SOW_X-HANGAR_Code_5009 (CUI) DRAFT.pdf
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This is a Statement of Work (SOW) for the third-generation X-Hangar Shelter system, a camouflage netting and expeditionary lifting structure project for the Naval Research Laboratory (NRL). The objective is to develop an improved camouflage vehicle mesh (CVM) cover system with enhanced signature management, durability, and reduced size, weight, and power (SWaP) for both the United States Marine Corps (USMC) and United States Air Force (USAF). The project involves designing, manufacturing, and delivering prototype systems that will undergo testing and evaluation by end-users, with the ultimate goal of creating a product ready for acquisition.
The contract will run for four years (one base year plus three option years), with key deliverables including two prototype X-Hangar systems, multiple interim progress reviews, system demonstrations, and design modifications based on end-user feedback. The CVM covers will be dual-sided with urban and tropical camouflage patterns, designed to obscure aircraft from visual, infrared, and radar detection. Technical requirements are extensive, covering spectral signatures, durability, breathability, and specific performance metrics across various environmental conditions. The project is controlled under Controlled Unclassified Information (CUI) guidelines and subject to export control regulations.
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CUI
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CAMOUFLAGE NETTING AND EXPEDITIONARY LIFTING
STRUCTURES (CNELS), OPERATIONAL TEST SUPPORT,
AND
JOINT TECHNOLOGY TRANSITION
STATEMENT OF WORK
WARNING - This document contains technical data whose export is restricted by the Arms
Export Control Act (Title 22, U.S.C., Sec 2751, et seq.) or the Export Administration Act of
1979 (Title 50, U.S.C., App. 2401 et seq.), as amended. Violations of these export laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DoD
Directive 5230.25.
Controlled by: US Naval Research Laboratory
Controlled by: Signature Technology Office, Code 5708
CUI Category: Defense
Limited Distribution/Dissemination Control C: US Government Employees and
Contractors
POC: scott.ramsey@nrl.navy.mil
Controlled by: US Naval Research Laboratory
Controlled by: Signature Technology Office, Code 5009
CUI Category: Defense
Limited Distribution/Dissemination Control C: US Government Employees and
Contractors POC: scott.a.ramsey30.civ@us.navy.mil mailto:scott.ramsey@nrl.navy.mil
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STATEMENT OF WORK
FOR
CAMOUFLAGE NETTING AND EXPEDITIONARY LIFTING STRUCTURES
(CNELS), OPERATIONAL TEST SUPPORT, AND
JOINT TECHNOLOGY TRANSITION
1.0 BACKGROUND
1.1 FY19-23 Camouflage Vehicle Mesh
This Statement of Work (SOW) sets forth the requirements for the Naval Research Laboratory, Signature Technology Office (NRL STO), to design, develop, and deliver a set of Expeditionary
Inflatable Hangar systems (aka “X-Hangar”) with camouflage covers incorporating passive, multimodal capability for USMC and USAF aircraft. This work builds upon previous NRL efforts for obscuration and concealment of multiple types of vehicle platforms against ground and airborne sensors using camouflage netting. The next-generation camouflage vehicle mesh (CVM) covers require improved breathability and durability for increased wind and snow loads, while maintaining current multispectral obscuration performance. The inflatable lifting structures will support the improved CVM systems covering the aircraft platforms.
Throughout an FY19-23 collaboration with ONR Global TechSolutions, the NRL STO performed field-testing of Contractor-developed first- and second-generation Camouflage Netting Systems
(Gen I in FY19-20, Gen II in FY21-23). The Camouflage Netting Systems (CNS) developed under this effort are coated with specialized materials that match visible shades mimicking grass fields and tropical environments for off-airport locations. Coatings were also developed to match visible shades commonly found in concrete and asphalt for on-airport locations. The coatings exhibit an additional low-contrast capability extending to the NIR (0.7-0.9 micron), SWIR (0.9-1.7 micron), and thermal IR (3.0-12.0 micron) spectral bands by mimicking the spectral reflectance values in these respective background environments. The CVM design also incorporates optimized RF-scattering capability at appropriate levels to obscure aircraft from 360-degree detection by both airborne and unmanned aerial surveillance systems (UAS).
First-generation CVM systems lacked the required durability and contrast (blending into background) in certain spectral bands required improvement. Second generation CVM systems improved the durability and blending aspects missing in the Gen I CVM, but also lowered airflow through the covers, which limited wind flow. The research and development of the third-generation CVM under this Statement of Work will attempt to correct this attribute, along with panel design, mounting, durability, lofting, and curtain functionality to deliver correctly reinforced systems for regular use and recurring deployment for USMC and USAF aircraft
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1.2 FY21-23 Inflatable Lifting Structures
In FY21, NRL STO developed an inflatable lifting structure to be used as an expeditionary shelter for aircraft (aka “X-Hangar”), and provided structural support of the CVM covering the aircraft.
The first generation X-Hangar system (FY21) was a semicircle design with a 2-ply fabric shell.
This system was very heavy to move and to lift during inflation. A second generation X-Hangar
(FY22-23) was designed with a single-ply fabric shell and parabolic shape that reduced overall weight and improved ease of lifting during inflation. The research and development of the third generation X-Hangar under this Statement of Work will attempt to improve size, weight, and power (lower SWaP) as well as improve mobility of the structure during both transport and service.
2.0 OBJECTIVES
The objectives for the third generation X-Hangar Shelter system under this SOW is to make signature and durability improvements upon the camouflage cover system, lower SWaP for the inflatable system and electronics and deliver improved systems to USMC and USAF end-users for testing and evaluation. End users shall then provide feedback in the form of an after-action report
(AAR) to NRL with suggested improvements/changes to a final X-Hangar system that will also be delivered at the end of the contract period of performance. The ultimate objective at the completion of this project is to have a product which meets the USMC and USAF requirements and is ready to transition to acquisition.
A list of project objectives is provided in Table 1.
Table 1. X-hangar Project Objectives
OBJECTIVE RATIONALE
Project Kickoff
USMC 1st MAW and USAF ACC A3/2/6K brief expectations, specifications, deliverables & timeline to Naval Research Lab from
Contractor
1st Production System
Production
Ametrine, Inc. and i2K Defense, Inc. produce initial production version of X-Hangar system based on specifications from USMC 1st
MAW and USAF ACC A3/2/6K
1st Production System
Delivery
Ametrine, Inc. delivers initial production X-Hangar system to USMC
1st MAW and USAF ACC A3/2/6K (unit/location TBD)
System Inspection &
Validation
System inspected & validated by USMC 1st MAW and USAF ACC
A3/2/6K for compliance with specifications, feedback provided to
NRL
Production System Re-
Work
Contractor refines 1st production X-Hangar system based on USMC
1st MAW and USAF ACC A3/2/6K inputs
Re-Worked Production
System Delivery
Contractor delivers re-worked production X-Hangar to USMC 1st
MAW and USAF ACC A3/2/6K (unit/location TBD)
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OBJECTIVE RATIONALE
System Inspection &
Approval
System inspected for compliance with specifications and approved by
USMC 1st MAW and USAF ACC A3/2/6K
System Production
Begins
Contractor begins production of remaining (XX) X-Hangar systems each for USMC 1st MAW and USAF ACC A3/2/6K
Final Production
System Deliveries
Contractor delivers (XX) X-Hangar systems to USMC 1st MAW and
USAF ACC A3/2/6K units
Project Closure USMC 1st MAW and USAF ACC A3/2/6K brief the satisfaction of expectations, specifications, deliverables & timeline to NRL
3.0 SCOPE OF WORK
The technical approach for this contract includes building a set of initial prototype systems meeting physical and signature requirements received from USMC and USAF end-users of the system.
NRL Code 5009 Signature Technology Office will provide contracting oversight, as well as engineering for developing a material solution for improved signature management of the X-
Hangar CVM covers. The Contractor shall design and manufacture the X-Hangar camouflage covers, inflatable structure, and system electronics, respectively. Each part of the X-Hangar system will require modification to bring up to MIL-SPEC standard, as well as reducing size, weight and power (SWaP) to be more conducive to expeditionary (rapid) deployment and setup/teardown. Once the prototype systems have been delivered to the end-users and thoroughly tested, a final set of physical and signature requirements will be drafted and provided to the
Contractor to build a final set of X-Hangar systems based on these requirements. The final set of
X-Hangar systems shall also be delivered to USMC and USAF end-users.
4.0 Requirements
4.1. Task 1: Project Management
The Contractor shall provide project management support as detailed below.
Task 1.1 Project Management Support
The Contractor shall:
4.1.1 Monitor the execution of the contract requirements to ensure timely delivery of contract deliverables.
4.1.2 Coordinate/resolve program issues/requirements when encountered and as necessary with government representatives.
4.1.3 Coordinate personnel in-processing and all associated security requirements.
4.1.4 Monitor contract expenditures to ensure the contract is fully executed as planned and notify the COR/POC of changes and funding issues.
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4.1.5 Purchase approved materials and equipment, as required, to accomplish the
CVM delivery and support.
4.1.6 Manage the deliveries of the 3rd Gen X-Hangar products throughout the contract, in accordance with the deliverable requirements.
4.1.7 Coordinate participation in the government field demonstration of the 3rd Gen
X-Hangar deliverables at the following locations
4.1.7.1 CONUS test – TBD
4.1.7.2 OCONUS test – TBD
4.1.8 Manage project subcontractors’ budget, schedule, delivery, quality, security, etc...
Task 1.2: Project Review Meetings
The Contractor shall host four Interim Progress Review (IPR) Meetings throughout the program.
These meetings shall include:
• IPR 1 – Design Review
• IPR 2 – Spin 1 Testing Review
• IPR 3 – Final Prototype Data Package Review
• IPR 4 – Deliverable Readiness Check
At each meeting the Contractor shall prepare meeting slides, host the meeting (either in-person at the Contractor or Government facility or virtually as a video conference), and send out meeting minutes after the conclusion of the meeting.
Task 1.3: Documentation
The Contractor shall prepare an SOP/User’s Manual for the deliverable system, which will be distributed to end users who take delivery of the system. The Contractor shall also prepare documentation for the project and system including a Final Report summarizing project activities, success and failures, and conclusions.
4.2. Task 2: System Engineering
In Task 2, the Contractor shall perform system engineering functions to include engaging with stakeholders, gathering requirements, and developing and maintaining a System Requirements
Specification (SRS)
Task 2.1 – Stakeholder Engagement
The Contractor shall identify Government stakeholders who will help drive the system requirements. On-going communication with the stakeholders shall continue throughout the duration of the project to keep them updated on project progress, schedule and technical outcomes.
Task 2.2 – Requirements Gathering
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Using the list of stakeholders identified in Task 2.1, the Contractor shall gather requirements for the system. These requirements may be based on end-user needs, concepts of operations
(CONOPs), lifecycle planning or any other relevant information.
Task 2.3 – System Requirements Specification
The Contractor shall refine the requirements gathered during Task 2.2 into a System Requirements
Specification (SRS). The SRS will be the document used to analyze design decisions and trade-space during the development portions of the project and will also be used for test planning to ensure that the system is evaluated properly against the requirements. The SRS will be a living document which shall be maintained by the contractor throughout the program.
4.3. Task 3: Research & Development
Task 3.1: Improved CVM Cover
A portion of the work shall be to improve performance of the camouflage cover.
Camouflage cover improvements, including, but not limited to: design shape based on X-
Hangar dimensions, integrated handles, connectors (Velcro and D-rings), front and rear curtain lifting system, anchoring system.
Task 3.2: Improved Inflatable Hangar Shelter
The X-Hangar inflatable lifting structure requires a number of improvements for the third generation system. X-Hangar inflatable improvements, including, but not limited to: shell material, design shape based on X-Hangar dimensions, integration of handles, access points (zippers, Velcro, etc), integration of heavy-duty materials for arch bases, etc. Replace water bladders (used to secure CVM covers and hangar bases to the ground) to sandbags.
Task 3.3: Improved Electronics/Control System
This task shall improve performance of the X-Hangar electronics system by combining air blowers and pressure monitors for lower weight, weatherproofing and compactness, and replace expensive/heavy/bulky fuel generator power with redundant photovoltaic batteries and solar panels.
4.4. Task 4: Systems Manufacture
This task will take the system improvements in in Tasks 1-3 and apply them to new, 3rd Generation
X-Hangars. Prototype 3rd Gen systems will be manufactured and delivered to both USMC and
USAF customers. These systems shall be tested and recommendations provided by end users for improvements and/or changes to design and functionality for the final X-Hangar system design and manufacture. Subtasks in this effort include:
4.4.1 Camouflage cover manufacture. Manufacture and deliver to end users a total of (2) prototype systems and (4) final X-Hangar systems.
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4.4.2 X-Hangar inflatable shelter manufacture. Manufacture and deliver to end users total of (2) prototype systems and (4) final X-Hangar systems
4.4.3 X-Hangar electronics and power. Manufacture and deliver to end users a total of (2) prototype systems and (4) final X-Hangar systems. .
4.5. Task 5 – Test and Evaluation
Task 5 will involve the Contractor completing multiple test and evaluation periods throughout the program. These evaluations will include both internal and external tests. Each test requires a test plan, which shall be written based on the specifications in the SRS. After each test, the Contractor shall report on the results of the test including a list of improvements needed in the next design iteration.
Task 5.1 – “Spin 1” Testing
Spin 1 testing includes both internal and external (Government) testing on the prototype produced during Task 2.1. The Contractor shall write a test plan for each Government test event and perform testing to determine how the prototype meets system requirements. At the conclusion of testing, the Contractor shall analyze and summarize the results of the tests. The Contractor shall hold an
Interim Progress Review (IPR) meeting with the Sponsor to review the data from testing.
Task 5.2 – “Final Prototype” Testing
Task 5.2 will be the culmination of the design/testing phase of the project, where the Contractor shall test the “Final Prototype” system. A test plan shall be produced before testing and at the conclusion of testing the contractor will review and summarize the test results. At the end of this task, the contractor will hold a “Deliverable Readiness Check” IPR, which shall demonstrate that the “Final Prototype” system meets system requirements and is ready to proceed to deliverable manufacturing.
4.6 3rd Generation X-Hangar System Specifications
Specifications for the 3rd Generation Aircraft Camouflage Vehicle Mesh (CVM):
4.6.1 CVM covers must be sufficiently sized to park aircraft inside the shelter
(approx. 83 cubic feet total volume). X-Hangar Shelter inner dimensions:
Length: 65 feet
Width: 65 feet
Height: 26 feet
4.6.2 Maximum CVM netting weight: 0.4 lbs/yd2 (6.4 oz/yd2)
4.6.3 CVM fabric durability 90-120 lbs tear strength
4.6.4 Breathability in the fabric structure to operate in high wind conditions (50 mph threshold, 75 mph objective)
4.6.5 Dual-sided CVM cover, (side one) urban/on-airport and (side 2) tropical/off-airport
4.6.5.1 Off-airport/Tropical side: Grassy or tropical pattern with green color palette on one side; see Section 4.7
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4.6.5.2 On-airport/Urban side: concrete/urban pattern with gray color palette on the opposite side; see Section 4.7
4.6.6 Portability: Maximum total of seven (7) CMV panels, including Two (2) front curtain panels
4.6.6.2 Two (2) rear curtain panels
4.6.6.3 Three (3) top (rectangular) panels
4.6.7 Dimensions, storage/transport: standard pallet size for netting system of CVM kit; can be multiple pallets if necessary
4.6.8 Unassembled, single nets require maximum 2-person portability (75-lb maximum weight per net)
4.6.9 Packed CVM (all nets) must be air portable via MV-22 and CH-53 (5 CVM systems total per aircraft)
4.6.10 Packed CVM systems (all nets) must be air drop-capable via C-130 variant
Specifications for the 3rd Generation Inflatable Hangar System:
4.6.11 Total of four (4) main arches (3.25’D) with a parabolic shape
4.6.12 Minimum of (21) cross beams (13’L x 3.25’D), with minimum (7) cross beams connecting in between each of the (4) main arches
4.6.13 Physical dimensions (see Figure 1)
4.6.14 Inflatable shell to be composed of minimum 630D strength, silicon rubber-coated nylon airbag fabric
4.6.15 Inflatable air bladders composed of high-elongation/break strength aromatic polyether urethane
4.6.16 Improvements in mobility of the X-Hangar system to roll freely over parked aircraft over all types of terrain by upgrading the base casters and wheels;
4.6.17 2” wide nylon webbing shape reinforcement straps located every 2’ on the exterior of the airbag shell of each arch bladder
4.6.18 Nylon webbing handles stitched into the airbag shell for ease of handling
4.6.19 Labels stitched into the airbag shell indicating which side is up
4.6.20 HDPE material stitched into the base of each arch for reinforced bases to enable ease of movement along all terrains
4.6.21 Appropriate number of 4”W ratchet straps for securing arch bases to tie-downs or stakes
4.6.22 (40) water bladders (80-100 lbs when filled) for securing the CVM cover and arch bases to the ground
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Figure 1. Physical dimensions of X-Hangar inflatable system
Specifications for the 3rd Generation Electronics System:
4.6.21 Portable Battery System:
1. General
○ Dimensions: 33 x 20 x 33 inches, on rolling caster wheels
○ Weight: Reasonable for 2-man carry (< 300 lbs)
○ Protection Rating: IP55, suitable for both indoor and outdoor installations
○ Cooling Method: Fan-cooled system to maintain optimal operating temperatures
○ Operating Temperature Range: 14°F to 122°F (-10°C to 50°C)
○ Operating Relative Humidity Range: 5% to 95%
○ Expansion Capability: Up to 19.2 KWh for extended power requirements
○ Bluetooth Module: Integrated
○ Enclosure Security: Yes
26’
65’
32.5’
65’
29.25’
65’
13’
65’
3.25’
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○ Installation Environment: Suitable for indoor and outdoor installations
2. Battery Specifications
○ Battery Type: Lithium Iron Phosphate (LiFePO4)
○ Nominal Battery Voltage: 48VDC
○ Rated Battery Capacity: 100Ah
○ Rated Battery Energy: 4.8 KWh
○ Cycle Life: Minimum 4500 cycles (80% Depth of Discharge, 80% End of Life, 0.2C, 25°C)
3. Power Output
○ Rated AC Output Voltage: 120VAC
○ Rated AC Output Frequency: 50Hz/60Hz (Adjustable)
○ Rated Output Power: 3500W
○ Peak AC Output Power: 7000W for handling power surges
4. Power Input
○ Rated AC Input Voltage: 110VAC/120VAC
○ Rated AC Input Frequency: 50Hz/60Hz
○ Maximum AC Bypass Current: 20A
○ Maximum Solar Input Power: 4400W
○ Maximum Battery Charge Current (Solar): 80A
○ Maximum Battery Charge Current (Total): 100A
4.6.23 Electric Inflator System
1. Housing and Material
○ Material: High-impact plastic optimized for durability and environmental resistance.
○ Enclosure: IP V6 rated, providing protection against dust and powerful water jets
○ MIL-SPEC Preparation: Enclosure parts designed with DFM principles to prepare for future MIL-STD-810 environmental endurance testing
2. Motor Specifications
○ Type: Two-stage, thru-flow discharge vacuum motor
○ Voltage: 120 volts AC, 60 Hz
○ Power Consumption: Maximum 1350 Watts
○ Airflow Capability: Up to 180 CFM
○ Efficiency: Engineered for maximum airflow with minimal power usage.
3. Pressure Sensors
○ Pressure Ranges: 0.5 to 60 inches of water column (inH2O), equivalent to approximately 0.018 to 2.16 PSI
○ Accuracy: Better than 0.25%
○ Interface: Digital (I2C/SPI), with selectable resolution of 16, 17, or 18 bits
4. Onboard Display and Control
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○ Features an onboard display with local buttons for manual override and direct control of target pressures
○ Allows users to monitor and adjust operational parameters in real-time
5. Communication and Networking
○ Technologies Supported: Wired TCP/IP, Bluetooth Low Energy (BLTE), and
Bluetooth
○ Security Measures:
■ Data Encryption
■ Secure Protocols: TLS 1.2 or higher for TCP/IP and IPsec for end-to-end encryption over networks.
■ Range and Data Rate: Up to 10 meters with a data rate of around 1 Mbps for Bluetooth connection
■ Interference Resistance: Employs frequency-hopping spread spectrum
(FHSS) techniques for enhanced signal security
○ Control System: Waterproof touch panels, power and override switches, and locking hose connections.
○ MIL-SPEC Communication Compliance: Meets MIL-STD-188 for communication interoperability and performance in tactical environments.
6. Safety Features
○ Monitoring: Integrated with real-time monitoring capabilities using advanced sensors.
○ Automatic Shutdown: Equipped with automatic safety protocols to deactivate the inflators if critical pressure thresholds are exceeded.
7. Power and Environmental Compliance
○ Power Requirements: 120V / 10.6A, equating to 1164 Watts, with a 6-foot power cord rated for 120V 15A.
○ Environmental Conditions: Operates effectively in a humidity range of 5%-95% and a temperature range of 14°F to 122°F (-10°C to 50°C).
○ Environmental and EMI Compliance: Designed with DFM considerations for future MIL-STD-810 environmental resilience and MIL-STD-461 EMI compatibility testing.
8. Data Logging and Analysis
○ Data Logging: Logs current status including date timestamp, pressure, and motor state to a local datastore.
○ Data Retrieval: Data can be accessed via a ruggedized tablet or downloaded directly from the inflators.
9. Software/Firmware Specifications
○ Firmware: Custom firmware hardened using PIC32 microcontrollers, utilizing the DSP technology from the existing pressure monitoring system.
○ Updates: Software updates are conducted via USB, ensuring secure and controlled update processes.
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10. Mechanical Specifications
○ Weight: 6 lbs
○ Flow Rate: 180 CFM
○ Max. Back Pressure: 2 PSI
○ Runtime: Up to 500 hours
11. Ruggedized Laptop for Dashboard Monitoring
○ Model: Dell Latitude 7230 Rugged Extreme
○ Processor: 12th Gen Intel® Core™ i5
○ Operating System: Windows 11 Pro
○ Memory: 8GB LPDDR5
○ Storage: 256 GB,
○ Graphics: Integrated Graphics
○ Display: 12" Touchscreen, with outdoor viewability
○ Communication: Wi-Fi 6E AX211, Bluetooth
○ Battery: 2 Cell, 35.6 Wh, ExpressCharge™ Capable
○ Ports: Top expansion port (RJ45), Right-hand side expansion port (USB-A)
○ Additional Features: Includes Intel vPro Technology for advanced management, GPS capabilities, and hazardous location certification
○ Purpose: Used to run the Python code for real-time dashboard monitoring of inflator status and performance metrics.
12. MIL-SPEC Testing and Compliance Preparation
○ Design for MIL-SPEC Testing: The Gen3 X-Hanger Inflator is designed with
DFM principles to facilitate future testing against MIL-STD-810 for environmental endurance and MIL-STD-461 for electromagnetic compatibility.
○ Quality Assurance: The design and manufacturing process aim to meet or exceed MIL-SPEC standards, with comprehensive testing planned in subsequent development phases.
4.7 CVM Cover Spectral Signatures
4.7.1 Visual (0.4-0.7µm)
4.7.1.1 Tropical CVM:
Dual-sided camouflage net; one side with shades and a pattern that mimic grass, an opposite side with shades and a pattern that mimic tropical rain forest. Shade values in Tables 1-2 below are listed in CIELab values and measured in accordance with American Association of Textile Chemist and Colorants
(AATCC) Evaluation Procedure 6, Section 2, utilizing a color spectrophotometer as the measurement instrument. Shades must meet tolerances for each phase listed in Tables 1-2 below. The percentage of each shade in the camouflage pattern is listed with the rendered RGB shades below
13 | 2 5 each table as an example. The percentages are suggested; the camouflage pattern and percentage of each shade in the pattern shall be at the discretion of the Contractor.
Table 2. CIELab Color Requirements for Tropical CVM - Grass side
Shade
CIELab Target Values 1st
Deliverable
Tolerance
Final
Deliverable
Tolerance L* a* b*
Light Green 59.00 -43.00 37.00 dE* = 8.00 dE* = 4.00
Olive 52.00 -18.00 38.00 dE* = 8.00 dE* = 4.00
Dark Green 40.00 -6.00 13.00 dE* = 8.00 dE* = 4.00
Light Green (60%) Olive (25%) Dark Green (15%)
Table 3. CIELab Color Requirements for Tropical CVM - Tropical side
CIELab Target Values 1st
Deliverable
Tolerance
Final
Deliverable
Tolerance L* a* b*
Light Green 59.00 -43.00 37.00 dE* = 8.00 dE* = 4.00
Olive 52.00 -18.00 38.00 dE* = 8.00 dE* = 4.00
Bark Brown 26.00 5.00 3.00 dE* = 8.00 dE* = 4.00
Black 22.00 2.60 2.00 dE* = 8.00 dE* = 4.00
Light Green (44%) Olive (19.5%) Bark Brown (15%) Black (21.5%)
4.7.1.2 Urban CVM:
Dual-sided camouflage net; one side with shades of gray and pattern that mimics concrete; one side with darker gray and black shades that mimics asphalt. Shade values in Tables 3-4 below are listed in CIELab values and measured in accordance with American Association of Textile Chemist and
Colorants (AATCC) Evaluation Procedure 6, Section 2, utilizing a color spectrophotometer as the measurement instrument. Shades must meet
14 | 2 5 tolerances for each phase listed in Tables 3-4 below. The percentage of each shade in the camouflage pattern is listed with the rendered RGB shades below each table as an example. The percentages are suggested; the camouflage pattern and percentage of each shade in the pattern shall be at the discretion of the Contractor.
Table 4. CIELab Color Requirements for Urban CVM - Concrete side
CIELab Target Values 1st
Deliverable
Tolerance
Final
Deliverable
Tolerance L* a* b*
Light Gray 79.00 0.00 1.00 dE* ≤ 8.00 dE* ≤ 4.00
Gray 71.00 1.00 0.00 dE* ≤ 8.00 dE* ≤ 4.00
Dark Gray 61.00 0.00 -2.00 dE* ≤ 8.00 dE* ≤ 4.00
Light Gray (33.3%) Gray (33.3%) Dark Gray (33.3%)
Table 5. CIELab color requirements for Urban CVM – Asphalt side
CIELab Target Values 1st
Deliverable
Tolerance
Final
Deliverable
Tolerance L* a* b*
Dark Gray 61.00 0.00 -2.00 dE* ≤ 8.00 dE* ≤ 4.00
Charcoal 37.00 0.00 0.00 dE* ≤ 8.00 dE* ≤ 4.00
Black 26.00 1.00 1.00 dE* ≤ 8.00 dE* ≤ 4.00
Dark Gray (33.3%) Charcoal (33.3%) Black (33.3%)
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4.7.2 Near-infrared (NIR, 0.7-0.9µm) and Shortwave Infrared (SWIR, 0.9-1.7µm)
Each shade listed in Tables 1-4 shall have an average apparent reflectance (%) over the specified near-infrared band (NIR 0.7-0.9µm) and shortwave infrared band (SWIR, 0.9-
1.7µm) that match target reflectance values provided in the tables below.
NIR and SWIR reflectivity measurements of the Contractor nets can be performed following AATCC Evaluation Procedure 6, Section 2, using a UV/Vis/NIR/SWIR spectrophotometer as the measurement instrument. The spectrophotometer should be calibrated annually to NIST standards, and every eight hours to a calibrated 99% reflectance standard. Measurements shall be in 1-nm increments from 700-900nm (NIR) and 900-1700nm (SWIR).
For each set of netting fabric samples, the NIR and SWIR % reflectance of a single color is to be measured on five random specimens, each rotated and measured at 0° and 90° azimuth angles, for a total of ten measurements per color, per fabric sample). Obtain a single average reflectance for each wavelength, then average apparent reflectance of each band by taking the average over 700-900nm for the NIR band and again over 900-1700nm for SWIR band.
4.7.2.1 Tropical CVM: Dual-sided camouflage net; average apparent NIR and SWIR target reflectance values for each shade for the grass side of the net listed in Table
6; average apparent NIR and SWIR target reflectance values for each shade for the tropical side of the net listed in Table 6:
Table 6. NIR & SWIR % Reflectance Requirements for Tropical CVM -
Grass side
Apparent Reflectivity
Target Values (%) Phase I
Tolerance
Phase II & III
Tolerance
NIR SWIR
Light Green 40.0 58.0 ±10.0 ±5.0
Olive 36.9 46.0 ±10.0 ±5.0
Dark Green 20.8 26.0 ±10.0 ±5.0
Table 7. NIR & SWIR % Reflectance Requirements for Tropical CVM -
Tropical side
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Shade
Apparent Reflectivity
Target Values (%) Phase I
Tolerance
Phase II & III
Tolerance
NIR SWIR
Light Green 40.0 58.0 ±10.0 ±5.0
Olive 36.9 46.0 ±10.0 ±5.0
Bark Brown 25.0 35.0 ±10.0 ±5.0
Black 20.8 26.0 ±10.0 ±5.0
4.7.2.2 Urban CVM: Dual-sided camouflage net; average apparent NIR and
SWIR target reflectance values for each shade for the concrete side of the net listed in Table 7; average apparent NIR and SWIR target reflectance values for each shade for the asphalt side of the net listed in Table 8:
Table 8. NIR & SWIR % Reflectance Requirements for Urban CVM - Concrete side
Apparent Reflectivity
Target Values (%) Phase I
Tolerance
Phase II & III
Tolerance
NIR SWIR
Light Gray 46.6 50.0 ±10.0 ±5.0
Gray 34.3 40.0 ±10.0 ±5.0
Dark Gray 20.9 30.0 ±10.0 ±5.0
Table 9. NIR & SWIR % Reflectance Requirements for Urban CVM - Asphalt side
Apparent Reflectivity
Target Values (%) Phase I
Tolerance
Phase II & III
Tolerance
NIR SWIR
Dark Gray 20.9 30.0 ±10.0 ±5.0
Charcoal 20.9 30.0 ±10.0 ±5.0
Black 20.8 26.0 ±10.0 ±5.0
4.7.3 Mid-wave Infrared (MWIR, 3-5µm) and Long-wave Infrared (LWIR, 8-12µm)
4.7.3.1 The aircraft cover must exhibit a thermal IR (MWIR and LWIR) signature that conceals/blends the covered aircraft with both grassy and tropical environments, providing concealment at 350m (T) and 1000m (O) from tactical ground sensors; 500 ft (T) and 1000ft (O) from aerial (UAS) sensors.
4.7.3.2 The aircraft cover must exhibit a thermal IR (MWIR and LWIR) signature
17 | 2 5 such that it obscures the aircraft IR signatures at 350m (T) and 1000m (O) from tactical ground sensors; 500 ft (T) and 1000ft (O) from aerial (UAS) sensors.
Synthetic Aperture Radar (SAR, X, Ku, and KA bands)
4.7.3.2 Capable of obscuring the aircraft from airborne synthetic aperture radar
(SAR), meaning SAR must be unable to discern/discriminate the object due to RF-scattering effects of the cover over the aircraft.
4.7.3.3 The radar Cross Section (RCS) of the CVM must have an attenuation based on the following parameters:
Table 10. Radar Cross Section (RCS) Thresholds and Objective Values for CVM
RCS Objective Minimum Average Apparent Attenuation
(RCS - dB)
O/T Threshold Objective
Radar Band Co-Channel Co-Channel C ≥ 8 ≥ 10 X ≥ 9 ≥ 10
Ku ≥ 11 ≥ 15 Ka ≥ 13 ≥ 18 W ≥ 16 ≥ 20
Durability
The CVM fabric must have a minimum tearing strength of 70 force-lbs (lbf) in both warp and fill directions, based on the test method prescribed in
ASTM D 2261-13, “Standard Test Method for Tearing Strength of
Fabrics by the Tongue (Single Rip) Procedure (Constant-Rate-of-
Extension Tensile Testing Machine).”
The CVM fabric must have a minimum breaking strength of 120 force-lbs (lbf) in both warp and fill directions, based on the test method prescribed in
ASTM D 5034-09, “Standard Test Method for Breaking Strength and
Elongation of Textile Fabrics (Grab Test).”
Breathability
The CVM fabric must have a minimum air permeability rating of 350 ft3/min per m2 based on the test method prescribed in ASTM D737-04, “Test
Method for Air Permeability of Textile Fabrics.”
Enable sufficient airflow through the concealment cover to reduce and minimize sheer stress due to high winds; >25 mph (T), >40 mph (O)
18 | 2 5
Allow harmful vapors such as JP5 jet fuel, petrol, and other noxious fumes to escape easily and not be contained under the cover, eliminating breathing and respiratory hazards.
Life Cycle
The CVM fabric must have a robustness and ruggedness capable of twenty don and doff cycles prior to major repair or replacement.
Patch Kit
Each CVM shall include a patch kit for on-the-fly repair to include:
Sufficient fabric to patch and repair up to three (3) square meters
Sew kit, including correct gauge thread and needles
Patching instructions
5.0 OTHER UNIQUE REQUIREMENTS
No unique requirements are anticipated to be encountered in the performance of this contract.
6.0 SPECIAL MATERIAL REQUIREMENTS
No special materials are anticipated to be encountered in the performance of this contract.
7.0 GOVERNMENT-FURNISHED PROPERTY, MATERIAL, EQUIPMENT, OR
INFORMATION (GFP, GFM, GFE, OR GFI)
7.1 Government Furnished Property, Material, and Equipment (GFP/GFM/GFE)
The Government will furnish copies of all applicable and required test planning, execution, security and safety control documents, or operational documents during contingencies, in a timely manner in order for the contractor to complete the assigned tasks. GFM may be requested to be returned upon completion of the task or at the end of the period of performance for this contract.
The Government does not anticipate onsite support for this requirement for actions, therefore the Government will not need to provide equipment, materials, or access to networks and systems under this contract.
7.2 Government Furnished Information (GFI)
Intellectual Property. The United States Marine Corps owns the patent rights in and to the design (Ornamental) and the functional features of the MARPAT™. Furthermore, the
United States Marine Corps owns trademark rights in the MARPAT™. Still further, the
19 | 2 5 patterns including, but not limited to, the MARPAT™, and each item including, but not limited to, the documents, materials and information, and all associated intellectual property, created, generated or produced in association with this effort are the sole property of the U.S. Government and not the Contractor. Therefore, without the prior written permission of the contracting officer neither the MARPAT™ nor any other data, documents, materials and/or information created or provided expressly for the contract shall be used by the Contractor for any purpose other than those purposes that are in support of, or for its performance under, the contract.
Other uses of the USMC Trademarks. In the event that an offeror is interested in seeking permission to use the MARPAT™ for other purposes, or is seeking to use other Marine
Corps trademarks/service marks not described herein, please contact the Marine Corps
Trademark Licensing Office through its website at: https://www.trademark.marines.mil/
MARPAT™ Fabric Patterns. MARPAT™ designs are patented and may not be reproduced for commercial purposes without the permission of the USMC.
8.0 EXPORT CONTROL CONSIDERATIONS
Any military information, technology, or subject matter listed within the International Traffic in
Arms Regulations (ITAR), U.S. Munitions List (USML), the Export Administration Regulations
(EAR), and Commerce Control List (CCL) are not releasable under EAR regulations 15 CFR Part
734.8.
The Camouflage Netting and Expeditionary Lifting Structure (CNELS) X-Hangar system under this contract is a technology that falls under Category XIII of the USML. The technology establishes methods to reduce camouflage signature (Category XIII.j(2)), which states, “Equipment, materials, coatings, and treatments that are specially designed to modify the electro-optical, radiofrequency, infrared, electric, laser, magnetic, electromagnetic, acoustic, electro-static, or wake signatures of defense articles or 600 series items subject to the EAR through control of absorption, reflection, or emission to reduce detectability or observability.”
As the technology under this contract is listed within the enumerated control lists of the USML, public release or export will only be authorized through the NRL Release Request Process as
Distribution Statement D, for U.S. Department of Defense (DoD) and U.S. DoD contractors only and not releasable into the public domain.
An export license for this project is required and the Contractor shall comply with export control regulations. Appropriate guidance documents are located at https://flankspeed.sharepoint-mil.us/sites/NRL_Export_Control. For more information and/or guidance, please contact the NRL
General Law Export Control staff at NRL_ECA@nrl.navy.mil or (202) 767-2244.
https://www.trademark.marines.mil/ https://flankspeed.sharepoint-mil.us/sites/NRL_Export_Control https://flankspeed.sharepoint-mil.us/sites/NRL_Export_Control mailto:NRL_ECA@nrl.navy.mil
20 | 2 5
9.0 PLACE OF PERFORMANCE:
All research, development, design, construction, and manufacturing shall be performed at the
Contractor facility. Field demonstrations and testing of the X-Hangar systems developed and delivered under this contract shall be performed at Military installations (locations TBD).
10. PERIOD OF PERFORMANCE:
The contract shall be from date of award through one year (12 months), with three (3) option years for a total of 48 months:
A. BASE YEAR - Date of award to twelve (12) months
B. OPTION YEAR 1 – 12 months
C. OPTION YEAR 2 – 12 months
D. OPTION YEAR 3 – 12 months
11.0 CONTRACT DATA REQUIREMENTS
The Contractor shall deliver the following as specified in this SOW. Table 11 is a compilation of contractual deliverables and corresponding with anticipated delivery dates.
11.1 Kickoff Meeting
The Contractor shall participate in a Kickoff Meeting with the end-users and NRL to discuss contract deliverables, test events, and any future system modifications.
11.2 1st Production System Delivery
11.2.1 Two (2) 3rd Gen Expeditionary Hangar (X-Hangar) Systems
11.2.1.1 One (1) CVM for USAF fixed wing or rotary wing aircraft with open-wing configuration with dual-sided urban/tropical camouflage color palette and pattern; repair kit; transport case(s).
11.2.1.2 One (1) CVM for USMC fixed wing or rotary wing aircraft with open-wing configuration with dual-sided urban/tropical camouflage color palette and pattern; repair kit; transport case(s).
11.3 IPR 1 – Design Review
11.4 IPR 2 – Spin 1 Testing Review
11.5 IPR 3 – Final Prototype Data Package Review
11.6 IPR 4 – Deliverable Readiness Check
11.7 Initial X-Hangar System Demonstration
The Contractor shall participate in a 3rd Gen X-Hangar demonstration performed by the government at a Military installation location TBD (CONUS & OCONUS locations). The demonstration will be a series of field tests of the Contractor’s X-Hangar for fixed wing and rotary
21 | 2 5 wing platforms. The X-Hangar system will be deployed and erected over aircraft specific for the
Hangar dimensions.
11.7.1 Any damage to the 3rd Gen Camouflage Vehicle Mesh during the demonstration due to design or manufacturing error will be borne by the Contractor, and damaged components replaced prior to 3rd Gen delivery of CVM to the offerer.
11.8 Design Modifications of System
The Contractor shall redesign and/or modify the X-Hangar system based on the recommended changes from the USAF and USMC end users from the initial X-Hangar System Demonstration.
11.9 2nd Production System Delivery
The Contractor shall deliver an initial X-Hangar system with redesign elements included in the delivery.
11.10 Final Production System Deliveries
The Contractor shall produce and deliver the final set of re-designed X-hangar systems to both
USAF and USMC end users.
11.11 Closeout Meeting
The Contractor shall participate in a Final Closeout meeting with the end-users and NRL to discuss contract deliverables and way forward.
Table 11. Contractor deliverables with corresponding anticipated delivery dates
DELIVERABLE TECHNICAL ISSUE ADDRESSED
QUANTITY DATE
COMPLETED
Kickoff meeting
Government expectations, specifications, deliverables & timeline delivered to Contractors
1 30 DAC
1st Production System
Delivery
Government receives product at
USMC/USAF (locations TBD) from
Contractor
2 90 DAC
3rd Gen X-Hangar
Demonstrations
Demonstrations performed by the government at a location TBD
(CONUS & OCONUS locations).
2 120 DAC
Design Modifications of
System
Address and incorporate end-user requested changes to system based on
T&E of 1st Production System
As applicable 210 DAC
2nd Production System
Delivery
Government receives re-worked product at USMC/USAF (locations
TBD) from Contractor, modified in
2 270 DAC
22 | 2 5
DELIVERABLE TECHNICAL ISSUE ADDRESSED
QUANTITY DATE
COMPLETED
accordance with feedback given to
Contractor
Final Production System
Deliveries
Government receives balance of product from Contractor at
USMC/USAF (locations TBD)
As applicable 330 DAC
Closeout Meeting
Government briefs satisfaction of expectations, specifications, deliverables and timeline to
Contractors
1 360 DAC
11.12 Documentation
11.12.1 Monthly Status Reports and Teleconferences
The contractor shall prepare a submit reports which include a summary of all technical progress on the project and all weekly verbal reports to the COR. A Milestone Chart and Planned Cost
Curve shall be provided. Subsequent reports shall depict cumulative costs expended by task and personnel as detailed in vouchers. The report shall also contain planned and actual cost curves including updated milestone charts. Contractor format for Monthly Progress Reports is authorized.
The contractor will hold monthly status teleconferences with the COR (and stakeholders when appropriate) on an as needed basis.
11.12.2 Technical Reviews
The contractor shall attend and participate in Integrated Product Team (IPT) meetings, requirements reviews, design reviews, system working group meetings, technical interchange meetings, test planning meetings, and other engineering meetings as required.
11.12.3 Technical Reports
The Contractor shall include preparation of technical reports, engineering drawings, program planning documents, periodic progress reports, and others as needed. The contractor shall prepare detailed test reports documenting all results from predicted analysis and test data identified in test plans.
11.12.4 Summary Final Report
The Contractor shall submit a comprehensive report all activities of a given task order deliverable.
Contractor shall submit test reports on all major testing performed on the contract. Contractor shall submit reports on all major analytic studies and surveys performed on the contract.
23 | 2 5
11.12.5 X-Hangar User’s Manual
The Contractor shall provide a user’s manual will be provided with each 3rd Gen camouflage netting system delivered. The manual will provide information on CVM deployment, retrieval
(including packing and storage), product care, and lofting mechanism.
12.0 SECURITY CONSIDERATIONS
The following are required at the time of proposal submission:
• Contractor personnel who require NRL base access or access to NRL unclassified material and/or unclassified systems shall possess a favorably completed DoD National Agency
Check with Law and Credit (NACLC);
• Contractor personnel who require access to Secret material must have, at a minimum, a favorably completed DoD National Agency Check with Law and Credit (NACLC) and final DoD granted Secret security clearance; and
• Contractor personnel who require access to Top Secret/SCI material must have, at a minimum, a favorably completed DoD National Agency Check with Law and Credit
(NACLC) and final DoD granted Top Secret security clearance with the eligibility of SCI.
The Contractor shall ensure that all classified material is handled in accordance with the issued
DD 254, the National Security Program Operating Manual (NISPOM) (DoD 5220.22M) and all
NRL and applicable Security Program Guides/Directives.
Contractor personnel having privileged user access to NRL information systems will require background investigations and security clearances commensurate with the access level and security classification of the system being accessed as specified in DON 5239.2M
(2009). System Administrators with privileged access may work in the computing, network and/or enclave environments. System Administrators with privileged access shall meet the training and certification requirements for IAT level I at the computing environment (CE), IAT level II at the network environment (NE), and IAT level III for the enclave environment as specified in DON 5239.2M (2009). The initiation of an SSBI is required for all System
Administrators with privileged access serving in these positions.
All contractors (including subcontractors) identified in the Statement of Work shall supplement their current security practices by requiring any personnel involved in executing the contract to complete Government-sponsored and administered Operations Security (OPSEC) training, OPSE-
1301.
12.1 DD Form 254
The Contractor shall be granted access to classified information necessary for performance of this contract upon contract award as specified in the basic DD Form 254. All contractor personnel
24 | 2 5 with access to unclassified information systems, including e-mail, require at a minimum, a favorably completed DoD National Agency Check with Law and Credit (NACLC).
12.2 Visitor Group Security Agreement (VGSA)
The Visitor Group Security Agreement (VGSA) outlines responsibilities in the following areas:
Contractor security supervision; Standard Practice Procedures; access, accountability, storage and transmission of classified material; marking requirements; security education; personnel security clearances; reports; security checks; security guidance; emergency protection; protection of government resources; DD Forms 254; periodic security reviews; and other responsibilities, as required.
The Contractor shall sign a Contractor Visitor Group Security Agreement to protect classified information involved in performance under this contract.
12.3 Identification (ID) Badges and Vehicle Passes
The Government will issue ID badges to Contractor personnel working at NRL in accordance with the requirements of Paragraph 1(b) BADGES of the NRL ROSC. A favorable trustworthiness determination is required in order for nominated contractor personnel to be granted access to NRL facilities and issued an NRL badge. NRL issued Contractor badges will be worn and readily visible at all times while contractor personnel are on NRL facilities.
The Contractor shall provide all requested information required for facilitating the use and possession of badges.
The Contractor shall ensure the immediately return all ID badges issued to Contractor employees under any of the following conditions completion of contract, relocation or termination of an employee, or upon request of the Contracting Officer or Contracting Officer's Representative.
13.0 SAFETY
The Contractor shall comply with safety requirements of NRL Requirements for On-Site
Contractors document, dated 8 December 2008.
14.0 DATA RIGHTS, DISTRIBUTION LIMITATIONS AND MARKINGS
The Contractor shall deliver all products and documents from this effort with unlimited rights to the Government unless specifically identified and asserted otherwise (Refer to DFARS 252.227-
7013 and 252.227-7014 for details). All data and reports shall contain the following:
CONTROLLED UNCLASSIFIED INFORMATION (CUI)
Refer to DoD 5200.48, “Controlled Unclassified Information (CUI), Effective 06 MAR 2020.
25 | 2 5
This material may be reproduced by or for the U.S. Government pursuant to the copyright license under clause at DFARS 252.227-7013 (February 2014).
The Contractor shall deliver Unlimited Rights to all technical data. Unlimited rights means right to use, modify, perform, display, release, or disclose technical data in whole or in part, in any manner and for any purpose whatsoever, and to have or authorize others to do so.
14.1 Identification and Assertion of Restrictions on the Government’s Use, Release, or
Disclosure of Technical Data
The Contractor asserts itself, or the persons identified below, that the Government’s rights to use, release, or disclose the following technical data should be restricted –
Technical Data to be
Furnished With
Restrictions*
Basis for
Assertion**
Asserted Rights
Category***
Name of Person
Asserting
Restrictions****
All drawings and documentation
Developed with
Government
Funding
Government
Purpose Rights
CONTRACTOR
NAME
All manuals
Developed with
Government
Funding
Government
Purpose Rights
CONTRACTOR
NAME
Any information on the manufacturing processes
Developed 100% at private expense Limited Rights
CONTRACTOR
NAME
Any information on the materials utilized
Developed with
Government
Funding
Government
Purpose Rights
CONTRACTOR
NAME
* If the assertion is applicable to items, components, or processes developed at private expense, identify both the data and each such item, component or process.
** Generally, the development of an item, component, or process at private expense, either exclusively or partially, is the only basis for asserting restrictions on the Government’s rights to use, release, or disclose technical data pertaining to such items, components, or processes.
*** Enter asserted rights category (e.g. government purpose license rights from a prior contract, rights in a SBIR data generated under another contract, limited or government purpose rights under this or a prior contract, or specifically negotiated licenses).
**** Corporation, individual, or other person, as appropriate.
File details come from the government source that posted it. Updated .