Abstract: Adjustable load line amplifier circuits may comprise a power amplifier that has a signal input terminal to receive an input signal, a powered signal output terminal to be coupled to a load that has changing impedances, and a transistor array of transistor cells operatively coupled in parallel between the signal input terminal and the powered signal output terminal such that the transistor cells are independently configured to amplify the input signal present at the signal input terminal and effect a selected load line impedance of the transistor array that corresponds to at least one of the changing impedances of the load. The transistor array controller may be configured to effect the selected load line impedance by selectively activating one or more of the transistor cells and/or providing the transistor cells with a selectable operating voltage.

Abstract: Adjustable load line amplifier circuits may comprise a power amplifier that has a signal input terminal to receive an input signal, a powered signal output terminal to be coupled to a load that has changing impedances, and a transistor array of transistor cells operatively coupled in parallel between the signal input terminal and the powered signal output terminal such that the transistor cells are independently configured to amplify the input signal present at the signal input terminal and effect a selected load line impedance of the transistor array that corresponds to at least one of the changing impedances of the load. The transistor array controller may be configured to effect the selected load line impedance by selectively activating one or more of the transistor cells and/or providing the transistor cells with a selectable operating voltage.

Abstract: An active chaff may be released by an aircraft to assist the aircraft in evading at least one of radar detection and a missile. The active chaff may include a signal generator, a signal spreading device, a microprocessor, a power source, and a substantially high-drag aerodynamic envelope. The signal generator may emit a signal to assist the aircraft in evading radar detection and/or a missile. The signal spreading device may spread the generated signal. The microprocessor may control the signal generator and the signal spreading device. The power source may power the signal generator and the microprocessor.

Abstract: An active chaff may be released by an aircraft to assist the aircraft in evading at least one of radar detection and a missile. The active chaff may include a signal generator, a signal spreading device, a microprocessor, a power source, and a substantially high-drag aerodynamic envelope. The signal generator may emit a signal to assist the aircraft in evading radar detection and/or a missile. The signal spreading device may spread the generated signal. The microprocessor may control the signal generator and the signal spreading device. The power source may power the signal generator and the microprocessor. Each of the signal generator, signal spreading device, microprocessor, and power source may be located on or within the substantially high-drag aerodynamic envelope.

Abstract: A temperature sensor is described that includes a base, a first set of posts attached to the base having a first coefficient of thermal expansion, a second set of posts attached to the base and having a second coefficient of thermal expansion, and two substantially parallel conductive plates forming a capacitor. The first of the conductive plates is fixed to the first set of posts and the second of the conductive plates is fixed to the second set of posts. Temperature changes cause the first set of posts and the second set of posts to elongate at different rates, thereby changing a distance between the conductive plates and therefore the resulting capacitance. A system and method are also described for determining resonant frequency associated with the sensor which correlates to the temperature at the sensor when multiple sensors are networked across a system.

Abstract: An active chaff may be released by an aircraft to assist the aircraft in evading at least one of radar detection and a missile. The active chaff may include a signal generator, a signal spreading device, a microprocessor, a power source, and a substantially high-drag aerodynamic envelope. The signal generator may emit a signal to assist the aircraft in evading radar detection and/or a missile. The signal spreading device may spread the generated signal. The microprocessor may control the signal generator and the signal spreading device. The power source may power the signal generator and the microprocessor. Each of the signal generator, signal spreading device, microprocessor, and power source may be located on or within the substantially high-drag aerodynamic envelope.

Abstract: A temperature sensor is described that includes a base, a first set of posts attached to the base having a first coefficient of thermal expansion, a second set of posts attached to the base and having a second coefficient of thermal expansion, and two substantially parallel conductive plates forming a capacitor. The first of the conductive plates is fixed to the first set of posts and the second of the conductive plates is fixed to the second set of posts. Temperature changes cause the first set of posts and the second set of posts to elongate at different rates, thereby changing a distance between the conductive plates and therefore the resulting capacitance. A system and method are also described for determining resonant frequency associated with the sensor which correlates to the temperature at the sensor when multiple sensors are networked across a system.