NAVAIR Points RFI for Marine Corps Medium Vary Tactical UAS – sUAS Information

The Naval Air Programs Command (NAVAIR), Program Govt Workplace for Unmanned Aviation and Strike Weapons (PEO U&W), Navy and Marine Corps Small Tactical Unmanned Plane Programs Program Workplace (PMA-263) at Patuxent River, MD is looking for business enter to determine potential options for a Medium Vary Tactical (MRT) UAS to be used by the US Marine Corps Expeditionary Forces.

The specified Medium Vary Tactical (MRT) Unmanned Plane System (UAS) needs to be able to offering Reconnaissance, Surveillance, and Goal Acquisition (RSTA) throughout day and evening operations throughout quite a lot of operational environments. The system needs to be ruggedized, sturdy, and quickly deployable, delivered prepared for operational use with minimal logistics, coaching, and sustainment burden. It ought to assist mission planning, real-time intelligence assortment, and enhanced situational consciousness for tactical models, and function independently or as a part of a safe, collaborative community. The system ought to assist operations together with, however not restricted to, RSTA, patrolling, safety and drive safety, convoy operations, and navy operations in city terrain (MOUT), and be able to working in austere places, throughout numerous international climates and climate situations, throughout day and evening operations, and inside degraded, denied, intermittent, and restricted (DDIL) radio-frequency environments.

Options able to carrying modular payloads and quite a lot of sensors, together with the availability of real-time Full Movement Video (FMV) by way of high-resolution electro-optical (EO) and/or infrared (IR) sensors, are of explicit curiosity. The Air Car (AV) needs to be able to working from stationary and cell platforms, together with amphibious ships and expeditionary superior bases. Vertical Takeoff and Touchdown (VTOL) options, together with fixed-wing VTOL (FW-VTOL) and multirotor VTOL configurations, are of curiosity.

The AV ought to assist autonomous or handbook launch and restoration inside designated or confined areas, with restoration strategies that decrease system harm and allow fast mission turnaround.

The Floor Management Station (GCS) needs to be man-portable and both present the required tools to observe sensor place and standing, management AV motion, and show video, or be interoperable with current widespread management techniques obtainable for U.S. Authorities procurement. The system needs to be designed for integration into tactical networks and assist safe knowledge sharing with different platforms and command components. All mission knowledge, together with video and mission merchandise, needs to be securely saved on the GCS and/or the AV utilizing detachable storage media.

Responses to this Sources Sought Discover could also be used to tell future acquisition planning and procurement choices. Subsequently, proposed UAS options have to be compliant with relevant Nationwide Protection Authorization Act (NDAA) necessities, together with however not restricted to NDAA FY2020 Part 848, NDAA FY2023 Part 817, NDAA FY2019 Part 889, and the American Safety Drone Act of 2023 (FY2024 NDAA, Public Legislation 118-31, Division A, Title XVIII, Subtitle B, Part 1821), or should clearly describe a reputable, time-bound path to compliance, together with identification of key dependencies, underlying assumptions, and anticipated timelines for attaining compliance.

To assist transparency and traceability of NDAA compliance, respondents might, at their discretion, leverage the Navy’s Small UAS Reusable Structure (SRA) framework to doc system parts, provide chain attributes, and relevant safety controls. The SRA offers government-backed instruments and self-assessment mechanisms that allow distributors to independently consider alignment with DoD-approved benchmarks and facilitate evaluation of compliance artifacts throughout market analysis actions.

Further info is accessible from the SRA Portal at: https://sra.navair.navy.mil

The SRA web site is Public Key Infrastructure (PKI) enabled, limiting entry to these customers who possess both a Division of Protection (DoD) Frequent Entry Card (CAC) or DoD Exterior Certificates Authority (ECA) certificates. Further info – together with directions for acquiring an ECA certificates – is accessible at https://www.cyber.mil/eca.  Accordingly, entry to the SRA web site could also be restricted for some respondents. Use of the SRA framework and related instruments will not be required for response to this RFI and is supplied for common consciousness and informational functions solely.

2. Goal
Any efficiency parameters referenced herein are supplied solely for market analysis functions and don’t represent finalized necessities or acquisition commitments.

PEO (U&W), PMA-263 is particularly taken with techniques with the next traits, in no explicit order:

• Air Car (AV) Most Gross Takeoff Weight (MGTOW) (with payload): < 20 lbs.
• Complete System Weight (together with launch/restoration tools and all peripheral gear):

 < 75 lbs.

• Complete Payload Capability: > 3.75 lbs.
• Baseline Payload: Twin-mode gimbaled EO/IR payload (EO [Ultra-High Definition – UHD], IR [High Definition – HD], laser rangefinder, laser designator).
• Datalink / Bandwidth: Safe video and knowledge hyperlinks using Superior Encryption Commonplace (AES) 256-bit encryption utilizing Federal Data Processing Commonplace (FIPS) 140-3 validated cryptographic modules; mounted energy output; bandwidth optimization throughout multiple frequency band.
• Payload Operation: Capability to assist simultaneous operation of a number of intelligence (multi-INT) payloads.
• Airspeed: > 25 knots indicated airspeed (KIAS).
• Endurance (takeoff to touchdown): ≥ 2.5 hours.
• Line-of-Sight (LOS) Vary: ≥ 40 kilometers.
• Propulsion: Electrical or hybrid-electric propulsion; non-petroleum-based (e.g. gasoline cell, renewable).
• Air Car Management: Operator-in-the-loop (OITL) with semi-autonomous operation.
• Air Car Steerage: Able to operation inside International Navigation Satellite tv for pc System (GNSS) denied environments, using M-Code GPS, inertial navigation models (INU), pc imaginative and prescient, and/or visual-inertial odometry (VIO).
• Multi-AV Management: Capability for a single GCS/operator to manage two or extra air autos.
• Personnel: Most of two (2) operator/maintainer wanted for deployment.
• Wind Limits: Operation in winds as much as 25 knots indicated airspeed (KIAS).
• Rain Limits: Operation in rainfall as much as 0.75 inches per hour.
• Payload Integration: Open, modular structure able to supporting integration of weapon payloads.
• Floor Management Station (GCS): Man-portable, cell, and network-enabled.
• Interoperability: Tactical Assault Package (TAK) suitable, supporting real-time dissemination of intelligence, surveillance, and reconnaissance (ISR) knowledge to U.S. Authorities Furnished Gear (GFE) info techniques.
• Launch and Restoration: Vertical Takeoff and Touchdown (VTOL).
• Expertise Readiness Degree: TRL 8 or larger – Ample maturity for speedy manufacturing, supply, fielding and deployment.

3. Requested Data

Respondents are invited to submit a technical white paper addressing the knowledge described under for his or her proposed resolution.  If any attribute is estimated, underneath improvement, or unknown on the time of submission, it needs to be clearly recognized as such.

Part 3A is meant to seize structured, quantitative system traits and efficiency attributes. Part 3B is meant to seize narrative descriptions of system structure, implementation method, operational concerns, limitations, and tradeoffs.  Respondents ought to keep away from duplicating knowledge supplied in Part 3A inside Part 3B until needed to elucidate implementation particulars.

3A. System Traits & Efficiency Attributes

Respondents are requested to handle the next system traits and efficiency attributes. The place relevant, determine demonstrated, estimated, or deliberate efficiency.

3A.1  System Dimension, Weight, and Transportability

• Air Car (AV) Most Gross Takeoff Weight (MGTOW), inclusive of payload
• AV weight with out payload
• Complete system weight, together with AV(s), Floor Management Station (GCS), launch/restoration tools, batteries, and peripheral gear
• Dimension and weight of the entire system packed for transport (per case)

    –     AV dimensions (assembled)

• GCS dimensions and weight (assembled)
• Transportability (e.g., man-portable, automobile transport, 2-person raise concerns)

3A.2  Launch, Restoration, and Basing

• Launch strategies supported (handbook, autonomous, VTOL, assisted)
• Restoration strategies supported (handbook, autonomous, VTOL, glide/stall, different)
• Touchdown zone necessities and restoration footprint
• Capability to launch and get better from confined areas
• Capability to function from stationary and cell platforms, together with maritime and amphibious environments
• Compatibility with shipboard operations and expeditionary superior bases
• Restoration concerns associated to system survivability and fast mission turnaround

3A.3  Propulsion and Energy

• Propulsion sort(s) (electrical, hybrid, fuel-based, renewable, and so forth.)
• Energy supply(s) for AV and GCS
• Energy administration method (mounted vs adaptive, endurance tradeoffs)

3A.4  Payload Capability and Modularity

• Complete obtainable payload capability
• Baseline payload configuration(s)
• Modular payload functionality and method
• Compatibility with a number of payloads and mission reconfiguration
• Capability to assist simultaneous or sequential multi-sensor / multi-INT operations

3A.5  Sensor Capabilities

• Sensor varieties supported (EO, IR, LRF, LD, different)
• Sensor decision and efficiency traits
• Sensor detection, recognition, and identification efficiency (e.g., NIIRS or equal)
• Gimbal sort and stabilization traits
• Excessive-resolution day/evening imagery functionality

3A.6  Command, Management, and Autonomy

• What autonomy modes exist (handbook, semi-autonomous, autonomous)
• Operator-in-the-loop (OITL) and/or man-in-the-loop (MITL) management ideas
• Mission planning and autonomous mission execution capabilities
• Multi-air automobile management from a single GCS/operator (same-vendor and cross-vendor concerns)

3A.7  Navigation and Steerage

• Navigation strategies employed (GNSS, M-Code GPS, inertial navigation, vision-based navigation, and so forth.)
• Functionality to function in GNSS-degraded or GNSS-denied environments
• Steerage and positioning redundancy approaches

3A.8  Communications, Datalinks, and Networking

• Datalink varieties and architectures
• Encryption strategies and safety approaches
• Spectrum agility and frequency administration
• Bandwidth administration and optimization
• Capability to function in degraded, denied, intermittent, and restricted (DDIL) RF environments
• Capability to function independently or as a part of a safe, collaborative community
• Integration with tactical networks and knowledge sharing with different platforms and command components
• Onboard compute capabilities to assist third celebration payload integration and/or edge processing

3A.9  Floor Management Station (GCS)

• GCS type issue and portability
• GCS working system(s) and software program structure
• Interoperability with current U.S. Authorities widespread management techniques
• Capability to observe sensor place and standing, management AV motion, and show video
• Networked vs standalone GCS operation

3A.10  Mission Information Dealing with

• Mission knowledge varieties generated (video, imagery, metadata, logs)
• Information storage places (AV, GCS, each)
• Use of detachable storage media
• Information safety and integrity measures

3A.11  Efficiency Envelope

• Most and optimum cruise pace
• Sprint pace
• Most endurance (takeoff to touchdown)
• Most endurance (most time the AV can stay airborne underneath normal day at sea stage situations, with a consultant or threshold payload weight).
• Most operational vary (LOS and different related modes)
• Working altitude limits (AGL and strain altitude / density altitude)

3A.12  Environmental Working Limits

• Temperature working limits
• Wind working limits
• Precipitation working limits
• Freshwater and saltwater publicity tolerance
• Water immersion limits
• Environmental storage situations

3A.13  Acoustic and Signature Traits

• Acoustic signature and noise traits
• Detectability concerns (if obtainable)

3A.14  Upkeep, Sustainment, and Logistics

• Operator-level upkeep actions supported
• Modular element substitute method
• Tooling necessities (specialised vs non-specialized)
• Larger-echelon upkeep ideas
• Spare elements and restore philosophy

3A.15  Manpower and Coaching

• Variety of personnel required to deploy and function the system
• Operator and maintainer roles
• Coaching burden and method

3A.16  Software program Assurance and Maturity

• Software program and firmware traceability and replace method
• Explainability and interpretability of autonomy-enabled features
• Expertise readiness stage (TRL)

3A.17  Development and Future Functionality

• Open structure concerns
• Payload and mission development paths
• Integration of extra capabilities over time

3B. Technical Method, Implementation, and Operational Issues

Present detailed narrative info in response to the questions listed under describing the system’s technical method, implementation, and operational concerns. Please reply the questions within the order during which they’re requested.

System Software program and Navigation

3B.1  What working system(s) are used on the air automobile (AV), companion pc, and floor management station (GCS)? Please specify variations, real-time working techniques, hypervisors, and whether or not a Software program Invoice of Supplies (SBOM) is accessible.

3B.2  How does your system navigate? Please describe the first place, navigation, and timing (PNT) strategies, together with GNSS constellations, inertial navigation, and sensor fusion methods.
3B.3  Is your system able to navigation with out GPS? If sure, describe the tactic (e.g., visual-inertial odometry, SLAM) and its efficiency limits, together with drift charges and re-localization functionality.
3B.4  Does your system use Selective Availability Anti-Spoofing Module (SAASM) or M-Code GPS? If that’s the case, please present particulars on receiver mannequin, keying/fill system compatibility, and timing holdover.
3B.5  What flight modes and mission management choices does your system assist (handbook, assisted, waypoint, geofence, terrain-following, loiter, hover-and-stare, autonomous mission execution, and so forth.)?

3B.6  Does your system make use of autonomy or synthetic intelligence (AI) for management, operation, decision-making, or machine studying? If sure, describe its features, compute {hardware}, and safeguards for human-on-the-loop or human-in-the-loop management.

Launch, Restoration, and Security

3B.7  Does your system have precision restoration functionality? If sure, please present touchdown accuracy knowledge (CEP), together with moving-platform restoration if relevant.
3B.8  Can the air automobile safely land in water? If sure, describe buoyancy, flotation time, corrosion safety, and whether or not re-launch from water is feasible.
3B.9  Is any launch or restoration tools required? If sure, describe the kind, measurement, weight, energy necessities, and setup/teardown time.
3B.10  What security options are built-in into the system (misplaced hyperlink procedures, misplaced GPS behaviors, return-to-home logic, auto-land, geofencing, flight termination, detect-and-avoid)?

3B.11  Establish the variety of personnel required to securely conduct launch, restoration, routine area operations, and upkeep for the proposed system.

Describe any assumptions, enabling automation, security concerns, environmental constraints, or operational limitations related to these personnel necessities.

Mapping and Mission Planning

3B.12  What mapping software program does your system use (e,g,, Google, FalconView, open-source options)?  Does it assist Digital Terrain Elevation Information (DTED) / Digital Elevation Mannequin (DEM) knowledge, Division of Protection (DoD) normal mapping, and disconnected operations?  What are the necessities for loading maps and DTED knowledge?
3B.13  How does the GCS talk with the AV?  Describe the info hyperlink, together with waveform, operational frequency bands, bandwidth, analog or digital implementation, encryption, anti-jam options, and whether or not the AV can autonomously execute a mission after mission add and launch with out communications to the GCS.  Establish whether or not the info hyperlink waveform is proprietary or standards-based.
3B.14  Can your system interface with DoD widespread working image (COP) or tactical networks (e.g., TAK/ATAK, ROS/ROS2, RAS-G IOP, STANAG 4586/4609/4607)? Please describe interfaces and compliance stage.
3B.15  Can a single GCS concurrently function a number of AVs? If sure, what number of, and the way is bandwidth and deconfliction managed?

Compliance and Safety
3B.16 Is your system NDAA-compliant (NDAA Sections 848 and 889, TAA, BAA)? If sure, what’s your course of for sustaining NDAA compliance?  Present supporting documentation and proof; if no, what steps are being taken to attain compliance?

3B.17 How and the place is mission knowledge (video, stills, flight logs) saved and guarded? Describe encryption at relaxation, entry management, and log integrity.
3B.18  Are you prepared to offer the Interface Management Doc (ICD) for avionics, payload, and battery interfaces underneath acceptable knowledge rights?
3B.19  Please listing all payloads presently obtainable, in improvement, and deliberate (EO/IR, SIGINT, LIDAR, comm relay, drop kits, and so forth.), together with their TRL and availability dates.
3B.20  Describe any distinctive capabilities that improve mission efficiency (e.g., deck operations, cold-weather kits, quiet propellers, confined-area VTOL).
3B.21  Does your system assist third-party payload integration? If sure, describe bodily, electrical, and software program interfaces, and previous examples of profitable integrations.
3B.22 Does your system have natural impediment or risk detection and avoidance functionality? If sure, describe the sensors and working limits.
3B.23  Does your system have swarm functionality, or is such functionality actively underneath improvement?  If sure, describe swarm measurement, comms structure, autonomy stage, and compatibility (if any) with heterogenous platforms.

Energy and Endurance

3B.24  If battery-powered, how are batteries recharged within the area and the way lengthy does a full recharge take following a maximum-endurance flight or sortie?
3B.25  What certifications do the batteries have (e.g., UN 38.3, UL, NOSSA, S9310, and so forth.)? Describe thermal administration and transport compliance.

Firm Expertise and Manufacturing

3B.26  What’s your organization’s expertise growing small UAS? Record packages of file, airworthiness processes used, and years of manufacturing expertise.
3B.27  What number of models have been produced or fielded? Establish prospects (USG, FMS, business) and operational hours if obtainable.
3B.28  What’s the manufacturing lead time for orders of 1–50, 51–100, 101–250, and 251–500 techniques?  Embody any provide chain constraints and describe mitigation methods employed to cut back manufacturing threat and lead-time impacts.

3B.29 What’s your present most manufacturing output monthly? Present present and/or projected output underneath the next capability situations:
Capability:

• 1 line, 1 shift, 5 days per week, 8 hours per day
• 1 line, 2 shifts 5 days per week, 8 hours per day (complete 16 hours effort)
• 1 line, 3 shifts, 5 days per week, 8 hours per day (complete 24 hours effort)
• Surge capability: Further manufacturing traces.
• Time beyond regulation/weekends

Sustainment and Logistics

3B.30  Are you able to present logistical assist, spare elements, and repairs? Describe sparing philosophy and turnaround occasions.
3B.31  Are you able to present Discipline Service Consultant (FSR) assist to maintain techniques in CONUS and OCONUS austere environments?
3B.32  Please escape personnel necessities for launch, mission execution, and restoration.
3B.33  What’s the anticipated coaching time for operator qualification? Present a syllabus or abstract if obtainable.

3B.34  Describe the meeting steps required to organize the air automobile from its field-packed state and the time required by a two-person workforce.
3B.35  What upkeep actions may be carried out on the area stage and what are the estimated occasions for every motion?

3B.36  As a part of sustainment ideas for austere or expeditionary environments, describe the feasibility of supporting additive manufacturing (e.g., 3D printing) of chosen non-critical spare elements by finish customers.

If relevant, determine instance half classes (e.g., covers, mounts, brackets, non-structural parts) and any technical, certification, or data-rights concerns.

Value and Availability

3B.37  What number of air autos (AVs) are included in a single full system? What number of batteries are included, and of what sort?  What’s the estimated unit price per full system (e.g., X AVs, 1 GCS, antennas, batteries, and required gear)?  Please present a CLIN-level price breakdown and guarantee phrases.
3B.38  Is that this product commercially obtainable? If sure, describe any variations between business and authorities configurations.
3B.39  Present your CAGE code, UEI, enterprise measurement underneath NAICS Code, and any relevant socio-economic classes (8(a), SDB, HUBZone, SDVOSB, WOSB).
3B.40  Is your organization foreign-owned, managed, or influenced (FOCI)? Present mitigation plans if relevant.

3B.41  Did your system obtain authorities funding for improvement (SBIR/STTR/OTA/BAA)? Present particulars and knowledge rights assertions.
3B.42  Can you present operator and upkeep manuals, fast reference playing cards, and coaching supplies? If sure, determine codecs and classification stage.

System Efficiency and Flight Envelope

3B.43  What are the system’s max payload capability, most vary, most endurance, cruise pace, service ceiling, and wind limitations (launch, cruise, restoration)?

3B.44  Establish the precipitation and icing situations underneath which your system can safely function.

3B.45  If utilizing hybrid or inside combustion engines, describe gasoline sort, consumption charges, and hot-refuel functionality.

3B.46  Present measured acoustic, radar cross-section (RCS), and electromagnetic signatures if obtainable.

Environmental & Regulatory Compliance

3B.47  What environmental {qualifications} does your system meet (MIL-STD-810H, MIL-STD-461G, IP rankings)?

3B.48  Can your system function from shifting autos or ship decks? If sure, specify examined speeds, sea states, and corrosion safety.

3B.49  What airworthiness approvals or CONOPS have been used (FAA Half 107 waivers, COAs, SORA ranges)?

3B.50  How does your system adjust to FAA Distant ID necessities and the way can Distant ID broadcasts be disabled in denied areas when approved?

Cybersecurity & Spectrum Assurance

3B.51  Describe your cybersecurity posture (safe boot, code signing, STIG/CIS compliance, vulnerability disclosure program).

3B.52  Describe your course of for assessing, securing, and sustaining the cybersecurity posture of fielded techniques over the system lifecycle.

Responses ought to deal with, as relevant:

• Vulnerability identification and disclosure (e.g., consumption, triage, coordination)
• Patch improvement, validation, and deployment (together with disconnected or austere environments)
• Configuration administration and management of presently fielded techniques
• Replace cadence and operational influence concerns

3B.53  What spectrum authorizations do you will have (NTIA, FCC) and the way is spectrum deconfliction dealt with in multi-ship operations?

Reliability, Maintainability, and Logistics

3B.54  What reliability and diagnostic options are included (e.g., Imply Time Between Failures (MTBF), built-in check (BIT/BITE), fault detection and isolation, and upkeep alerting)?

3B.55  Describe packaging and transport necessities (case measurement/weight, MIL-STD-2073 packaging, 463L pallet compatibility).

3B.56  Are parts line-replaceable (LRUs)? Record instruments required and calibration wants.

3B.57  Present beneficial spares, consumables, and calibration intervals for one yr of operations.

3B.58  Present element lifecycle standing and expertise roadmap for the subsequent 24 months (deliberate upgrades, Finish-of-Life (EOL) notices).

3B.59  Present estimated complete price of possession (TCO) for 5 years, together with vitality price, spares burn charge, and upkeep man-hours per flight hour (MMH/FH).

Interoperability, Information, and Mission Assurance

3B.60  What metadata requirements are used for video/telemetry (Movement Imagery Requirements Board (MISB) / Key-Size-Worth (KLV))? Describe time synchronization strategies (Community Time Protocol (NTP) / Precision Time Protocol (PTP, IEEE-1588)).

3B.61  Does your system assist geo-caging and in-field updates of no-fly zones?

3B.62  Present outcomes of any interoperability testing or plug-fest participation (TAK, RAS-G IOP, STANAG 4586).

3B.63  Describe the system’s command and management (C2) structure, together with whether or not C2 interfaces are open, modular, or proprietary, and the way C2 features are distributed between the GCS, air automobile, and exterior mission techniques.

3B.64  Describe human elements design (Night time Imaginative and prescient Goggle (NVG) compatibility, glove-friendly controls, display screen readability in daylight/evening).

4. Submission/Responses/Doc Markings

SUBMISSION

All , succesful, and accountable enterprise/sources that want to reply to this RFI are requested to submit info by way of electronic mail to Contract Specialist, Ms. Karleigh Corridor at [email protected] and Procuring Contracting Officer, Ms. Kristen Ferro at [email protected].  When you’ve got any particular questions (regarding this Sources Sought Discover solely) please submit them by way of electronic mail to [email protected] and [email protected]. Informational conferences won’t be entertained right now.

E-mail MUST include the next within the topic line: “[CONTRACTOR NAME] RFI Response for MRT UAS (Discover 243-26-024, PMA-263)”

RESPONSES

Notice that file sizes bigger than 5MB usually are not beneficial, as they might not be receivable as a consequence of Navy Marine Corps Intranet safety protocol.

Responses are restricted to not more than 30 pages, not together with preprinted info materials.

As a way to maximize effectivity and decrease the hassle concerned within the analysis course of, all submissions should adjust to the next format and content material:

• 8.5 x 11-inch web page
• single-spaced typed traces
• newspaper column formatting will not be permitted
• 1-inch margins on all sides
• not smaller than a 12-point font with out condensing
• images, photos or hyperlinks are permitted
• recordsdata shall be Microsoft Workplace 2016 suitable or PDF format; no ZIP recordsdata

DOCUMENT MARKINGS

It’s incumbent upon sources offering responses to this Discover to precisely mark all knowledge with all acceptable knowledge rights, distribution, and classification markings.  All info submitted will likely be adequately safeguarded from unauthorized disclosure in accordance with FAR 15.207. All submissions have to be clearly marked with the next caption: For Official Use Solely, Releasable to Authorities Businesses for Analysis Functions Solely.  Responses that fail to adjust to the above directions or current concepts not pertinent to topic, might not be reviewed. All info acquired in response to this Discover that’s marked proprietary will likely be dealt with accordingly. Data submitted in response to this Discover is submitted for free of charge to the Authorities and won’t be returned. The Authorities is underneath no obligation to offer responses or feedback to info acquired from individuals however might request extra info following evaluation.  Notice: If particular person is a international concern or if a U.S. particular person has a workforce member or accomplice who’s a international entity, adherence to all Worldwide Visitors and Arms Laws (ITAR) is required. 

All materials supplied in response to this Request for Data shall be UNCLASSIFIED.

Authorities Assist Contractors have entered into Non-Disclosure Agreements (NDAs) with the Authorities, which precludes them from disclosing any proprietary knowledge outdoors of the Authorities. Nevertheless, if respondents need a separate NDA with Authorities assist Contractors, respondents ought to submit an NDA type, together with directions, to the factors of contact listed on this discover on the time of their submission. If respondents select to not submit an NDA type for completion, their submission of a response to this announcement constitutes consent that the Authorities Assist Contractors may have entry to their proprietary info. The Authorities will NOT be answerable for the disclosure of any confidential/proprietary info not clearly marked. At any time after receipt of Request for Data responses, the Authorities might contact respondents independently for additional clarification of the submittal.

It’s the respondent’s duty to observe this web site for the discharge of any follow-on info.

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• Feb 11, 2026 07:41 am ESTParticular Discover (Unique)

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