Abstract: A system for accurately measuring and delivering a predetermined amount of fuel to a vehicle for a specified mission. This system rapidly refuels vehicles to a specific wet vehicle weight. The fuel loading value is determined based upon an algorithm, which accounts for interactions of mission duration, and/or mission payload weight, and/or mission environmental effects. The fuel loading is accomplished by using one or more measuring tubes with a floating valve, which precludes the continued flow of fuel into the tank when the predetermined amount of fuel is delivered. The measuring tubes can be of specific lengths each corresponding to an output of the algorithm or a single telescoping tube that enables varying the length of the tube. Each unique tube length corresponding to a unique output of the algorithm. An alternative system comprises different sized fuel bladders. These systems enable a rapid foolproof method of refueling.

Abstract: A method of controlling a gas booster comprises computing in an engine control unit a reference discharge pressure for the gas booster. In the engine control unit, an actual discharge pressure of the gas booster and the reference discharge pressure are compared. The engine control unit generates a correcting signal derived from the step of comparing. The engine control unit sends the correcting signal to an inlet valve in flow communication with the gas booster. The inlet valve is adjusted in response to the correcting signal. It is emphasized that this abstract is provided to comply with the rules requiring an abstract that will allow a searcher or other reader to ascertain quickly the subject matter of the technical disclosure. The abstract is submitted with the understanding that it will not be used to interpret or limit the scope or meaning of the claims.