Abstract: A system for controlling the application of firing signals to electrically fired ammunition rounds which are chambered in the gun or the like. A plurality of insulated contacts are installed in the firing chamber wall so as to connect electrically to mating insulated contacts which are built into the case of the chambered round. Various configurations of annular contact rings are provided for both the inner surface of a gun firing chamber and for the mating exterior surface of a cartridge to be positioned therein. Timing control circuitry for such systems is also disclosed, suitable for use in a single barrel gun or a multiple barrel gun of the Gatling type or a revolving chamber gun with one or more fixed barrels.

Abstract: A dual-mode, radio frequency, optical-wavelength detector apparatus includes RF-transparent optical elements adapted to focusing optical energy in a wavelength range including ultraviolet through infrared wavelengths, on an optical detector, and an RF antenna located behind the optical elements. One embodiment of the apparatus employs a Cassegrain infrared optical telescope system having a concave primary mirror, the front surface of which has applied thereto multiple layers of dielectric material comprising an interference filter reflective in a band of infrared wavelengths, and transmissive to radio frequency energy. A convex secondary mirror having a similar reflective coating is so located as to reflect infrared energy backwards through a central coaxial perforation through the primary mirror onto an infrared detector.

Abstract: A radar system (20) has a chaotic code source (22) with a chaotic code output (23), which generates a chaotic code according to a chaotic difference equation. The radar system (20) further includes a transmitter (24) with a carrier signal source (28) of a carrier signal (29), and an encoder (30) having as a first input the carrier signal (29) of the carrier signal source (28) and as a second input the chaotic code output (23) of the chaotic code source (22), and as an output a transmitted radar signal (36) having the chaotic code output (23) encoded onto the carrier signal (29). A radar system receiver (26) includes a correlator (46) having as a first input the chaotic code output (23) of the chaotic code source (22) and as a second input a received radar signal (44), and as an output an indication of the correlation of the first and second inputs. The correlation is used to determine the distance, speed, or other characteristic of an object that reflected the radar signal.

Abstract: A fragmentation warhead device has a fabric liner woven from high-strength fibers located between the explosive charge and the fragments. The liner has a maximum diameter larger than that of the overall warhead, and is compressed to fit closely around the explosive charge prior to detonation by forming one or more longitudinal folds or pleats in the fabric. The fragments are retained against the outer surface of the sleeve prior to detonation by a suitable outer enclosure, and may be located between adjacent pleats in the fabric. On detonation, the sleeve expands to contain the gases produced by the explosion for an extended period of time.

Abstract: The improved diamond composite (10) exhibits increased oxidation resistance at elevated temperatures, as well as anti-reflective properties. The composite (10) includes a diamond (12), the surfaces (14) of which are protected by an adherent coating (16) consisting essentially of a layer (18) of hafnium carbide adhering and chemically bonded to the diamond (12), a layer (20) of hafnium oxy-carbide adhering and chemically bonded to the hafnium carbide layer (18) and an oxidation-resistant layer (22) of hafnium oxide adhering and chemically bonded to the hafnium oxy-carbide layer (20). Preferably, the coating (16) is sufficiently thin so that it or at least the hafnium oxide layer (22) thereof has about one-quarterwavelength thickness. The method of forming the composite (10) employs sputtering hafnium metal in an argon atmosphere, preferably at about 100.degree.

Abstract: A multi-spectral seeker system for detecting radiation in the infrared (IR) band and a plurality of radio frequency (RF) bands suitable for use in a guided missile is disclosed. The IR and RF seekers are coaxially integrated on a single gimbaled platform and share a common aperture without significant performance degradation. In the preferred embodiment, the IR seeker uses a Cassegrainian reflector assembly with surfaces reflective to IR but transparent to RF signals. The first RF seeker uses a resonant dichroic reflector antenna which is transparent to RF signals at frequencies no closer than 0.5 octaves from the dichroic reflector system operating frequency. The second RF seeker may use any suitable RF antenna system although a planar-array of multi-mode spiral antennas or a standard flat plate slotted array are preferred. The second RF seeker may operate in an active, semi-active, or passive mode.

Abstract: An unmanned air vehicle capable of vertical take-off and landing, hovering and high-speed horizontal cruise flight. A forward centerbody houses an engine and carries a single rotor assembly having a plurality of propellers lying in a plane substantially perpendicular to the centerline of the forward centerbody. A coaxial aft centerbody is secured to the aft end of the forward centerbody and typically houses the vehicle avionics. A plurality of stators extend outwardly of the aft centerbody, in a plane substantially parallel to the propellers. A single toroidal duct surrounds the rotor assembly and the stators and is secured to the stators. A plurality of movable control vanes are secured between the duct and aft centerbody aft of the stators. A flight control system, typically housed in the aft centerbody, controls the engine and the vanes to cause the vehicle to selectively move upwardly, downwardly, hover or translate to forward, horizontal, motion with the rotor in a plane within 80.degree. of vertical.

Abstract: A radar homing system in a guided missile for intercepting one of a group of targets, such as aircraft flying in formation. Offset circuitry places undesired Doppler target returns outside of the IF filter bandpass frequency of the system. The system is designed to take cognizance of the highest Doppler frequency derived from the targets.

Abstract: A fixture for performing tensile tests on advanced materials at extremely high temperatures (greater than 2500 degrees fahrenheit). The fixture allows gripping a specimen without introducing thermal gradient in the specimen. It incorporates a self aligning feature while avoiding thermal stress problems inherent in using different materials at elevated temperatures.

Abstract: A circuit arrangement to convert high voltage direct current energy into radio frequency energy that includes photoconductive switch means which is periodically closed by a pulsed light source, such as a laser, to generate the radio frequency energy. A segmented transmission line which includes a plurality of photoconductive switches positioned a half-wavelength apart that are closed simultaneously by the laser may be used to generate the radio frequency energy. The photoconductive switches may also be connected in parallel and closed by time delayed light pulses to generate the radio frequency energy. The pulses generated may also be used to excite a resonator circuit coupled to a load to increase the duration of the high frequency oscillation and to shape (filter) the resultant waveform. Other configurations utilizing photoconductive semiconductor discs and annular metal electrode configurations which may be closed by light pulses are also illustrated.

Abstract: A gimbal mount for mounting a seeker for a large look angle comprises a base support frame for attachment to an airframe, a roll axis frame having a base and a pair of spaced apart forwardly positioned gimbal supports mounted for rotation about the roll axis of the frame, a pitch gimbal ring pivotally mounted on the roll axis frame for pivoting about a pitch axis, a yaw gimbal frame pivotally mounted for pivoting about a yaw axis on the pitch gimbal, a pitch drive motor and a yaw drive motor coaxially mounted directly on and coaxial of the roll axis frame, and a drive cable connecting the respective motors to the respective gimbals.

Abstract: A method and apparatus for providing a switchable electromagnetic interference (EMI) barrier. The method protects an object against electromagnetic radiation, through the steps of: providing an object to be protected from electromagnetic radiation; placing a barrier sheet adjacent to the object, the sheet being opaque to radiation when exposed to light; directing the light against the sheet when a barrier to the radiation is desired; and extinguishing the light when passage of the radiation through the sheet is desired. One embodiment is a switchable electromagnetic radiation barrier system that includes a photoresistive sheet interposed between a source of electromagnetic radiation and an object to be protected from the radiation. This sheet is opaque to the radiation when exposed to light of a selected visible intensity range. A light source adjacent to this sheet directs the light against the sheet.

Abstract: A multichannel filter architecture having an external sequencer to provide timing and control signals which enable the filter to function as a plurality of filters because of its multiplexing operation. The filter samples input data and applies the filter functions to each sample. There may be a single input composed of either a single input or multiple time-multiplexed inputs. The multiplexing functions the same way independent of the input form. The filter functions are programmable and reprogrammable, allowing them to be changed by software rather than a redesign of hardware for a new filter function.

Abstract: A frequency-based neural network in which the state of a neuron is indicated by the frequency of an impulse stream emitted by the neuron uses an interconnectivity structure employing a frequency-modulation multiplexing scheme to weight and communicate the pulse stream from an emitting neuron to receiving neurons in another network level.

Abstract: A control system for thrust vector controlled (TVC) cruciform missiles having only pitch and yaw thrusters is disclosed wherein roll damping feedback signals are generated from bank angle data in a separate feedback loop with appropriate gain and compensation. Additional roll rate compensation is added to the missile pitch and yaw rate control subsystem by multiplying actual roll rate by pitch and yaw control deflections and inserting the resultant roll rate compensation command in the pitch and yaw rate error control loops. The addition of these two control feedback loops to the existing pitch and yaw thrust vector control system reduces roll rates caused by aerodynamic forces without the need for aerodynamic or reaction roll control means.

Abstract: Integration at the chip level is supported by an architecture for self-testing and self-configuration of an integrated circuit. Self-testing requires the generation of test signals based on primary root polynomials, application of the test signals to functionally redundant modules, and evaluation of the response of the modules to the test signals. The response produced by a module is compared against the response predicted from error-free operation of the module. Modules whose responses correspond to the expected responses are interconnected for circuit operation. All of the architecture for self-testing and self-configuration is integrated with the tested and configured modules.

Abstract: A velocity tailoring system for a defensive automatic gun having controllable muzzle velocity capability. The system includes velocity determination and control apparatus for determining the projectile discharge velocity necessary to achieve an effective target impact velocity that is less than a predetermined projectile shatter velocity. The projectile discharge velocity control signal is provided to the defensive automatic gun system.

Abstract: A folding wing structure for improved missile aerodynamic performance and manuverability with a minimum payload space requirement which comprises a leading edge spar and at least one trailing edge spar spaced apart from each other by a plurality of transverse ribs, the spars being approximately parallel to each other with the ribs positioned along the spars to divide the structure into a series of parallelograms. The spars and ribs are pivotally joined together with the spars being further pivotally joined to an air frame of an aerodynamic vehicle or missile. In a folded position the spars and rib structure collapse to occupy a minimal amount of volume in a recessed area of the air frame. A spring or piston member secured to at least one, spar forces the spars apart and out from the fuselage to an erected wing position at predetermined sweep angles relative to the fuselage.

Abstract: Broadly the disclosure relates to a warhead positioner system which includes a warhead construction comprising a cylindrical missile section having a sector-shaped ordnance charge forming one quadrant thereof, means supporting said missile section for rotational movement about the longitudinal axis of the missile, torque motor means for controlling the rotational position, and means conducting electrical signals to said torque motor from an electric seeker head whereby the charge is positioned so as to be directed toward a desired target upon being detonated. Further, the electrical signal conducting means comprise digital-type circuitry responsive to the electric seeker head output for positioning the charge in one of four quadrants and further analog circuitry for positioning the charge in either half of the selected quadrant.

Abstract: A convoluted fan structure is provided along the bottom surface of each diagonal segment of a petal-formed aft cover for a missile canister. As the cover petals open under influence of rocket exhaust impingement on the cover, the fan structures cover the diagonal areas toward the corners of the opening. This prevents recirculation of rocket exhaust gases from the plenum into the canister through the formerly open corner areas and augment the closure force to restore the petals to the closed position after completion of missile launch.