Abstract: A propulsion system for an airplane to permit it to achieve vertical and/or short take-offs and landings. The propulsion system is integrated into a wing/nacelle unit and includes a thrust vectoring system. A separate flow turbofan engine is mounted in each wing/nacelle unit. A system of three flaps is located at the rear of each wing/nacelle unit for deflecting the turbofan engine exhaust downward, rearward, or any angle in between. These three flaps are arranged to provide a main thrust nozzle in the horizontal flight position without any additional flaps between them. One flap is located at the wing/nacelle upper surface trailing edge. Two slots are provided at the leading edge of this flap. The upper forward most slot is provided as an exit nozzle for the engine turbine exhaust, which is shrouded from the fan exhaust. The second of these two slots removes a portion of the high energy fan exhaust from the fan discharge duct and ejects it over the flap upper surface.

Abstract: A technique for correlating two images, differing in size, but of identical spatial content. The technique is based on the Cauchy-Schwarz Inequality and is derived in such a way as to eliminate the requirement for division, thereby realizing practical real time implementation with presently available electronic hardware. In the embodiment disclosed, reference and data image signals require no pre-processing for the removal of mean and gain factors prior to being individually supplied to the correlator. The correlator is built around modules which can be configured serially with delay lines to adapt to virtually any image configuration. Simulation tests have shown the embodiment to be superior to prior art correlators utilizing other algorithms under conditions of noise, offset and gain differences.

Abstract: A time shared transceiver laser system which may be rapidly switched between two subsystems while using the full power of the laser beam and which also generates a local oscillator beam required for coherent detection. A method of time sharing and for generating the local oscillator is disclosed.

Abstract: A method for augmenting a noise-adaptive predictive proportional navigation terminal guidance scheme. In a third order configuration with noise adaptive varying gain parameters calculated as a function of time-to-go, this system implements an optimal control law to augment proportional navigation with a target acceleration feed forward term and a navigation ratio which is a function of time-to-go and the control effort weighting factor. This third order system may also implement another optimal control law to even greater advantage, taking into account not only target acceleration but also missile acceleration in a feedback loop which, together with the navigation ratio, are both functions of time-to-go and autopilot dynamics, whereby first order autopilot time lag is accounted for. This system is particularly useful for high and medium altitude targets and results in significant miss distance improvement for terminal guidance against small maneuvering targets.

Abstract: A system for testing digital circuit units at the design speed of the circuit. A first memory stores a minimized set of optimum generated predetermined test patterns for application to a unit under test. A second memory stores expected signature patterns corresponding to signature patterns that are derived from the unit under test in response to the predetermined test patterns when the unit under test is functioning properly. A signature analyzer derives signature patterns from a unit under test in response to the application of the test patterns to the unit. A comparator compares the derived signature patterns with the expected signature patterns and provides an indication of the results of the comparison.

Abstract: A removable and replaceable locating pin adapted to locate a workpiece on a tooling fixture for machining thereof. The locating pin includes a locator pin having various illustrated configurations is adapted to cooperate with a workpiece for positioning the workpiece in various directions of restraint. The locating pin is provided with manually actuatable locking means that permits easy adjustment or removal of the specific locator pin as a particular machining operation may require. Flexibility of the set up of the tooling for machining of a workpiece is enhanced.

Abstract: Method and apparatus which allows the component leads of pre-taped electronic components to be solder tinned to preserve the solderability and shelf life of such component leads. Pre-taped electronic components and the like are prepackaged in a reel and positioned in the apparatus such that the reel is free to rotate. Both leads of each component are secured to corresponding adjacent component leads by tape. The electronic components are moved through a plurality of processing stages such that one lead of each component is solder tinned, one of the processing stages removing the tape from the leads to enable the soldering thereof. After soldering of the leads, tape is applied thereto. The process is then repeated for the other leads of each component.

Abstract: A pouch for protecting electrosensitive components contained therein from physical shock and electrostatic damage during handling and storage. In one embodiment, the pouch comprises two composite panels, each comprising a sheet of conductive material as the outside layer, a sheet of electrostatic-free material as the inside layer and a layer of open cell cushioning material sandwiched therebetween. Each panel is sealed to enclose the material therein and both panels are then sealed together on both sides and one end. The open end has an interlocking closure to allow components to be inserted into the pouch and for the pouch to be thereafter closed.In another embodiment, the pouch is formed of a pair of extruded, tubular members respectively constituting the conductive material layer and the electrostatic-free material layer with sheets of cushioning material sandwiched between them. The assembly is sealed at one end and provided with a releasable closure member at the other end.

Abstract: A fragile, movable apparatus such as a rotatable infrared optical prism assembly is mounted in a projectile housing on a crushable support pad. When the projectile is launched, the fragile, movable apparatus crushes the pad and receives effective support from the pad. After launch, a resilient member positions the fragile, movable apparatus away from the crushed pad and provides the necessary freedom of movement for the fragile, movable apparatus.

Abstract: A method for augmenting a noise-adaptive predictive proportional navigation terminal guidance scheme. In a fourth order configuration with noise adaptive varying gain parameters calculated as a function of time-to-go, this system implements an optimal control law to augment proportional navigation with target and missile information terms and a navigation ratio which is a function of time-to-go. By employing a fourth order system, enhanced use may be made of information already available in the guidance computer and missile control system to decouple target motion information from the missile control signals. Decoupled target motion information facilitates blind-mode operation in the end game, the last few seconds before intercept. Decoupled missile control information enables the airframe to be controlled to predefined orientations for aimed warhead applications.

Abstract: A method for augmenting the value of range uplink information in a predictive proportional navigation terminal guidance scheme. A second order configuration, with noise adaptive varying gain parameters calculated as a function of time-to-go, is particularly useful for high altitude, minimally maneuvering targets. This configuration results in acceptable miss distances, better than conventional proportional navigation, with sensitivity to unmodeled errors being substantially less than that in modern guidance systems. A third order configuration makes enhanced use of range uplink information to provide improved terminal guidance against lower altitude maneuvering targets. The sensitivity of the third order configuration is similar to that of conventional proportional navigation but with better miss distance results.

Abstract: Method and apparatus which allows the component leads of pre-taped electronic components to be solder tinned to preserve the solderability and shelf life of such component leads. Pre-taped electronic components and the like are prepackaged in a reel and positioned in the apparatus such that the reel is free to rotate. Both leads of each component are secured to corresponding adjacent component leads by tape. The electronic components are moved through a plurality of processing stages such that one lead of each component is solder tinned, one of the processing stages removing the tape from the leads to enable the soldering thereof. After soldering of the leads, tape is applied thereto. The process is then repeated for the other leads of each component.

Abstract: A pivotal pistol grip firing mechanism mountable upon an operator-portable rocket launcher for use in aiming and electrically arming and firing a rocket loaded within the launcher is disclosed. A mounting bracket attached to the exterior of the launcher supports a pistol grip pivotally, between a carrying position and a firing position. The pistol grip houses a percussion activated thermal battery together with a firing pin assembly for activating the battery to supply power to fire the rocket. Energy to activate the thermal battery is not available until a firing pin spring is compressed by positioning the pistol grip in the firing position. A trigger and safety lever assembly in the pistol grip control the release of the firing pin. A manual safety switch in the pistol grip circuitry prevents transmission of the battery output unless closed by the operator prior to firing.

Abstract: A missile launching system adapted for installation in a standard commercial aircraft without modification of the aircraft structure. The system comprises a plurality of frame members, linear tracks which are movable longitudinally relative to the frame members, a plurality of launch tubes for storing the missiles, an exit port for installation in an pre-established aircraft fuselage opening, and associated equipment for selectively launching the missiles from the launch tubes through the exit port. The entire system is assembled from individual components, all of which are sized to be placed on board the aircraft through a standard passenger door opening. In preparation for installing the system in a commercial aircraft, the passenger seats and related equipment conventionally installed in the interior of such an aircraft are removed. The frame members of the system are then mounted to the standard seat tracks in the floor of the aircraft.

Abstract: An injection laser is provided with a modulator which includes an external resonator cavity including a lithium niobate crystal and a spherical mirror closely coupled to the rear end of the laser with a source of bias voltage for selectively tuning the resonator for high frequency modulating the laser.

Abstract: A matrix multiplier system incorporating an integrated fiber optic coupling array in combination with an arrangement for individually modulating the signals on the respective optical fiber transmission lines to develop the matrix multiplication. Each of the individual couplers accomplishes the coupling of an input signal into a bi-directional fiber optic transmission line with high efficiency and unilateral coupling effect. The signal thus coupled into the bi-directional transmission line is reflected back to the coupler output after multiplication by the modulating vector component for the individual coupler element. Because of the fabrication of a large number of identical fiber optic couplers in a compact, integral array and the manner in which the light signals can be modulated, the matrix multiplier system is extremely effective in pattern recognition, signal discrimination, selected signal enhancement, and the like.

Abstract: A superconducting coil having an elongated longitudinally extending first hollow metallic housing and adapted to provide a cooling passage of liquid helium therein. At least one superconducting metallic conductor is disposed within the housing which is surrounded with an electrical and thermal insulating material. An elongated second metallic housing surrounds the inner insulated structure and is adapted to be mechanically connected to similar structure when arranged into a coil structure having a predetermined configuration. A method of manufacture is also disclosed as well as how the novel integrated coil and case structure is advantageously employed in an improved fusion reactor structure and Magneto Hydrodynamic Magnet Structure.

Abstract: A microwave lens is constructed of a homogeneous body of closed cell rigid polyurethane foam with aluminum flakes dispursed throughout and having a configuration defining an axis and opposed lens surfaces. The method of the invention includes selecting a mold having a cavity of the appropriate configuration, preheating the mold, and filling the mold with a mixture of low density polyurethane foam components and fine aluminum flakes evenly dispersed throughout the foam structure allowing the mixture to cool and form a body of the appropriate configuration.

Abstract: Methods and apparatus are disclosed for preventing a missile's rocket exhaust gases from contacting and adversely affecting, such as by overheating, the launch rails from which a missile may be launched. Such apparatus includes orifices and pressure/flow controls in association with the rails in order to produce a cold gaseous stream directed in opposition to the exhaust gases during at least the initial phase. The stream creates a boundary plane or barrier between the rails and the exhaust gases, thereby shielding the rails from damage due to overheating.Arrangements are provided to control the time and duration of the stream so that it may be limited to the period of actual need.

Abstract: A Ka-band orthogonal hybrid fin-line mixer includes a two-piece housing forming an orthogonal hybrid-T junction having a fin-line mounted within the waveguide E-plane at the output of the orthogonal hybrid-T junction with one-half of the fin-line substrate mounted within the top waveguide housing and the other half inserted within the bottom waveguide housing.