01E00800 |
| CRADLE SECTION |
| 1 |
| 01E00800 |
| CRADLE SECTION |
| 1 |
| 01E00877 |
| FIXTURE, HYDRO-TEST |
| 1 |
| 12E00116 |
| DOLLY, MM RSLP MOTOR |
| 1 |
| 12E00920 |
| CLOSURE, MINUTEMAN N |
| 1 |
| 12E00920 |
| CLOSURE, MINUTEMAN N |
| 1 |
| 12E00920 |
| CLOSURE, MINUTEMAN N |
| 1 |
| 12E00920 |
| CLOSURE, MINUTEMAN N |
| 1 |
| 83008J01994 |
| FIXTURE HYDROSTATIC |
| 1 |
| 6625BU |
| STAND, FSU DISPLAY |
| 1 |
| 01E00804 |
| HARNESS, FWD STAND |
| 1 |
| 01E00624 |
| ADAPTER FORK LIFT SH |
| 1 |
| M57 MOTOR TEST |
| PLASMA CAP SIGNAL CO |
| 1 |
| M57 MOTOR TEST |
| PLASMA CAP SIGNAL CO |
| 1 |
| 83008J02159 |
| FIXTURE, NOZZLE LEAK |
| 1 |
| 83008J02172 |
| SHROUD, PLUGGING |
| 1 |
| 83008J02175 |
| CAM, HARD STOP |
| 1 |
| 83008J02176 |
| END MILL, CASE CUTTI |
| 1 |
| 83008J02177 |
| PLATE, SLIP |
| 1 |
| PART NUMBER |
| DESCRIPTION |
| QTY |
| UOM |
| COST |
| EXT. COST |
| 83008J02179 |
| TRAP ARM, PLUGGING |
| 1 |
| 83008J02180 |
| EXCISING TOOL, AUTOM |
| 1 |
| 83008J02229 |
| CHOCK, HARNESSED MOT |
| 1 |
| 83008J02230 |
| FIXTURE, TRANSPORTAT |
| 1 |
| 83008J02304 |
| EXCISION TOOL, PROPE |
| 1 |
| 83008J02306 |
| CHOCK, TRANSPORTATIO |
| 1 |
| 83008S02263 |
| PROPELLANT EXCISE TE |
| 1 |
| 83008J02533 |
| LIFTING FIXTURE |
| 1 |
| 2U141710-01 |
| ADAPTER DIFFUSER |
| 1 |
| 2U141711-01 |
| ADAPTER LOAD TEST |
| 1 |
| 2U141712-01 |
| CHOCK MOTOR |
| 1 |
| T17064-1 |
| BRACKET MOUNTING |
| 1 |
| T17064-1 |
| BRACKET MOUNTING |
| 1 |
| T17064-1 |
| BRACKET MOUNTING |
| 1 |
| 1045-4909-001 |
| MANIFOLD DETONATING |
| 1 |
| 1045-4909-001 |
| MANIFOLD DETONATING |
| 1 |
| T17059-1 |
| PLATE VIBRATION |
| 1 |
| T17059-2 |
| PLATE VIBRATION |
| 1 |
| T17059-3 |
| PLATE VIBRATION |
| 1 |
| 2U141716-01 |
| REMOVAL TOOL |
| 1 |
| 2U141723-01 |
| PLUG HOUSING |
| 1 |
| 2U104909-201 |
| BEAM LIFTING |
| 1 |
| 4U120759 |
| PROTECTOR, POLAR BOSS |
| 1 |
| 3268962-100 |
| FIXTURE ASSEMBLY |
| 1 |
| 3268962-100 |
| FIXTURE ASSEMBLY |
| 1 |
| 3268962-103 |
| FIXTURE ASSEMBLY |
| 1 |
| 3235310 |
| HOIST RIG SUPPORT |
| 1 |
| 3235310 |
| HOIST RIG SUPPORT |
| 1 |
| 3268962-101-103 |
| CART ASSEMBLY |
| 1 |
| PART NUMBER |
| DESCRIPTION |
| QTY |
| UOM |
| COST |
| EXT. COST |
| 3268962-101-103 |
| CART ASSEMBLY |
| 1 |
| 3268962-101 |
| CART ASSEMBLY |
| 1 |
| 3268962-101 |
| BRACKETS LH |
| 1 |
| 3268962-101 |
| BRACKETS LH |
| 1 |
| 3268962-101 |
| BRACKETS RH |
| 1 |
| 3268962-101 |
| BRACKETS RH |
| 1 |
| 2U141599-01 |
| RING HANDLING |
| 1 |
| 2U141600-01 |
| SPACER / ADAPTER |
| 1 |
| 2U141633-01 |
| DELUGE WATER |
| 1 |
| 3268892 |
| MONITOR OVERSPEED |
| 1 |
| 3262962 |
| FIXTURE CALIBRATION LVDT |
| 1 |
| NONE |
| ANALYZER PARTICLE SIZE |
| 1 |
| 3235310 |
| PANE HYDRAULIC SUPPLY |
| 1 |
| 3268962 |
| ECE TURBO HYDRAULIC |
| 1 |
| 3275534-4 |
| STAND ENEC G/B |
| 1 |
| 3549440 |
| STAND ENEC TURB |
| 1 |
| 3268698-1 |
| ASSEMBLY TEST PANEL |
| 1 |
| 3268962 |
| STAND TVA TEST 2ND |
| 1 |
| 3268962 |
| TANKS HELIUM BOTTLES |
| 1 |
| 3268962 |
| ACTUATOR SERVO SUPPLY |
| 1 |
| 3268962 |
| ACTUATOR SERVO RETURN |
| 1 |
| TOOL NUMBER |
| DESCRIPTION |
| QTY |
| UOM |
| COST |
| EXT. COST |
| T2000014-001 |
| RECOVERY SYSTEM, FREON |
| 1 |
| T2001966-001 |
| MOLD COMPRESSION |
| 1 |
| T2001967-001 |
| MOLD COMPRESSION |
| 1 |
| T2000015-001 |
| SUPPORT STAND, VERTICAL, TORIDAL TANK DRAIN |
| 1 |
| T416502-16-001 |
| FLANGE, ASSY NOZZLE |
| 1 |
| T416431-301-023 |
| HANDLING RING AFT |
| 1 |
| T430231-201-001 |
| ANTI-FLIGHT, HOWRE |
| 1 |
| T1042124-002 |
| TEMPERATURE CONDITIONING CAR |
| 1 |
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