Abstract: A circuit which performs regulator or limiter functions at current and voltage levels below the operating ranges of conventional zener diodes. The output of an op amp is connected through a diode to a main input terminal which may be connected between a power source and one end of a load resistor. A first current limiting resistor connects the main input terminal to the inverting input of the op amp. A second current limiting resistor connects the non-inverting input of the op amp to the wiper terminal of a potentiometer which permits adjustment of a simulated zener voltage V.sub.z. A pair of supply voltage terminals of the op amp are connected to voltages V.sub.cc and V.sub.ee, respectively. A pair of fixed terminals of the potentiometer are also connected to voltages V.sub.cc and V.sub.ee, respectively. The simulated zener voltage V.sub.z may be positive or negative, and may be adjusted to any value within limits determined by voltages V.sub.cc and V.sub.

Abstract: A sealing liner of flexible material such as Teflon has a downwardly tapering side wall which is positioned over a header. A case is positioned over the liner, and the top of the case is moved into engagement with the top of the liner to capture the tapered side wall of the liner between the side walls of the header and the case to provide a tight cold flow seal so that small particles working loose from the case cannot reach the header.

Abstract: Probes for testing circuitry comprising plural oriented, circular cross-section, microcircuit probes positioned in a dielectric base and having connections on the opposite side of base to attach probe circuitry. A method of manufacture of such probes includes assembling a laminate of a dielectric base, and an aluminum mandrel, drilling holes in the laminate at positions corresponding to the eventual probe positions, electroless plating the entire package, passivating the electroless plated coating, plating the entire assemblage until the holes are substantially filled with plating, separating and shearing off the layers of plating from the laminate, applying a photoresist and developing it on the aluminum side corresponding to the holes for the probes, and on the opposite side corresponding to the desired circuitry, removing the material on the aluminum side to expose the aluminum, dissolving the aluminum to expose the probes, and soldering and reflowing the solder on the probes.

Abstract: Method and apparatus for preventing combustion of exhaust gases in rocket launch systems using a plurality of launch tubes connected to a plenum including pressure sensors in each launch tube, a control system sensitive to atmospheric pressure and launch tube pressure which provides a signal to an inert gas supply flow controller to initiate flow of gas into the plenum when pressure in a launch tube, after launch of a rocket, reaches a predetermined level.

Abstract: Probes for testing circuitry comprising plural oriented, circular cross-section, microcircuit probes positioned in a dielectric base and having connections on the opposite side of base to attach probe circuitry. A method of manufacture of such probes includes assembling a laminate of a dielectric base, and an aluminum mandrel, drilling holes in the laminate at positions corresponding to the eventual probe positions, electroless plating the entire package, passivating the electroless plated coating, plating the entire assemblage until the holes are substantially filled with plating, separting and shearing off the layers of plating from the laminate, applying a photoresist and developing it on the aluminum side corresponding to the holes for the probes, and on the opposite side corresponding to the desired circuitry, removing the material on the aluminum side to expose the aluminum, dissolving the aluminum to expose the probes, and soldering and reflowing the solder on the probes.

Abstract: An undersea weapon comprising a warhead, a rocket motor, detection, homing and control systems and a hydropulse underwater propulsion system in an integral unit. The weapon is launched at a previously detected target, such as a submarine, on a ballistic trajectory through the air by means of the rocket motor. The weapon enters the water near the submarine, which is thereafter detected by an on-board system incorporating active and/or passive detection. The thus-determined submarine direction is utilized by the control system to guide the weapon toward the submarine under water. A hydropulse motor utilizes the empty rocket motor as the propulsion chamber and provides the underwater propulsion to propel the weapon through the water toward the submarine, where the warhead then detonates on contact with the submarine. Alternatively, the weapon may be air dropped near a previously detected target, in which case there need be no propellant in the rocket motor.

Abstract: A bistatic passive radar system and method for airborne use in a first aircraft in conjunction with a host transmitter located in a second aircraft that may be at a different altitude than the first aircraft, characterized by a system and method for determining the distance between the aircraft. The system for determining the distance between the aircraft includes a system for receiving radar signals from the host transmitter directly and via reflection from a selected ground target located between the two aircraft; a system coupled to the receiver for determining the apparent range R.sub.a from the host transmitter on the second aircraft to the receiver on the first aircraft in response to receipt of the radar signals; a device on the first aircraft for determining the altitude H of the first aircraft; a device on the first aircraft for determining the angle .theta.

Abstract: A receiver for locating a source of RF radiation received by a four-arm spiral antenna having an angular measurement frame normal to the antenna axis, including a detection circuit for detecting signals received from each of the spiral arms in response to receipt of RF radiation by the antenna; a first comparison circuit for comparing signals detected from a first opposite pair of the spiral arms to produce a first signal that is proportional to a first function of the frequency of the received RF radiation and the angular displacement of the radiation source in the measurement frame; a second comparison circuit for comparing signals detected from the remaining opposite pair of the spiral arms to produce a second signal that is proportional to a second function of the frequency of the received RF radiation and the angular displacement of the radiation source in the measurement frame; and a processing circuit for processing the first and second signals to produce third and fourth signals that are proportional

Abstract: A multi-burn restartable solid rocket fuel having plural layers, each independently ignitable, including a central core, and at least one outer cylindrical layer separated from the central core by a non-ignitable layer, and the method of utilization therefor including first igniting the central core in an end burned configuration, and subsequently or concurrently igniting the next adjacent layer or layers in an end burned configuration, as desired.

Abstract: A platinum-cadmium sulfide Schottky barrier photovoltaic detector which is capable of sensing near ultraviolet and short wavelength visible radiation with extremely small response to wavelengths longer than about 5200 angstroms. The detector is fabricated with both the ohmic and barrier contacts located on the same side of the cadmium sulfide substrate to facilitate wire attachment by high-speed bonding techniques. A titanium-gold-titanium infrared shield structure is deposited directly on the substrate and is utilized to provide a connection between the ohmic contact and the substrate. An insulating layer of silicon dioxide covers the shield structure. A thin layer of platinum is deposited directly on the substrate in a small central optically active area surrounded by the insulated shield structure. A metal boundary layer overlies the periphery of the platinum layer and prevents the barrier contact metalization from affecting the properties of the Schottky barrier.

Abstract: An optical floating deck modulator to modulate a control element of an electron device, such as the grid of a Klystron tube or traveling wave tube, having two high power MOSFET switching devices connected in series between a high positive and a high negative voltage source (which also supply the high voltage to the electron device) with the control element coupled between the MOSFET devices. This arrangement provides a low resistance path between the two voltage potentials and the control element being modulated, as the two MOSFET devices are switched alternately ON and OFF and thus achieves fast rise and fall times over a very high voltage swing. Each MOSFET device has a separate drive circuit (deck) and each deck comprises a photo diode information receiver coupled to a transimpedance amplifier, the output of which is amplified by a bipolar transistor amplifier and a FET amplifier. Total isolation between the decks and the information source is achieved by an optic link therebetween.

Abstract: The disclosed common aperture seeker antenna includes a parabolic array of crossed dipoles. This array is substantially reflective for radiated electrical signals in one band, and substantially transmissive for radiated electrical signals outside of that band. A monopulse (four-element) waveguide feed is rigidly positioned on the concave side of the parabolic array at the focal point thereof. The parabolic reflector antenna operates in the one band to provide a high gain active system for accurate tracking of targets. A planar spiral antenna is rigidly positioned on the convex side of the parabolic array in axial alignment with the parabolic reflector antenna. This wideband antenna operates over a multioctave frequency band below that of the one band to provide a low gain system for passive tracking of targets. The two antenna systems coexist in such a manner that each utilizes the available aperture to its fullest extent.

Abstract: An apparatus for feeding a plurality of items to a unit having a variable demand. The apparatus includes a frame rotatably supporting a first shaft in a fixed position, and a last shaft rotatably supported in a fixed position, the last shaft supplying items to the unit, the first shaft discharging the items from the apparatus at a variable rate, and at least two rotatable pivotally mounted, intermediate shafts to guide the items between the first and last shafts and accumulate them during load demand. The rate of feed by the last shaft is different from that of the first shaft and is determined at least by the extent of accumulation at the intermediate shafts, and optionally also by the differential in feed rate existing between the first and last shafts.

Abstract: A dual directional, wavelength demultiplexer including an optical fiber mounted and adhered to a curved surface having a clad single-fiber core, a planar surface extending partially into and along the fiber through the cladding, a prism mounted on the surface having two reflective surfaces positioned to receive multiple signals from the fiber travelling in opposite directions, optical gratings positioned at the reflective surfaces effective to diffract and demultiplex the signals, and photodiode arrays mounted adjacent the prism to receive the demultiplexed reflected signals.

Abstract: A tandem rocket launcher is provided by mounting plural rockets in an elongated launch tube with associated guide and launch equipment for each rocket. A conical shield is placed between the rockets which deflects exhaust gases generated by firing the forward rocket away from the rearward rocket. The shield is then removed by firing of the subsequent rocket or pivoting of two halves of the deflector away from the path of travel of the subsequent rocket.

Abstract: A propulsion motor for an underwater vehicle such as an anti-submarine weapon. The motor includes a propulsion chamber into which water is admitted and then rapidly expelled through an exhaust nozzle, developing thrust to propel the vehicle. Gas generators are used to develop the successive hydropulses to expel the water following each filling of the motor chamber with water. In one particular embodiment of an anti-submarine weapon which is directed through the air to the vicinity of a submarine by a rocket motor, the hydropulse underwater propulsion system can use the same chamber as the rocket motor.

Abstract: In a closed loop servo system in which the input signal is inaccessible and not available for measurement, but the error signal and output signal are both accessible and measurable, a filter configuration is provided which can be inserted into the error signal path of the system to reduce the undesirable effects of noise or other unwanted signals without appreciably affecting the closed loop dynamics of the overall system. In the generalized system a filter having the characteristics g(s) in LaPlace notation is inserted into the error signal path of the system to filter selected components of the error signal. A second filter having the characteristics h(s) which satisfies the equation g(s)+h(s)=1, is coupled between the output signal and the output of the filter having the characteristics g(s).

Abstract: An optical fiber wavelength demultiplexer including an optical fiber mounted and adhered to a curved surface having a clad single fiber core, a planar surface extending partially into and along the fiber through the cladding, a prism mounted on the surface having a reflective diffraction grating surface positioned to receive signals from the fiber travelling in one direction and demultiplex such signals, and an array of photodiodes mounted adjacent the prism to receive the demultiplexed signals.

Abstract: A rolling arc gimbal mount includes a base having means for attachment to a support structure and an arcuate yoke supported in the base by recirculating bearing means. The recirculating bearing including a raceway formed in opposite sides of the yoke and in opposed facing mounts on the support structure with plurality of balls or rollers disposed between the yoke guideway and the base guideway and including recirculating guides.

Abstract: A solar heat collector utilizing an elongated vertical mast to support a rectangular parabolic reflector and a transparent cover. The mast is located at the focal point of the parabolic reflector, and the fluid to be heated enters the unit at the bottom, is partially heated as it rises by convection, enters the mast at the upper portion thereof, and is transported downward while being further heated due to the mast focal point location. The unit is rotatable about the mast to maximize heat transfer.