A14_MR_OC_and_or_EU_UAS_Fire_Flight_Svcs_RFI_5_2_2025_1.docx
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- Solicitation number
- 140D0425R0063
About this file
This is a Request for Information (RFI) from the Department of the Interior seeking information on fully contractor-operated and maintained fixed-wing Unmanned Aircraft Systems (UAS) for emergency fire flight services over a five-year period. The RFI outlines detailed technical specifications for UAS, including minimum and exceeded performance requirements across multiple operational parameters such as aircraft type, flight performance, launch and recovery capabilities, and command and control systems.
Key specifications include requirements for fixed-wing UAS weighing 300 pounds or less, capable of operating at density altitudes up to 15,000 feet, with flight durations up to 14 hours at maximum payload, and operational temperatures ranging from 0-115 degrees Fahrenheit. The UAS must have secure digital data links with FIPS compliant encryption, advanced loss of link capabilities, and flexible flight planning features including geo-fencing and programmable flight profiles. The solicitation number is 140D0425R0063 and focuses on emergency fire flight services for the Department of the Interior's Departmental Offices Interior Business Center.
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Department of the Interior Request for Information Non-covered UAS Emergency Fire Flight Services
Purpose: This Request for Information (RFI) is intended to identify fully contractor operated and maintained flight services for fixed-wing Unmanned Aircraft Systems (UAS) in support of the Department of the Interior (DOI) emergency fire flight services for the period of five years. Operations may include but are not limited to the following:
All minimum specifications identified in are the mandatory requirements for the UAS. Meeting exceeded specifications are of benefit to the Government and are desired but not required for award.
Flight Performance
| Item |
| Minimum Specification |
| Exceeded Specification |
| Aircraft Type |
| Fixed wing, assisted launch/landing or VTOL, runway independent, 300 pounds or less. |
| Launch and Recovery Area |
| Maximum area of 300’x300’. |
| Maximum area of 200’x200’. |
| VTOL Launch Ceiling |
| 8,500’ site DA for VTOL at max payload |
| Flight Ceiling |
| 12,000’ Density Altitude (DA) |
15,000’ DA.
| Flight Duration |
| Up to 8 hours at max payload. |
| Up to 14 hours at max payload. |
| Wind Limit |
| Takeoff/landing: 20 knots. |
| Takeoff/landing: 30 knots. |
| Wind Limit |
| Operate in sustained winds of 25 knots. |
| Operate in sustained winds of 35 knots. |
| Operational window |
| Day and night capable based on FAA criteria. |
| Temperature |
| Operational temperature of 32-100 degrees Fahrenheit. |
| Operational temperature of 0-115 degrees Fahrenheit. |
| Climb Rate |
| Climb rate of 200’/minute at minimum DA at maximum payload. |
Command and Control
| Item |
| Minimum Specification |
| Exceeded Specification |
| Range |
| C2 range of >15nm. |
| C2 range of >25nm. |
| Uplink Frequency |
| Secure digital data link with FIPS compliant encryption. |
| Downlink Frequency |
| Secure digital data link with FIPS compliant encryption. |
| Lost Link |
| Loss of Link (LOL) capability: return to launch or land now. |
| Selectable LOL: Return to launch, land now, route retrace, programmable point. |
| Flight Planning |
| Ability to program restricted areas of operations (geo-fence). |
| Ability to program a flight plan based on a GIS produced polygon (shape file). |
| Flight profile |
| Ability to loiter at an assigned altitude with <200’ deviation. |
| Transponder |
| Mode C programmable. |
| Mode C/S programmable. |
TCAS
TCAS unit at ground station.
Satellite link
Command and Control and video transmission via Satellite link
| Altimeter |
| Programmable based on altimeter setting (inHG). |
| UAS Location Display |
| Location displayed on GCS in latitude and longitude in degrees, decimal minutes (DDD MM.MM) format. |
| UAS Altitude Display |
| Altitude displayed on GCS in feet above mean sea level (MSL). |
| Radios |
| Programmable VHF AM and FM at ground station (FCC compliant). |
| Programmable VHF AM and FM mounted in the UAS. |
| Operations |
| Compliant with DOI, DOA, FAA policy (COA, ECOA, MOA, etc.). |
| Maps |
| Upload Incident Fire Operational PDF Maps for flight operations in the GCS |
Ground Terminal
| Item |
| Minimum Specification |
| Exceeded Specification |
| Live Video Feed |
| 50” monitor displaying live EO/IR gimbal feed at ground station. Display will be split screen with contextual map (fire perimeter) and camera view. |
Transmit video feed to a remote user at the incident command post (ICP) or designated location using wave/mesh/ad-hoc/MIMO networking or other technology for example Streamcaster or Starlink.
Payload
| Item |
| Minimum Specification |
| Exceeded Specification |
| Payload |
| Stabilized gimbal dual (EO/IR) Long Wave IR (LWIR) with 640 x 480 resolution. |
| Equipped with multiple modular payload configuration such as EO/IR gimbal and a separate mapping payload. Additionally include a stabilized gimbal dual (EO/IR) mid-wave (MWIR) |
| EO and IR Images |
| Capture still images in EO and IR. |
| High resolution EO/IR zoom (30-50x). |
| Mapping |
| Map a fire perimeter with the target cursor or other means. |
| Autonomous precision mapping near real-time. |
Data Standards
| Item |
| Minimum Specification |
| Exceeded Specification |
| Telemetry |
| Provide flight telemetry data upon request. |
| Video |
| Provide extractable GIS metadata (MSBI compliant) for both EO and IR. |
| Capture/transmit ESRI compliant video to be viewed/edited with the ERSI Full Motion Video (FMV) extension. |
| Fire Perimeter Data |
| Capture incremental GPS points around a fire perimeter and export them as a KML or SHP file. Desired horizontal accuracy is approximately 100’. |
| Map and share fire perimeter in real-time. |
| Points of Interest |
| Capture geotagged still images/videos as directed. Geotagging format is DDD MM.MM. Desired horizontal accuracy is approximately 100’. |
| Share geotagged images in real-time. |
| Data storage |
| Vendor will deliver/destroy data in compliance with federal standards. |
Time Requirements
| Item |
| Minimum Specification |
| Exceeded Specification |
| Mobilization |
| Vendor will be on site and operational within 72 hours of dispatch. |
| Vendor will be on site and operational within 24 hours of dispatch. |
| Data Delivery |
| Deliverable data will be provided within 4 hours of request. |
| GIS (point, line, polygon) data will be delivered to incident personal within 1 hour of request Compliant GIS and video data will be delivered to incident personal within 1 hour of request. |
| Launch (once on site and available) |
| 30 minutes after request. |
| 15 minutes after request. |
| Gimbal Tasking |
| Real-time tasking from GCS. |
| Near real-time tasking from remote user’s target. |
Requirement: The Government will direct UAS missions while supporting objectives. All collected data will be the property of the DOI. All flights will follow one of the following authorizations and are the responsibility of the contractor:
· Follow the provisions of 14 CFR Part 107
· UAS operations within restricted, prohibited and warning areas must be authorized by the controlling authority. Operators must comply with any restrictions placed on the operation by the controlling authority.
· Waiver requests under 14 CFR Part 107
· Certificate of Authorization obtained by contractor.
On-Call unit prices are intended to be a daily availability rate. Exclusive Use unit prices are intended to be a guarantee for 90 days at an estimated 540 hours, as well as the option for an additional 30 days for an estimated 180 hours. Contractors will be responsible for but not limited to:
· Transportation, system set-up, mission execution, storage, and tear down
· Support vehicles
· Potential flight operations up to 14hr/day for 14 consecutive days
· Maximum of 8hr flight time per pilot
UAS must be compliant with the requirements of Federal Acquisition Regulation (FAR) 52.240-1, Prohibition on Unmanned Aircraft Systems Manufactured or Assembled by American Security Drone Act-Covered Foreign Entities. Vendors offering UAS must identify all compliant components to ensure the requirements of the FAR clause. UAS must be <55lbs. The DOI, Office of Aviation Services (OAS), seeks the following information to be provided from vendors:
1. Is the UAS manufactured in whole or in part, by an entity domiciled in an adversary country?
Yes_____ No_____
If Yes please describe what components:
2. Identify the following critical electronic components:
| Critical Electronic Components |
| Country of Origin |
| Make |
| Model |
Flight controller
Ground control system/processor
Radios
Digital transmission devices
Cameras
Gimbal
3. Does the UAS use operating software (including cell phone or tablet applications, but not cell phone or tablet operating systems) developed, in whole or in part, by an entity domiciled in an adversary country?
Yes_____ No_____
4. Does the UAS use network connectivity or data storage located outside the United States, or administered by any entity domiciled in an adversary country?
Yes_____ No_____
5. Does the UAS contain hardware and software components used for transmitting photographs, videos, location information, flight paths, or any other data collected by the UAS manufactured by an entity domiciled in an adversary country?
Yes_____ No_____
6. Please provide a detailed list of all potential UAS and payload combinations with daily cost estimates.
7. Please provide any relevant past experience.
8. Please provide location of contractor’s home base.
The term ‘‘adversary country’’ means the Democratic People’s Republic of Korea, the Islamic Republic of Iran, the People’s Republic of China, the Russian Federation, or, as determined by the Secretary of Commerce, any other foreign nation, foreign area, or foreign non-government entity engaging in long-term patterns or serious instances of conduct significantly adverse to the national or economic security of the United States.
The term “critical electronic component” means any electronic device that stores, manipulates, or transfers digital data. The term critical electronic component does not include, for example, passive electronics such as resistors, and non-data transmitting motors, batteries, and wiring.
The term "manufactured" has the definition provided in FAR 52.225-18, as the "place where an end product is assembled out of components, or otherwise made or processed from raw materials into the finished product that is to be provided to the Government.” If a product is disassembled and reassembled, the place of reassembly is not the place of manufacture.
This announcement is for information research and planning purposes only and is not to be construed as a commitment by the Government for any actual procurement of supplies. This is not a request for proposal, request for quote, or invitation for bid, nor does its issuance obligate or restrict the Government to an acquisition approach. The Government does not intend to award a contract on the basis of any responses or pay for the preparation of information submitted or use of such information.
Depending on responses received, the Government may request additional information or demonstration units to be provided at a later date.
In addition to providing information on items one through 10 above, vendors should submit the following:
Company Name Primary Point of Contact Name Phone Number Email Address Business Size (NAICS 541360, Geophysical Surveying and Mapping)
Questions concerning this request shall be submitted no later than May 16, 2025. Questions will only be accepted via email, addressed to Contracting Officer, Stephanie Boles, Boles_proposal_submissions@ibc.doi.gov.
Submissions must be sent to Contracting Officer, Stephanie Boles, Boles_proposal_submissions@ibc.doi.gov and by 1:00 PM Eastern Time, June 6, 2025.
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