SOW_STANDARD Missile-6 MK37 AFD 6520476 FY25 OA_rev2.docx
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- Attached to
- OA Testing of SM6 MK37
- Solicitation number
- N00174-25-SIMACQ-E2-0034
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This Statement of Work (SOW) outlines Ordnance Assessment (OA) testing for the Standard Missile-6 (SM-6) Block I MK37 Arming/Firing Device (AFD), Part Number 6520476. The testing will be conducted at Pacific Scientific Energetic Materials Company (PSEMC) in Chandler, Arizona and involves comprehensive evaluation of twenty-four (24) Government Furnished fleet-returned units from Naval Surface Warfare Center, Indian Head Division (NSWC IHD), plus one additional test setup unit from PSEMC.
The testing protocol includes multiple phases: baseline visual inspection, artificial aging, non-destructive testing, environmental testing, and all-fire tests. Specific tests encompass radiographic X-ray examination, electrical testing, seal integrity checks, transportation shock and vibration tests, temperature and humidity evaluations, and shipboard vibration testing. The contractor must deliver a test procedure work order 10 days prior to testing and a comprehensive technical report within 30 days after completing destructive testing. The solicitation number is N00174-25-SIMACQ-E2-0034, and the opportunity is classified as a Special Notice by the Department of the Navy Naval Sea Systems Command.
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SOW-20250301
28 Feb 2025
STATEMENT OF WORK FOR
ORDNANCE ASSESSMENT TESTING OF THE
STANDARD MISSILE-6 (SM-6)
MK37 ARMING FIRE DEVICE, PART NUMBER L6520476
1. INTRODUCTION.
Scope. This statement of work (SOW) defines the efforts to conduct Ordnance Assessment (OA) testing of the STANDARD Missile-6 (SM-6) Block (Blk) I MK 37 Arming/Firing Device (AFD) Part Number (P/N) 6520476 at Pacific Scientific Energetic Materials Company (PSEMC) in Chandler, Arizona. Testing will include artificial aging, non-destructive, environmental, and ballistic testing of twenty-four (24) Government Furnished fleet-returned units provided by Naval Surface Warfare Center, Indian Head Division (NSWC IHD). One (1) additional test setup unit, P/N 105200-1, shall be supplied by PSEMC.
On-Site Visit and Coordination.
PSEMC shall notify NSWC IHD at least fourteen (14) business days prior to All-Fire testing, so technical representative(s) can make travel arrangements to witness testing.
Government Furnished Materials (GFM).
The Government will furnish the following Government Furnished Property (GFP) to the contractor for use in performance of this contract:
MK37 AFD (Navy P/N 6520476, PSEMC P/N 105200-1) 24
· The material will be delivered at the Government’s expense to the contractor’s facility.
· Only the material listed above and on the GFP Attachment will be furnished by the Government. All other material required for performance of this contract shall be furnished by the contractor.
· Within 30 days after GFM is determined by the contractor to be lost, damaged, destroyed, no longer usable, or no longer needed for the performance of the contract, the contractor shall notify the Contracting Officer, in writing, thereof.
· Disposition instructions for the GFM are as follows: Material will be destroyed by the contractor.
APPLICABLE DOCUMENTS.
Drawings: MK37 Arming/Firing Device, 6520476 Test Procedures: Pacific Scientific Energetic Materials Company Acceptance Test Procedure (ATP) Document No. ATPL6520476 Specification:
Critical Item Product Fabrication Specification, Arming-Firing Device, Rocket Motor, MK 37 Mod 0, AEGIS ER Booster, WS-32915
REQUIREMENTS.
A work order shall be delivered prior to testing in accordance with CDRL A001.
All test results & reports shall be delivered in accordance with CDRL A002.
Artificial Aging Twenty-two (22) units in Test Matrix.
shall undergo artificial aging prior to beginning non-destructive Testing (NDT) in Section 3.2.2. Baseline visual inspection shall be conducted prior to artificial aging IAW Section 3.2.2.1. Artificial aging schedule shall be provided by Government TPOC prior to contract award.
Unit Testing
Unit testing shall be performed on twenty-four (24) Government Furnished AFDs and one (1) test setup unit (TSU) provided by PSEMC. Units with lot numbers are listed in Test Matrix.
. Testing shall be performed in accordance with ATP 6520476 (current revision) and in accordance with tests as shown in Test Matrix.
. If tests listed in Test Matrix.
are not included in the PSEMC ATP, tests shall be conducted in accordance with PSEMC local instructions and in accordance with drawings in Section 2. The test sequence shown in Test Matrix.
must be maintained throughout the test program.
Test Matrix.
Table 1. Test Matrix
| TEST |
| ATP Section Number |
| SOW Section Number |
| ESD14C001-008 |
| ESD15G001-009 |
| ESD16D001-010 |
| ESD17J002-001 |
| TOTAL |
| 1 |
| Visual Inspection |
| 6.2 |
| 3.2.2.1 |
| 6 |
| 6 |
| 6 |
| 6 |
| 24 |
| 2 |
| Radiographic (X-Ray) |
| - |
| 3.2.2.3 |
| 6 |
| 6 |
| 6 |
| 6 |
| 24 |
| 3 |
| Electrical Testing |
| 6.3 thru 6.6 |
| 3.2.2.5 |
| 1 |
| 1 |
| 4 |
| Seal Integrity |
| 6.7 |
| 3.2.2.7 |
| 1 |
| 1 |
| 5 |
| Artificial Aging |
| * |
| 3.1 |
| 6 |
| 6 |
| 5 |
| 5 |
| 22 |
| 6 |
| Visual Inspection |
| 6.2 |
| 3.2.2.1 |
| 6 |
| 6 |
| 5 |
| 5 |
| 22 |
| 7 |
| Electrical Testing |
| 6.3 thru 6.6 |
| 3.2.2.3 |
| 6 |
| 6 |
| 5 |
| 5 |
| 22 |
| 8 |
| Seal Integrity |
| 6.7 |
| 3.2.2.7 |
| 6 |
| 6 |
| 5 |
| 5 |
| 22 |
| 9 |
| Transportation Shock |
| 6.8 |
| 3.2.3.1 |
| 7 |
| 7 |
| 5 |
| 5 |
| 24 |
| 10 |
| Transportation Vibration |
| 6.9 |
| 3.2.3.3 |
| 7 |
| 7 |
| 5 |
| 5 |
| 24 |
| 11 |
| Temperature and Humidity |
| 6.13 |
| 3.2.3.3 |
| 7 |
| 7 |
| 5 |
| 5 |
| 24 |
| 12 |
| Shipboard Vibration |
| 6.14 |
| 3.2.3.6 |
| 7 |
| 7 |
| 5 |
| 5 |
| 24 |
| 13 |
| Visual Inspection |
| 6.2 |
| 3.2.2.1 |
| 7 |
| 7 |
| 5 |
| 5 |
| 24 |
| 14 |
| Radiographic (X-Ray) |
| - |
| 3.2.2.3 |
| 7 |
| 7 |
| 5 |
| 5 |
| 24 |
| 15 |
| Squib Output (+73F) |
| 7.2 |
| 3.2.4.1 |
| 7 |
| 7 |
| 5 |
| 5 |
| 24 |
*Artificial aging schedule to be provided by TPOC prior to contract award
Non-destructive Inspections and Electrical Tests.
Visual inspection shall be conducted on 24 units in Test Matrix.
in accordance with PSEMC ATPL6520476 Section 5.2. Additionally, visual inspection shall be conducted before and after specific tests listed in Table 1.
Radiographic X-Ray Examination shall be conducted on 24 units in Test Matrix.
in accordance with PSEMC radiographic procedures. This examination shall be conducted before artificial aging and after environmental testing, Section 3.2.3, as stated in Table 1.
Electrical Tests shall be conducted on 2 units prior to artificial aging and the remaining 22 units after Aging in Test Matrix.
in accordance with PSEMC ATPL6520476 Section 6.3 thru 6.6.
Seal Integrity (Alcohol Immersion) shall be conducted on 2 units prior to artificial aging and the remaining 22 units after artificial aging as shown in Test Matrix.
in accordance with PSEMC ATPL6520476 Section 6.7.
Environment Tests.
Transportation Shock testing shall be conducted on 24 units in Test Matrix.
in accordance with PSEMC ATPL6520476 Section 6.8 after Visual Inspection described in 3.2.2.1.
Transportation Vibration, Non-Operating, shall be conducted on 24 units in Test Matrix.
in accordance with PSEMC ATPL6520476 Section 6.9 after Visual Inspection described in 3.2.2.1.
Temperature and Humidity testing shall be conducted on 24 units in Test Matrix.
in accordance with PSEMC ATPL6520476 Section 6.13 after Visual Inspection described in 3.2.2.1.
Shipboard Vibration testing Insulation resistance shall be conducted on 24 units in Test Matrix.
in accordance with PSEMC ATPL6520476 Section 6.14 after Visual Inspection described in 3.2.2.1. A subsequent visual inspection shall be conducted after this testing.
Environment test results shall be recorded. A copy of test results, and, if necessary, associated non-conformance reports, shall be delivered.
Photographs shall be taken of the test setup for each environment test and copies delivered.
All-Fire Tests.
Squib Output shall be conducted on 24 units in Test Matrix.
in accordance with PSEMC ATPL6520476 Section 6.13 after Visual Inspection described in 3.2.2.1. Test units shall be fired at +73F.
DELIVERABLES.
See all deliverables in Table 2.
TEST PROCEDURE (Test Work Order) (CDRL A001). A copy of the work order(s) detailing the procedures in Test Matrix.
shall be provided for Government review/approval at least 10 days prior to the start of testing for NSWC IHD technical representative’s approval.
TECHNICAL REPORT - STUDY/SERVICES (Test Data) (CDRL A002). A copy of all non-destructive and destructive test results shall be provided to NSWC IHD within 30 days of completion of destructive testing. Non-destructive test results shall be inclusive of inspection results, electrical test results, test equipment list and calibration information, any conditioning chamber temperature profiles, x-rays, and photographs. Destructive test results shall be inclusive of associated current and pressure time traces, photographs, test equipment list and calibration information, and conditioning chamber temperature profiles. Current and pressure-time data shall also be submitted in digital file format compatible with Microsoft Excel (e.g. .csv or .xls).
CDRL Summary.
Table 2. CDRL SUMMARY
CDRL
NUMBER
| TITLE |
| FIRST SUBMISSION |
| SUBSEQUENT SUBMISSION |
| CDRL A001 |
| TEST PROCEDURE |
(SOW Sections 3 and 4.1)
| Ten (10) days prior to the start of testing |
| Revision |
| CDRL A002 |
| TECHNICAL REPORT - STUDY/SERVICES |
(SOW Sections 3 and 4.3)
| Within thirty (30) days after completion of destructive testing |
| None |
Deliverable Address and Points of Contact
NSWC IHD Technical Representative:
Christine Hughes, Code E24CH Phone: 301-744-2372 Email: Christine.m.hughes28.civ@us.navy.mil
WAWF Acceptor:
Chrissy Fish-DeAtley, Code E24CF Phone: 301-744-2313 WAWF email notifications shall be sent to: christina.m.fishdeatley.civ@us.navy.mil
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