1. Introduction
This RFI is in accordance with the Federal Acquisition Regulation (FAR) Part 15.2 and is solely published to obtain
information for use by PEO AVN and PM UAS, Redstone Arsenal.
This RFI does not constitute an invitation for bids, a request for proposal, a solicitation, a request for quote or an
indication that the Government will contract for the items provided by responder. The Government will not
reimburse responders for any costs associated with the preparation or submission of the information requested.
Response to this RFI is strictly voluntary and will not affect any potential offeror's ability to submit an offer if the
Government releases a solicitation. The Government will disregard any requests for a solicitation package. The
Government does not intend to award a contract based on this RFI or otherwise pay for the information
requested. The Government will not return submittals to the responders. The Government may request that
responders provide additional information/details based on their initial submittals.
2. Objective
The PEO AVN/PM UAS seeks industry information to identify potential solutions for a Joint Tactical Autonomous
Resupply System (JTAARS). JTAARS is an autonomous aerial cargo delivery system organic to the maneuver
commander that shall provide options for rapid and agile sustainment of highly mobile tactical combat forces,
operating in a widely dispersed manner in the tactical support and close areas. JTAARS shall enable maneuver by
reducing the tactical force's dependence on ground lines of communication and sustainment, reducing threats to
manned convoys and manned aerial systems, lightening Soldier load, and shrinking the supply chain during day
and night operations in all environmental conditions. The system should be rugged, durable, lightweight, and ready
to use as delivered with minimal logistic, training, and support requirements. The air vehicle should be capable of
autonomous or single-person manual launch with minimal support equipment from a small, confined area. It should
be capable of either a manual or an autonomous recovery to the same launch area. The recovery method should
minimize and prevent system damage and ensure short turn-around time between missions. The Ground Control
Station (GCS) should be man-portable and consist of the necessary equipment to monitor the sensor(s) position
and status and control the aircraft.
a) Requested Information. The Government requests a general description of the potential solution's configuration to
include the GCS, data link, air vehicle(s), and support equipment. Identify the following technical attributes of the
potential solution. Notate if a specific attribute is estimated or unknown:
1) Total System Weight (Air Vehicle with payload and GCS)
2) Air Vehicle weight without payload
3) Size and weight of total system packed for shipping and tactical transport
4) Size of Air Vehicle (fuselage length and wingspan width)
5) Size and weight of the GCS
6) System level upper and lower temperature operational limits
7) System level precipitation exposure or operational flight limits
8) Maximum wind limitations (launch and recovery cross wind component limitations)
9) Maximum operational altitude limits (Above Ground Level and Pressure Altitude)
10) Describe any other MIL-STD-810 standards of compliance
11) Maximum air vehicle range (maximum range assuming no line of sight obstructions)
(Describe limiting factor or system characteristics)
12) Maximum Endurance (maximum time the air vehicle can remain airborne under standard day at sea level
conditions)
13) Maximum Air Vehicle airspeed and minimum stall airspeed
b) Provide detailed information in response to the questions listed below:
1) What is the minimum number of personnel required for system operations?
2) What is the programmed training time for operator certification?
3) To what standard and level is the data link encrypted?
4) What are the different types of flight modes and mission control methods used by the system? Describe GCS
capabilities (manual, autonomous, waypoints, loiter, hover and stare, etc.)
5) What safety features (i.e., lost link, lost Global Positioning System (GPS), etc.) are integral to the system?
6) What is the operating system software?
7) What mapping software does the system use (Google maps, Falcon View, open source, etc.); and, does the
system have Digital Terrain Elevation Data (DTED)? Does the system use Department of Defense (DoD)
mapping and imagery?
8) How does the GSC communicate with the air vehicle?
9) Is the system capable of simultaneous multiple air vehicle operations from a single GCS?
10) How does the system navigate?
11) What other unique capabilities are available with the system that may enhance mission performance?
12) Is the air vehicle water recoverable? Is recovery equipment required? If so, please provide description.
13) Does the system have a precision recovery capability? What is the recovery destination target of accuracy?
14) What is the assembly sequence from a transported configuration to launch configuration?
(A field packed system: all the required equipment to accomplish a mission and configured for field conditions
transport)
15) What is the production lead-time, including any production/delivery constraints?
16) Is logistical support available with spare parts and repairs of damaged parts?
17) What is the estimated unit cost per full system? Provide unit costs given the following quantities: 1-500, 501-
1,000, and 1,001-2,000.
18) How is the system maintained?
19) What is the Operational Readiness (OR) rate of your current system?
20) How is a system stored when not in an operational mode?
21) Set up time (time required to go from packed to system airborne)?
22) What is the system storage requirement in cubic feet?
23) What is the system fuel/power source, describe:
(a) If battery powered, how are batteries recharged and how much time is required to return to full charge
following a maximum endurance flight?
(b) Do the batteries have a certification (i.e., Underwriters Laboratories (UL), etc.)? What battery charging
equipment is required?
(c) Type/Class.
(d) Environmental Considerations / Hazardous Materials (HAZMAT).
(e) Risks associated with normal operations and mitigation.
(f) Handling/Storage/Transportation Requirements.
(g) What are the battery cycle characteristics and battery composition (expected battery lifecycles)?
The PEO AVN/PM UAS is specifically interested in systems with the following characteristics:
1) Minimum payload capacity of 125lbs (single lift)
2) Capable of transporting payload for 13 KM combat radius and returning to point of origin (26 KM round-trip)
without requiring refuel/recharge
3) Short Field Takeoff and Landing or Vertical Takeoff and Landing (VTOL)
4) Artificial intelligence enabler characteristics to support mission execution and mitigate data link, GPS navigation
interruptions, fuel cell/flight management, high density fuel cell, and/or battery power
5) Lightweight, easily portable (small size vehicle).
6) System Architecture with Modular Open Systems Approach (MOSA) interoperability characteristics including
with Scalable Control Interface (SCI).
7) Employment by a two-Soldier crew.
8) Transportable by the types of vehicles that are organic to the assigned unit, no specialty equipment or vehicles
will be necessary to transport JTAARS.
9) Capable of transporting all classes of supply.
10) Sustainment 95% Success Rate 4 PLTs / 24 HRs; 30 Min Max Repair
11) Adequate maturity for immediate production, delivery, fielding and deployment
12) All weather/all environment capability (ability operate in rain, wind, dust, hot and cold temperatures)
(+45c, cold -20c, wind 25kts and light icing .2in )
Please provide your Commercial and Government Entity (CAGE) code and business size under North American
Industry Classification System (NAICS) Code. If you are a small business per the parameters of NAICS Code, do
you also qualify under any of the sub-categories: 8(a), Small Disadvantaged Business, HUB Zone, etc.?
Are you a foreign-owned, foreign-controlled, or a foreign-influenced company? Did you receive funding to develop
your system from any Governmental agencies?
3. Responses
All interested, capable, and responsible sources that wish to respond to this RFI, please respond with a white
paper via electronic mail no later than 14 days after the above release date. Please limit responses to no more
than 20 pages, 12-point font, not including preprinted information material. Respondents shall not submit
classified information. No telephone requests will be accepted.
