Abstract: A cartridge having an electrothermal ignition device, in which, ignition conduits extend axially through a first propellant-charge powder (4) filling a cartridge sleeve (5), with the conduits essentially comprising an electrical wire (11-13) that is guided axially through a tube (14-16) comprising a second propellant-charge powder. Propellant-charge-powder tubes (14-16) comprising an optically transparent propellant-charge powder are used so that even cartridges (1) having a first propellant-charge powder (4) that is difficult to ignite can be ignited rapidly and reliably, requiring the smallest possible quantity of electrical energy.

Abstract: A propellant system for launching a large-caliber projectile includes a propellant having at least three partial charges. The first partial charge is adapted to acceleration requirements of the projectile; the second partial charge has a higher combustion velocity than that of the first partial charge; and the third partial charge has a lower combustion velocity than that of the first partial charge. The propellant system further includes an electric energy supply and control device connected to the propellant for igniting the propellant. The electric energy supply and control device has a plasma generator for affecting a combustion behavior of the propellant such as to obtain for said first partial charge, after ignition of the propellant, a maximum gas pressure level of always the same magnitude independently from an initial propellant temperature, and to obtain, for the third partial charge, a conversion such as to prolong the maximum gas pressure level in a predeterminable manner.

Abstract: An ammunition cartridge with electric propellant ignition includes a combustible case having a length dimension, a rearward end closed by a metal case bottom and a front end; a combustible propellant powder contained in the case; and an electrically insulated high-voltage electrode passing through the case bottom into the case. The electrode has an outer end situated externally of the case and is connectable to a current source and an inner end situated within the case. A current distributor is situated within the case and is electrically connected to the inner end of the electrode. At least three conductor wires are electrically connected to the current distributor and extend at least partially parallel to the length dimension within the case through the propellant powder. An electric contact arrangement is situated within the case in the front end thereof and is secured to the case.

Abstract: A method of coating an inner face of a metal tube with an electrically conducting coating material includes the steps of positioning a wire, made of the coating material, generally axially in an interior of the tube, along the inner face thereof; and passing an electric current pulse of sufficient intensity through the wire to cause an explosive vaporization thereof, whereby particles of the vaporized material impinge on the inner face of the metal tube and form a layer thereon.

Abstract: A method and an arrangement are provided for breaking up composite material comprised of elastic materials combined with metallic materials. The composite material is placed into an insulated vat holding liquid nitrogen via a transporting device and is positioned below a unipolar electrode arrangement. An energy source generates high-energy pulses that are applied to the composite material by the electrode arrangement. The composite material is torn apart by the high-energy pulses and is separated by a subsequently resulting pressure pulse.

Abstract: A device for protecting an optical component from a laser beam. The device includes a carrier which is light-pervious in a predetermined spectral range and is positionable in an expected path of a laser beam directed to the optical component; and a metal oxide film applied to the carrier. The film is light-pervious in the same spectral range and is oriented such as to intercept a laser beam directed to the optical component.

Abstract: An energy converter for generating high-power pulses includes a housing defining a chamber having an open side; an electrode assembly supported in the chamber; a power supply for applying a voltage to the electrode assembly; a fluid medium accommodated in the housing and being in contact with the electrode assembly for receiving pulses from the electrode assembly; and a diaphragm attached to the housing and closing the open side of the housing for encapsulating the electrode assembly and the fluid medium in the chamber. The diaphragm has an inner surface oriented toward the chamber and is in contact with the fluid medium. The diaphragm further has an outer surface oriented away from the chamber and is arranged for contacting a substance to be comminuted, whereby mechanical pulses transmitted from the fluid medium to the diaphragm are applied by the diaphragm to the substance to be comminuted.

Abstract: An apparatus for continuously applying a coating to a running web, includes an elastic doctor blade having first and second ends, a frontal ride adapted to be oriented towards the web and a reverse side opposite the frontal aide and adapted to be oriented away from the web. The apparatus further has a clamping device firmly holding the doctor blade by engagement therewith in a zone of the first end. The clamping device positions the doctor blade for contacting the web at the second end along a scraping line. The apparatus also has an inflatable actuator engaging the reverse side of the doctor blade between the clamping device and the first and of the doctor blade. The actuator has a pressurized state in which a surface portion of the actuator is enlarged by an inflating fluid towards the reverse side of the doctor blade for pressing it against the web. A fluid pressure source is connected to the in inflatable actuator.

Abstract: A method and apparatus for determining the roll angle position of a rotating flying body (2) relative to a fixed station (1) with the aid of a laser (3) light beam (4, 24) emitted by the fixed station (1) and received by the flying body (2). To determine the roll angle position of the flying body located at an arbitrary position within the guide beam (4) precisely and simply, a phase-coded laser light beam (guide beam) is produced with the aid of an optical element, particularly a holographic optical element (6). This guide beam (14) is then decoded in a receiving apparatus (8) of the flying body by means of a further holographic element (11) that is rigidly connected to the flying body (2). The further holographic element (11) is configured such that maximum brightness or intensity only occurs at the receiving detector (13) if it is located parallel to the holographic element (11) on the side of the laser (3), i.e., non-mirror-symmetric information must be impressed upon the guide beam (4).

Abstract: An apparatus for flight path correction of flying bodies, such as projectiles, rockets and the like, with the aid of a laser guide beam, wherein the course of the respective flying body is determined and processed in a measuring apparatus associated with the firing apparatus and containing an optical receiving detector in order to obtain an appropriate correction signal, and wherein the correction signal is then transmitted, through encoding of the laser guide beam, to a receiving apparatus disposed in the tail portion of the flying body. To determine the course of the flying body in a simple manner, both an optical light source for producing a light beam and an optical receiving detector are disposed on the measuring apparatus, and triple reflector or mirror elements, that reflect the incident light beam back in its initial direction independently of the respective angle of incidence, are disposed on the bottom of the flying body or at the ends of the guiding mechanism of the flying body.

Abstract: A method and an apparatus for flight path correction of one or more projectiles (2-6) with the aid of a guide beam (9), wherein target data, such as speed, range and direction of movement, are continuously acquired in a fire-guidance system associated with the firing device (1), for example, an automatic cannon, and are transmitted to the laser apparatus (21) that produces the guide beam (9), and wherein each projectile includes a receiving apparatus (31) which receives the guide beam (9).

Abstract: A gun barrel has an erosion-reducing, electrically non-conductive lining extending along a length portion of the gun barrel. The lining is made of a polyimide.

Abstract: In order to be able to automatically locate and map ammunition over a large area without endangering the searching crew, ground-scanning sensors are mounted on a relatively light-weight, unmanned, remote-controlled vehicle which then travels over the area contaminated with ammunition. The controlled vehicle is controlled from, and the sensor signals are evaluated in, a second vehicle which is generally disposed in the immediate vicinity of the area being examined. The controlling vehicle, which is preferably armored, also accommodates the operating crew.

Abstract: An acceleration sensor includes a silicon substrate with a micromechanical bender bar constituting a testing mass having one end mounted the silicon substrate and a free end opposite the one end. A ferromagnetic core is mounted on the free end of the micromechanical bender bar. An excitation coil is supported on the ferromagnetic core for furnishing an inhomogeneous magnetic field when supplied with an alternating current. A cooled superconducting quantum interference detector (SQUID) arrangement is mounted adjacent the ferromagnetic core for detecting changes in the inhomogeneous magnetic field produced by the excitation coil and produces a useful signal in dependence of changes in the inhomogeneous magnetic field.

Abstract: An electrothermal firing device (1) including a tube containing a charge chamber (4') in which a first electrode (9) is disposed at the end of the charge chamber (4') adjacent the breechblock (2) and a second electrode (10) is disposed at the end of the charge chamber adjacent the projectile (6). To permit the first electrode (9) adjacent the breechblock to be arranged in the charge chamber without expensive supports, in contrast to such prior art devices, this first electrode (9) is configured as the grounded electrode and the second electrode (10) is configured as the high voltage electrode. Preferably, the two electrodes (9, 10) are arranged in an exchangeable cartouche (18) so that conventional charge chambers employing corresponding loading devices can be retrofitted in a simple manner for use with electrothermal firing devices (1).

Abstract: A rail gun for accelerating a projectile therein includes a hollow insulating body forming a gun tube; and two rail assemblies supported in the gun tube and together defining an acceleration channel to accommodate a projectile for being propelled therein by a plasma armature generated by a high intensity current flowing through the rail assemblies and an electric arc connecting the rail assemblies. At least one of the rail assemblies includes a layer of an electrically conducting metal wool mass extending along and bounding the acceleration channel and an insulating substance held in the metal wool mass.

Abstract: A flying body is provided with target detection capability. The flying body has an exterior wall and a target detection device for scanning a target area disposed within the body. The target detection device includes a combined laser transmitting/receiving system, having a laser and a laser radiation detector, stationarily mounted within the flying body. A holder is displaceably mounted for movement between a first position within the body and a second position where the holder extends outside of the exterior wall of the body. A first deflection mirror is disposed on the holder for reflecting radiation coming from the target area onto the laser radiation detector when the holder is in the second position. Additionally, a second deflection mirror is disposed on the holder for deflecting radiation coming from the laser toward the target area when the holder is in the second position.

Abstract: A radar antenna arrangement (1) for a determination of the effective radar backscatter cross section .sigma..sub.eff of radar targets (2) as a function of the geometrical position of the target with reference to the radar antenna arrangement to be able to determine the effective radar backscatter cross section in a simple manner, even for a case where the radar beam no longer fully illuminates the radar target (2) to be examined and the position of the phase center (15) of the antenna (11) changes relative to the target (2), the radar antenna (11) is arranged on a rotatable antenna platform (10) outside of the rotation axis (12) of the antenna platform (10). In order to be able to scan the entire radar target (2) successively in time, the antenna platform (10) is pivotal about two axes (13, 14) that are perpendicular to the rotation axis (12). The radar target (2) to be examined is disposed on a revolving platform (3) which likewise rotates during the measuring process.

Abstract: To obtain high contrast images of objects which are in an area covered with rich vegetation and which additionally are given a camouflage coating, the wavelength specific differences in reflection behavior of the clutter and of the camouflage coating of the object are utilized. For this purpose, the apparatus according to the invention includes at least two image pick-up elements, particularly CCD cameras, whose output signals are fed to a signal processing arrangement whereby are combined. On the side of the object, respective optical filters are disposed in front of the image pick-up elements so as to cause each image pick-up element to have its maximum sensitivity in a different spectral range.

Abstract: A propellant casing assembly for an electrothermic projectile firing device has a casing and an electrically energizable coil disposed in the casing. The coil vaporizes at a predetermined current intensity and generates at least one part of propellant gases for accelerating a projectile.