Abstract: A digital thermometer includes a first oscillator to generate a first clock signal, wherein a period of the first clock signal remains constant in view of changes in a temperature of the apparatus and a first counter coupled to the first oscillator, the first counter to count a fixed number of cycles of the first clock signal associated with a measurement period. The digital thermometer further includes a second oscillator to generate a second clock signal, wherein a period of the second clock signal varies with changes in the temperature and a second counter coupled to the second oscillator, the second counter to generate an output representing a count of a number of cycles of the second clock signal that occur during the measurement period. In addition, the digital thermometer includes calibration circuitry coupled to the second counter, the calibration circuitry to calibrate the output of the second counter to generate a value representing the temperature of the apparatus.

Abstract: A high density, generally recognized as safe, hybrid rocket motor is described, having a density-specific impulse similar to a solid rocket motor, with good performance approaching or equal to a liquid rocket motor. These high density hybrid motors resolve the packaging efficiency/effectiveness problems limiting the application of safe, low cost hybrid motor technology.

Abstract: A hearing aid configured for handsfree control. The hearing aid comprising one or more microphones configured to receive an input signal from the surroundings and a signal processor configured to process the input signal from the surroundings and a receiver configured to emit at least a part of said processed input signal into an ear of a hearing aid user, wherein the signal processor is further configured to process a gestural signal from a user of the hearing aid and make a control change to the hearing aid based on the gestural signal.

Abstract: A high density, generally recognized as safe, hybrid rocket motor is described, having a density-specific impulse similar to a solid rocket motor, with good performance approaching or equal to a liquid rocket motor. These high density hybrid motors resolve the packaging efficiency/effectiveness problems limiting the application of safe, low cost hybrid motor technology.

Abstract: A high density, generally recognized as safe hybrid rocket motor is described which has a density-specific impulse similar to a solid rocket motor, with good performance approaching or equal to a liquid rocket motor. These high density hybrid motors resolve the packaging efficiency/effectiveness problems limiting the application of safe, low cost hybrid motor technology.

Abstract: Described herein are compositions comprising, and methods for using a composition comprising, Staphylococcal Exfoliative Toxin A (ETA) in an amount and duration sufficient to decrease the Stratum Corneum in a region of a subjects skin.

Abstract: Described herein are compositions comprising, and methods for using a composition comprising, Staphylococcal Exfoliative Toxin A (ETA) in an amount and duration sufficient to decrease the Stratum Corneum in a region of a subjects skin.

Abstract: A high density, generally recognized as safe hybrid rocket motor is described which has a density-specific impulse similar to a solid rocket motor, with good performance approaching or equal to a liquid rocket motor. These high density hybrid motors resolve the packaging efficiency/effectiveness problems limiting the application of safe, low cost hybrid motor technology.

Abstract: Systems comprising a combination of the handheld imaging system with a nanoparticle multimodal contrast agent are disclosed. The imaging system exploits the advantages of both near-infrared emission and the photoacoustic effect by employing calcium phosphosilicate nanocolloid that encapsulates NIR and CT/MRI contrast agents for enhanced deep tissue imaging as well as a portable NIR/PA system using a tunable pulsed laser, CCD imaging technology and acoustic transducer arrays. Methods for using the system, for example in rapid diagnosis of trauma such as that inflicted on a battlefield, are provided.

Abstract: The invention relates to a device for in vivo sampling of biological species, comprising: a tubular sheath extending between a proximal end of said sheath and a distal end of said sheath, said distal end of the sheath having a projecting part, a rod extending between a proximal end of said rod and a distal end of said rod, capable of sliding in the sheath between a retracted position in which the distal end of the rod is located inside the sheath and a deployed position in which the distal end of the rod extends beyond the distal end of the sheath, said rod comprising a capturing support for capturing said biological species, made from a porous material, arranged in a distal region of the rod on a portion of the circumference of the rod such that the capturing support is located outside the sheath when the rod is in the deployed position of same.

Abstract: A universal capacitive power factor corrector usable with single phase inductive loads encases one capacitor, of 10 microfarads, one 240 volt varistor, one 22 microhenry coil, and a 330 k ohm resistor within a housing having a power cord, on off switch, 4 amp fuse, and a indicator lamp. Overall design to correct poorly designed single phase inductive current loads for home or small business.

Abstract: A bi-propellant rocket motor having controlled thermal management is disclosed. The rocket motor produces thrust using a solid or gel-phase primary propellant that can be either fuel- or oxidizer-rich, with a complementary self-pressurizing secondary propellant selected to balance the primary propellant in terms of the equivalence ratio. The motor houses multiple propellant grains arranged in such a configuration that each chamber containing a primary grain serves as both propellant storage and the main combustion chamber for that propellant grain as it burns with the secondary propellant. The secondary propellant is stored separately, and the flow routed past the primary propellant chamber to provide cooling for adjacent primary propellant chambers limiting the temperature rise in the motor structure.

Abstract: A bi-propellant rocket motor having controlled thermal management is disclosed. The rocket motor produces thrust using a solid or gel-phase primary propellant that can be either fuel- or oxidizer-rich, with a complementary self-pressurizing secondary propellant selected to balance the primary propellant in terms of the equivalence ratio. The motor houses multiple propellant grains arranged in such a configuration that each chamber containing a primary grain serves as both propellant storage and the main combustion chamber for that propellant grain as it burns with the secondary propellant. The secondary propellant is stored separately, and the flow routed past the primary propellant chamber to provide cooling for adjacent primary propellant chambers limiting the temperature rise in the motor structure.

Abstract: A module comprising: (a) a housing; (b) a tray mounted in the housing, wherein the tray comprises at least: (i) a first and second submodule, each submodule having one or more compartments for containing individual add/drop filters; (ii) a first plurality of cascaded add/drop filters installed in the first submodule; and (iii) a second plurality of cascaded add/drops filters installed in the second submodule; and (c) connectors mounted to the housing and optically connected to the fibers at the ends of the first and second plurality of cascaded add/drop filters.

Abstract: A module comprising: (a) a housing; (b) a tray mounted in the housing, wherein the tray comprises at least: (i) a first and second submodule, each submodule having one or more compartments for containing individual add/drop filters; (ii) a first plurality of cascaded add/drop filters installed in the first submodule; and (iii) a second plurality of cascaded add/drops filters installed in the second submodule; and (c) connectors mounted to the housing and optically connected to the fibers at the ends of the first and second plurality of cascaded add/drop filters.