MST Refuel System Requirement Specifications.pdf
PDF 39 KB Posted
- Attached to
- FY26 Expeditionary Refueling System
- Solicitation number
- FA485526BALD0001
About this file
This is a statement of requirements for a mobile single-point refueling system designed for the United States Air Force Special Operations Command (USAF/AFSOC). The system must fit within a Polaris MRZR vehicle—with the main pump and support items constrained to 48.5 inches wide by 36.0 inches long by 35.0 inches high in the cargo bed, and additional equipment limited to 48.5 inches wide by 23.0 inches long by 36.0 inches high in the rear seat area. The system must operate in austere land environments across a temperature range of -30°F to 120°F and transfer JP8, JETA, and JETA1 aviation fuel from a 5,000-gallon collapsible bladder at a discharge rate of 200 to 250 gallons per minute.
The pump must be powered by an internal combustion, multi-fuel engine with electric start and manual backup capability, weigh no more than 500 pounds with handles suitable for four-person carry, and comply with military specifications. Required features include 2.0-inch camlock hose connections, a 50.0 PSI nozzle pressure limit, a 55.0 PSI pressure relief valve, a 30-foot emergency kill switch, test ports, an on-pump flow meter, and de-fueling capability. The system shall include two 50-foot collapsible hoses with camlock ends and D3 nozzles (Cla-Val 347GF with specified options including dry-break quick disconnect, strainer ball valve, grounding cable, and hose-end regulator), one 10-foot suction hose, and HEPCV compliance. Support deliverables include an operations manual, fuel testing kit, maintenance tools, maintenance parts, and one day of training for 10 personnel at either Cannon AFB or the contractor's facility.
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Text version
MST Refuel System Requirement.
Looking for single point refueling system that fits in the cargo bed of a Polaris MRZR capable of refueling USAF/AFSOC aircraft form a collapsible fuel bladder in austere environments.
Size Requirement:
Main pump and support items fit in Bed of Polaris MRZR. NOT to exceed.
Width: 48.5in Length: 36.0in Height: 35.0in
Other equipment can/must fit in rear MRZR seat area. NOT to Exceed.
Width: 48.5in Length: 23.0in Height: 36.0in
Pump Requirements:
Location of Operations: Land, Austere Min Ops Temp: -30F Max Ops Temp: 120F Fuel to be Stored/Transferred: JP8, JETA, JETA1 Discharge Rate: 200-250 gallons/min Fuel Storage Source: 1 QTY of 5K Collapsible Bladder Hose Connections: Camlock, 2.0in, Male/Female Pump power: Internal Combustion, Multi-Fuel, Electric Start with Manual Backup Safety Standards: Mil-Spec Nozzle Pressure Limit: 50.0 PSI Emergency Stop: Yes, 30.0ft Kill switch/Deadman Test Ports: Yes Pressure Relief: Yes, 55.0 PSI Flow Meter: Yes, at pump Max Weight: 500lbs, with handles for 4 man carry/lift/move De-Fuel Capability: Yes
Hose:
2 QTY of 50.0ft collapsable hose with Camlock Ends & D3 Nozzle 1 QTY of 10.0ft suction side hard hose with Camlock Ends Max Distance from discharge point: 100.0ft Nozzle Types: Cla-Val 347GF underwing nozzle with Option "D-3C D3 male QD inlet with swivel connection", Option "R-5C 55 PSIG hose end regulator", Option QDV "Dry break quick disconnect", Option SBV "Strainer ball valve", Option H "Standard Handles", Option G "Grounding cable" HEPCV Required: Yes
System Training:
Numbers of Trainees: 10 Number of Days: 1 Location: Cannon AFB or Company Location
Support Equipment:
Operations Manuel: Yes Fuel Testing Kit: Yes Maintenance Tools: Yes Maintenance Parts: Yes
File details come from the government source that posted it. Updated .