Description
The United States Air Force is seeking information on a single point refueling system that can fit in the cargo bed of a Polaris MRZR and is capable of refueling USAF/AFSOC aircraft from a collapsible fuel bladder in austere environments. The system must meet specific size and pump requirements, including a discharge rate of 200-250 gallons per minute and a fuel storage source of 1 quantity of 5K collapsible bladder. The system must also meet certain safety standards, including a nozzle pressure limit of 50.0 PSI and an emergency stop with a 30.0ft kill switch/deadman.
• The system must be capable of operating in temperatures ranging from -30F to 120F.
• The system must be able to store and transfer JP8, JETA, and JETA1 fuel.
• The system must have a hose connection with Camlock, 2.0in, Male/Female.
• The system must have a pump power with Internal Combustion, Multi-Fuel, Electric Start with Manual Backup.
• The system must have a safety standard of Mil-Spec.
• The system must have a nozzle pressure limit of 50.0 PSI.
• The system must have an emergency stop with a 30.0ft kill switch/deadman.