System and method relates to a fuel control and distribution system comprising a fuel source, a fuel line, wherein the fuel source is connected to the fuel line, a fuel pump, wherein the fuel line is connected to the fuel pump, a main fuel line, wherein the fuel pump is connected to the main fuel line, a first remote transport truck, wherein the first remote transport truck comprises a first remote transport truck fuel line, wherein the main fuel line is connected to the first remote transport truck and wherein the first remote transport truck fuel line is connected to the first remote transport truck, a first tap line, wherein the first remote transport truck is connected to the first tap line, and a first fuel cap, wherein the first fuel cap comprises a first fuel level sensor, wherein the first tap line is connected to the first fuel cap and wherein the first fuel cap is adapted to be removably attached to a first equipment fuel tank.

A system delivering fire retardant materials in fighting a surface fire is provided, having an aircraft carrying the fire-retardant material, a hose deployable from the aircraft, the delivery hose connected to the reservoir and having a controllable nozzle at a deployed end with a remotely operable valve, an end effector connected by a multi-axis gimbal at the deployed end of the delivery hose the end effector having fixed wings with ailerons and elevators, and a rudder, the ailerons, elevators and rudder moved by electrical actuators, and control apparatus and circuitry in the aircraft and the end effector enabling an operator in manipulating the ailerons, elevators and the rudder. An operative in the aircraft controls the end effector via the control apparatus to fly at a lower altitude and in a different path than the aircraft, and opens the remotely operable valve to deliver the fire-retardant material from the delivery hose.

A system delivering fire retardant materials in fighting a surface fire is provided, having an aircraft carrying the fire-retardant material, a hose deployable from the aircraft, the delivery hose connected to the reservoir and having a controllable nozzle at a deployed end with a remotely operable valve, an end effector connected by a multi-axis gimbal at the deployed end of the delivery hose the end effector having fixed wings with ailerons and elevators, and a rudder, the ailerons, elevators and rudder moved by electrical actuators, and control apparatus and circuitry in the aircraft and the end effector enabling an operator in manipulating the ailerons, elevators and the rudder. An operative in the aircraft controls the end effector via the control apparatus to fly at a lower altitude and in a different path than the aircraft, and opens the remotely operable valve to deliver the fire-retardant material from the delivery hose.

A refueling system has a first vehicle having a fuel tank connected to a deployable fuel hose with a nozzle on the deployable end, a second vehicle carrying a supply of fuel, having a refueling panel with a refueling port adapted to connect to the nozzle on the deployed end of the fuel hose, an end effector joined to the fuel hose proximate the nozzle, the end effector having a plurality of thrusters providing thrust in a plurality of directions; and control circuitry in the first vehicle and in the end effector enabling an operative to vary direction and thrust of the thrusters. The operative controls the thrusters through the control circuitry to direct the nozzle toward and to connect the nozzle to the refueling port on the refueling panel of the second vehicle.

A refueling system has a first vehicle having a fuel tank connected to a deployable fuel hose with a nozzle on the deployable end, a second vehicle carrying a supply of fuel, having a refueling panel with a refueling port adapted to connect to the nozzle on the deployed end of the fuel hose, an end effector joined to the fuel hose proximate the nozzle, the end effector having a plurality of thrusters providing thrust in a plurality of directions; and control circuitry in the first vehicle and in the end effector enabling an operative to vary direction and thrust of the thrusters. The operative controls the thrusters through the control circuitry to direct the nozzle toward and to connect the nozzle to the refueling port on the refueling panel of the second vehicle.

A refueling vehicle may have a front fuel dispensing module with at least one or more hoses for dispensing fuel product from the fuel tank to an external tank. The front fuel dispensing module is located between the cab and the fuel tank containing the fuel product.

A refueling vehicle may have a front fuel dispensing module with at least one or more hoses for dispensing fuel product from the fuel tank to an external tank. The front fuel dispensing module is located between the cab and the fuel tank containing the fuel product.

Fuel delivery systems, such as those incorporated in propane trucks or other fuel delivery trucks, are provided for loading, transport and offloading of fuel and/or other deliverables. In some embodiments, a fuel transfer reel is supported forward of an engine compartment. In some embodiments, a fuel transfer reel is supported between an engine compartment and a fuel vessel.

Fuel delivery systems, such as those incorporated in propane trucks or other fuel delivery trucks, are provided for loading, transport and offloading of fuel and/or other deliverables. In some embodiments, a fuel transfer reel is supported forward of an engine compartment. In some embodiments, a fuel transfer reel is supported between an engine compartment and a fuel vessel.

A system for fighting fires has a source of fire-retardant material, a delivery hose connected to the source has a delivery nozzle at an end, and an end effector carrying the delivery hose proximate the nozzle. The end effector has controllable thrusters, an imaging device, and control circuitry including a display monitor, the control circuitry providing commands controlling actuators varying thrust and direction of the thrusters, and a valve in the delivery nozzle. With the delivery hose deployed, images from the end effector are transmitted to the control circuitry and displayed on the display monitor, and an operator viewing the images on the display monitor uses the command inputs to maneuver the end effector, carrying the nozzle at the end of the delivery hose to a position proximate an active fire, and opens the valve on the nozzle, delivering fire retardant material from the nozzle onto the fire.