US3027842A - Fuze - Google Patents
Fuze Download PDFInfo
- Publication number
- US3027842A US3027842A US651871A US65187146A US3027842A US 3027842 A US3027842 A US 3027842A US 651871 A US651871 A US 651871A US 65187146 A US65187146 A US 65187146A US 3027842 A US3027842 A US 3027842A
- Authority
- US
- United States
- Prior art keywords
- oscillator
- fuze
- antenna
- coil
- projectile
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 239000004020 conductor Substances 0.000 description 12
- 230000008878 coupling Effects 0.000 description 4
- 238000010168 coupling process Methods 0.000 description 4
- 238000005859 coupling reaction Methods 0.000 description 4
- 108010036050 human cationic antimicrobial protein 57 Proteins 0.000 description 4
- 239000003990 capacitor Substances 0.000 description 3
- 150000001875 compounds Chemical class 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 230000001681 protective effect Effects 0.000 description 2
- 240000007829 Haematoxylum campechianum Species 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000009172 bursting Effects 0.000 description 1
- 238000005474 detonation Methods 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000011810 insulating material Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000004382 potting Methods 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C13/00—Proximity fuzes; Fuzes for remote detonation
- F42C13/04—Proximity fuzes; Fuzes for remote detonation operated by radio waves
Definitions
- the present invention relates generally to radio proximity fuzes and more particularly to an improved electronic fuze of the general type described in the co-pending patent application of Merle A. Tuve and Richard B. Roberts, Serial No. 471,388, filed in the United States Patent Oifice on January 6, 1943, entitled Fuze, and assigned to the same assignee as the present application and invention, now abandoned.
- a fuze of this class comprises an oscillator for generating radio frequency signals, an antenna system including an exciter antenna and a projectile casing for radiating the signals, an amplifier coupled to the oscillator for selectively amplifying a modulated signal in the oscillator plate or Work circuit, the last-mentioned signal having a predetermined amplitude indicative of tar-get proximity, and a gaseous grid-controlled discharge tube responsive to the amplified modulated signal for producing a detonating current.
- the fuze is associated with an electrical detonator controlled by this detonating current and, of course, suitable bursting changes for causing explosion of the projectile when it comes close to the target.
- the antenna system included an exciter antenna comprising a cap mounted exteriorly of the projectile nose or largely embedded therein, the soldered connection between the conductor leading from said cap to the oscillator coil became loosened, when the projectile was discharged from the gun, with resultant failure of the fuze to operate.
- This condition was brought about because the adiabatic temperature increase due to stagnation pressure on the apex of the projectile nose caused the temperature at said apex to rise to approximately 700 R, which temperature was, of course, suflicient to cause melting of the soldered connection.
- One of the principal objects of the present invention is to provide an improved radio proximity fuze wherein the exciter antenna is contained completely within the recess of the projectile nose with the result that there will be no soldered connections to be subjected to high temperatures.
- Another object of the invention resides in the provision of an improved fuze of this character which will be of relatively light weight and compact construction and capab-le of easy assembly, such considerations being of paramount importance in fuzes for use in small missiles.
- FIGURE 2 is a side elevation of the device, as seen from a substantially diametrically opposed reference position of view, and also partly broken away;
- FIGURE 4 is a circuit schematic of the oscillator, antenna and associated electrical circuits employed in the fuze.
- FIG. 4 in a brief description of the electrical elements of the embodiment shown in FIG. 1,
- an electronic tube 11 of the triode type having an electron-emitting filamentary cathode 12, a control electrode, or grid, 13, and an anode, or plate, 14.
- a single coil of conductive material 16 having an antenna extension portion 17, an impedance matching transformer section 18 and an inductance section 19, serving as the oscillator tank coil, forms a part of the oscillator.
- a conductor 20 connects a tap of coil 16 to the grid of the tube 11 and a conductor 22 connects one terminal of the coil to ground terminal 23.
- the tank circuit of the oscillator also includes a capacitor 25, connected between the ground terminal 23 and the plate or anode 14 by conductors 24 and 27.
- the numeral 45 indicates generally a converging projectile nose of plastic material and preferably of two-piece construction.
- the nose includes a base portion 47 and an ogive portion 48, and said nose has a hollow interior defining a chamber 49.
- the fuze unit including the above described electrical components is shown generally at 50, and includes a base 52 on which is mounted an amplifier unit including the above-mentioned amplifier (not shown in detail).
- the amplifier unit is surrounded by a metal shield 53, and an oscillator support 54 is rigidly secured to the top of the shield.
- the oscillator support is of circular shape and includes a base portion 55 and a mid-portion having annularly disposed circular recesses adapted to receive the resistors, chokes and capacitor.
- the oscillator support includes a coil form 56, of suitable insulating material, and said coil form surrounds the electronic tube 11 to provide a measure of protection therefor.
- the coil form is closed at its upper end by a hemispherical cap 57, which cap may be fabricated integrally with the form and which form can be made integrally with the oscillator support 54, thus providing a central well in which the tube 11 is received.
- the fuze In operation the fuze is installed in a projectile as shown in FIG. 1.
- the oscillator generates radiant-energy carrier signals.
- Target proximity changes the radiation resistance of the radiating system comprising antenna 17 and the projectile casing and this change causes a modulated signal to appear at terminal 35.
- the remaining phases of operation are like the corresponding phases of operation of the fuze described in the co-pending application referred to hcreinabove.
- the base 52, the amplifier-containing shielding member 53, the oscillator support 54, the coil form 56, and cap 57 comprise a unitary assembly for positioning the oscillator and antenna sections of the fuze in the projectile nose with optimum space utilization.
- Considerable space is saved by housing tube 11 within coil form 56.
- Another space-saving expedient is the disposition of resistors 29 and 33, capacitor 25 and chokes 38 and 42 in the space between phase portion 55 and the tip of the projectile.
- oscillator circuits such as the grid coupled and well-known Colpitts can be used, if desired.
- a signal generator in the ogive comprising an oscillator having at least one electron tube, a protective casing surrounding said tube throughout its length, a cap closing said casing and having an arcuate surface, and a coil wound on said casing and having an extended portion projecting over said cap, said coil constituting an oscillator coil and matching transformer and said extension constituting an antenna.
- said coil constituting an oscillator coil and matching transformer and said said extension constituting an antenna.
- a hollow projectile nose open at its base, a closure for the base, said closure and said nose defining a closed chamber, an oscillator housed in said chamber and having a plurality of components including an electron tube, and an oscillator support including a coil form providing a central Well and a plurality of annularly arranged recesses, said electron tube being mounted in said central well, and the components of said oscillator being disposed in said annularly arranged recesses.
- a hollow projectile nose open at its base, a closure for the base, said closure and said nose defining a closed chamber, an oscillator housed in said chamber, said oscillator having a plurality of components including an electron tube, an oscillator support including a coil form providing a central Well and a plurality of annularly arranged recesses, said electron tube being mounted in said central well, the components of said oscillator being received in said annularly arranged recesses, a hemispherical cap closing said coil form, an oscillator coil and an impedance matching transformer wound on said form, and an antenna comprising a continuation of the conductor composing said transformer, said antenna extending transversely over said cap and terminating in closely spaced relation to the topmost turn of said transformer.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
Description
J. J. HOPKINS April 3, 1962 FUZE Filed March 4, 1946 INVENTOR JOHN J HOF KIIVS BY jzfldfiw ATTORNEY United States Patent The present invention relates generally to radio proximity fuzes and more particularly to an improved electronic fuze of the general type described in the co-pending patent application of Merle A. Tuve and Richard B. Roberts, Serial No. 471,388, filed in the United States Patent Oifice on January 6, 1943, entitled Fuze, and assigned to the same assignee as the present application and invention, now abandoned.
In the abovementioned co-pending application there is disclosed an electronic fuze adapted to cause detonation of a projectile upon attainment of proximity to a target. A fuze of this class comprises an oscillator for generating radio frequency signals, an antenna system including an exciter antenna and a projectile casing for radiating the signals, an amplifier coupled to the oscillator for selectively amplifying a modulated signal in the oscillator plate or Work circuit, the last-mentioned signal having a predetermined amplitude indicative of tar-get proximity, and a gaseous grid-controlled discharge tube responsive to the amplified modulated signal for producing a detonating current. The fuze is associated with an electrical detonator controlled by this detonating current and, of course, suitable bursting changes for causing explosion of the projectile when it comes close to the target.
It has been found that where the antenna system included an exciter antenna comprising a cap mounted exteriorly of the projectile nose or largely embedded therein, the soldered connection between the conductor leading from said cap to the oscillator coil became loosened, when the projectile was discharged from the gun, with resultant failure of the fuze to operate. This condition was brought about because the adiabatic temperature increase due to stagnation pressure on the apex of the projectile nose caused the temperature at said apex to rise to approximately 700 R, which temperature was, of course, suflicient to cause melting of the soldered connection.
One of the principal objects of the present invention, therefore, is to provide an improved radio proximity fuze wherein the exciter antenna is contained completely within the recess of the projectile nose with the result that there will be no soldered connections to be subjected to high temperatures.
Another object of the invention resides in the provision of an improved fuze of this character which will be of relatively light weight and compact construction and capab-le of easy assembly, such considerations being of paramount importance in fuzes for use in small missiles.
For a better understanding of the present invention, reference is made to the following specification, taken in connection with the accompanying drawings, wherein:
FIGURE 1 is an elevational perspective view of a preferred embodiment of fuze in accordance with my invention, illustrating its relationship to broken away portions of a projectile in which it is installed;
FIGURE 2 is a side elevation of the device, as seen from a substantially diametrically opposed reference position of view, and also partly broken away;
FIGURE 3 is a top plan view of the fuze; and
FIGURE 4 is a circuit schematic of the oscillator, antenna and associated electrical circuits employed in the fuze.
Referring first to FIG. 4 in a brief description of the electrical elements of the embodiment shown in FIG. 1,
included in the fuze is an electronic tube 11 of the triode type, having an electron-emitting filamentary cathode 12, a control electrode, or grid, 13, and an anode, or plate, 14. A single coil of conductive material 16 having an antenna extension portion 17, an impedance matching transformer section 18 and an inductance section 19, serving as the oscillator tank coil, forms a part of the oscillator. Specifically, a conductor 20 connects a tap of coil 16 to the grid of the tube 11 and a conductor 22 connects one terminal of the coil to ground terminal 23. The tank circuit of the oscillator also includes a capacitor 25, connected between the ground terminal 23 and the plate or anode 14 by conductors 24 and 27. Anode 14 is coupled to a suitable source B+ of space current (not shown) through a plate resistor 29, conductor 30 and terminal 31. The signal output circuit from plate 14 comprises conductor 32, resistor 33, conductor 34 and the terminal 35, which terminal is adapted to be coupled to an amplifier input circuit. The amplifier is of the same general type as that described and illustrated in the co-pending patent application mentioned in the first paragraph of this specification and, therefore, need not be described herein. The filament heating circuit is completed from a source A (not shown) through chokes 38 and 42, conductors 37, 41, 39 and 43, and terminals 40 and 44. The circuit components and conductors illustrated in FIGS. 1, 2 and 3 have the same reference numerals as their respective assemblies shown in FIG. 4.
Referring now specifically to FIG. 1, the numeral 45 indicates generally a converging projectile nose of plastic material and preferably of two-piece construction. The nose includes a base portion 47 and an ogive portion 48, and said nose has a hollow interior defining a chamber 49.
The fuze unit including the above described electrical components is shown generally at 50, and includes a base 52 on which is mounted an amplifier unit including the above-mentioned amplifier (not shown in detail). The amplifier unit is surrounded by a metal shield 53, and an oscillator support 54 is rigidly secured to the top of the shield. The oscillator support is of circular shape and includes a base portion 55 and a mid-portion having annularly disposed circular recesses adapted to receive the resistors, chokes and capacitor. The oscillator support includes a coil form 56, of suitable insulating material, and said coil form surrounds the electronic tube 11 to provide a measure of protection therefor. The coil form is closed at its upper end by a hemispherical cap 57, which cap may be fabricated integrally with the form and which form can be made integrally with the oscillator support 54, thus providing a central well in which the tube 11 is received.
After the improved fuse has been mounted in a projectile nose during assembly, as illustrated in FIG. 1, a suitable potting compound is poured into the nose through openings in base 52 and base portion 55, one of these openings being shown generally at 59. Other openings may be provided to permit free flow of the compound, so that there are no air pockets, to the end that the parts may be rigidly secured in place.
In operation the fuze is installed in a projectile as shown in FIG. 1. The oscillator generates radiant-energy carrier signals. Target proximity changes the radiation resistance of the radiating system comprising antenna 17 and the projectile casing and this change causes a modulated signal to appear at terminal 35. The remaining phases of operation are like the corresponding phases of operation of the fuze described in the co-pending application referred to hcreinabove.
It will be particularly noted that the base 52, the amplifier-containing shielding member 53, the oscillator support 54, the coil form 56, and cap 57 comprise a unitary assembly for positioning the oscillator and antenna sections of the fuze in the projectile nose with optimum space utilization. Considerable space is saved by housing tube 11 within coil form 56. Another space-saving expedient is the disposition of resistors 29 and 33, capacitor 25 and chokes 38 and 42 in the space between phase portion 55 and the tip of the projectile.
It is desired particularly to point out that, in view of the fact that the antenna element 17 is contained entirely within the chamber 49, there will be no need for soldered connections to be exposed to the high temperatures present at the apex of the projectile during flight. Therefore, fuze failure due to breaking down of soldered antenna connections will be eliminated.
It will also be understood that, by substituting an antenna contained wholly within the chamber 49 for the type formerly employed, i.e., one mounted on the outer surface of the ogive of the projectile nose, or embedded therein, fuze failure due to leakage of water vapor about said antenna and into the fuze is prevented.
While there has been shown what is at present considered to be a preferred embodiment of my invention, it will be obvious to those skilled in the art that various changes and modifications may be made therein without departing from the true spirit and scope of the invention. For example, oscillator circuits such as the grid coupled and well-known Colpitts can be used, if desired.
I claim:
1. In a fuze for electrically detonated projectiles having a chambered ogive, a signal generator in the ogive and comprising an oscillator having at least one electron tube, a protective casing surrounding said tube throughout its length, a cap closing said casing and having an arcuate surface, and a coil wound on said casing and having an extended portion projecting over said cap, said coil constituting an oscillator coil and matching transformer and said extension constituting an antenna.
2. In a fuze for electrically detonated projectiles having a chambered ogive, a signal generator in the chambered ogive and comprising an oscillator having at least one electron tube, a protective casing for said tube, a cap closing said casing and having an arcuate surface,
and a coil wound on said casing and having an extended portion projecting over said cap, said coil constituting an oscillator coil and matching transformer and said said extension constituting an antenna.
3. The combination with a radio proximity fuze having a projectile nose formed with a hollow interior defining a chamber, of an oscillator for generating electromagnetic waves, said oscillator having a coil form with a coil wound thereon and a cap closing said form at one end, said cap having an arcuate surface, and an antenna electrically connected with the coil and trained over said arcuate surface, said antenna being contained wholly within the chamber and being of such electrical length that optimum electrical coupling to the projectile with consequent optimum preloading of the oscillator will take place.
4. In a radio proximity fuze, a projectile having a hollow nose defining a chamber, an electro-magnetic wave generator in the chamber, an antenna for said generaton, said antenna comprising an arcuately disposed strand of wire contained entirely within said chamber, and a hemispherical support for rigidly mounting the antenna in the chamber.
5. In a radio proximity fuze, a hollow projectile nose open at its base, a closure for the base, said closure and said nose defining a closed chamber, an oscillator housed in said chamber and having a plurality of components including an electron tube, and an oscillator support including a coil form providing a central Well and a plurality of annularly arranged recesses, said electron tube being mounted in said central well, and the components of said oscillator being disposed in said annularly arranged recesses.
6. In a radio proximity fuze, a hollow projectile nose open at its base, a closure for the base, said closure and said nose defining a closed chamber, an oscillator housed in said chamber, said oscillator having a plurality of components including an electron tube, an oscillator support including a coil form providing a central Well and a plurality of annularly arranged recesses, said electron tube being mounted in said central well, the components of said oscillator being received in said annularly arranged recesses, a hemispherical cap closing said coil form, an oscillator coil and an impedance matching transformer wound on said form, and an antenna comprising a continuation of the conductor composing said transformer, said antenna extending transversely over said cap and terminating in closely spaced relation to the topmost turn of said transformer.
References Cited in the file of this patent UNITED STATES PATENTS 1,427,833 McCullough Sept. 5, 1922 1,747,938 Hull Feb. 18, 1930 1,853,632 Mouromtseff Apr. 12, 1932 1,900,293 Logwood Mar. 7, 1933 1,993,436 Eberhard Mar. 5, 1935 2,037,946 Stusser Apr. 21, 1936 2,404,553 Wales July 23, 1946 FOREIGN PATENTS 376,783 Great Britain July 14, 1932 539,224 Great Britain Sept. 2, 1941
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US651871A US3027842A (en) | 1946-03-04 | 1946-03-04 | Fuze |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US651871A US3027842A (en) | 1946-03-04 | 1946-03-04 | Fuze |
Publications (1)
Publication Number | Publication Date |
---|---|
US3027842A true US3027842A (en) | 1962-04-03 |
Family
ID=24614556
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US651871A Expired - Lifetime US3027842A (en) | 1946-03-04 | 1946-03-04 | Fuze |
Country Status (1)
Country | Link |
---|---|
US (1) | US3027842A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3327631A (en) * | 1962-10-08 | 1967-06-27 | Giannini Controls Corp | Flight vehicle position sensing system |
US3577925A (en) * | 1965-11-26 | 1971-05-11 | Louis A Schmidt | Housing for ballistic telemetering sonde |
US3757698A (en) * | 1972-02-28 | 1973-09-11 | Us Navy | Low-interference seeker dome attachment |
US4004519A (en) * | 1976-04-12 | 1977-01-25 | The United States Of America As Represented By The Secretary Of The Navy | Projectile power generator |
US4313118A (en) * | 1980-06-30 | 1982-01-26 | Calvin Noel M | Microwave proximity sensor |
US20100058946A1 (en) * | 2008-09-08 | 2010-03-11 | Geswender Chris E | Smart fuze guidance system with replaceable fuze module |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1427833A (en) * | 1919-08-02 | 1922-09-05 | Glenn L Martin | Radiotelegraphy |
US1747938A (en) * | 1927-02-08 | 1930-02-18 | Gen Electric | Shielding system |
US1853632A (en) * | 1925-04-28 | 1932-04-12 | Westinghouse Electric & Mfg Co | Multiunit tube |
GB376783A (en) * | 1931-04-14 | 1932-07-14 | Horace William Adey | Improvements in or relating to thermionic valves |
US1900293A (en) * | 1926-10-29 | 1933-03-07 | Rca Corp | Means for increasing the selectivity of tuned radio frequency systems |
US1993436A (en) * | 1931-04-21 | 1935-03-05 | Eberhard Heinrich | Transmitter device |
US2037946A (en) * | 1933-12-26 | 1936-04-21 | Stusser Joseph | Radio receiver |
GB539224A (en) * | 1939-11-27 | 1941-09-02 | George William Walton | Improvements in or relating to the remote control of moving objects by means of radiant energy |
US2404553A (en) * | 1941-08-06 | 1946-07-23 | Jr Nathaniel B Wales | Electric fuse and setting apparatus |
-
1946
- 1946-03-04 US US651871A patent/US3027842A/en not_active Expired - Lifetime
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1427833A (en) * | 1919-08-02 | 1922-09-05 | Glenn L Martin | Radiotelegraphy |
US1853632A (en) * | 1925-04-28 | 1932-04-12 | Westinghouse Electric & Mfg Co | Multiunit tube |
US1900293A (en) * | 1926-10-29 | 1933-03-07 | Rca Corp | Means for increasing the selectivity of tuned radio frequency systems |
US1747938A (en) * | 1927-02-08 | 1930-02-18 | Gen Electric | Shielding system |
GB376783A (en) * | 1931-04-14 | 1932-07-14 | Horace William Adey | Improvements in or relating to thermionic valves |
US1993436A (en) * | 1931-04-21 | 1935-03-05 | Eberhard Heinrich | Transmitter device |
US2037946A (en) * | 1933-12-26 | 1936-04-21 | Stusser Joseph | Radio receiver |
GB539224A (en) * | 1939-11-27 | 1941-09-02 | George William Walton | Improvements in or relating to the remote control of moving objects by means of radiant energy |
US2404553A (en) * | 1941-08-06 | 1946-07-23 | Jr Nathaniel B Wales | Electric fuse and setting apparatus |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3327631A (en) * | 1962-10-08 | 1967-06-27 | Giannini Controls Corp | Flight vehicle position sensing system |
US3577925A (en) * | 1965-11-26 | 1971-05-11 | Louis A Schmidt | Housing for ballistic telemetering sonde |
US3757698A (en) * | 1972-02-28 | 1973-09-11 | Us Navy | Low-interference seeker dome attachment |
US4004519A (en) * | 1976-04-12 | 1977-01-25 | The United States Of America As Represented By The Secretary Of The Navy | Projectile power generator |
US4313118A (en) * | 1980-06-30 | 1982-01-26 | Calvin Noel M | Microwave proximity sensor |
US20100058946A1 (en) * | 2008-09-08 | 2010-03-11 | Geswender Chris E | Smart fuze guidance system with replaceable fuze module |
US7819061B2 (en) * | 2008-09-08 | 2010-10-26 | Raytheon Company | Smart fuze guidance system with replaceable fuze module |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3572247A (en) | Protective rf attenuator plug for wire-bridge detonators | |
US2264450A (en) | Gun perforator | |
US2821139A (en) | Shielded initiator | |
US4291627A (en) | Electrical fuze with a plurality of modes of operation | |
US3027842A (en) | Fuze | |
SE431590B (en) | CONTACT WITH HIGH FREQUENCY FILTER FOR AN ELECTRIC TENDER | |
US3351012A (en) | Explosive bridgewire initiators | |
US2958804A (en) | Electron beam tube and circuit | |
US2509903A (en) | Antenna and oscillator coil unit | |
US2963620A (en) | Sensing igniter | |
US4848233A (en) | Means for protecting electroexplosive devices which are subject to a wide variety of radio frequency | |
US1832052A (en) | Electric mine firing device | |
US3573831A (en) | Proximity fuze microstrip antenna | |
US3065436A (en) | Sheathed heating element | |
US3000314A (en) | Fuze | |
US2894161A (en) | Method and apparatus for electric ignition | |
GB1100374A (en) | Grenade with a shaped hollow charge | |
US2510639A (en) | Cavity resonator system | |
US1868224A (en) | Julius scbrttrmaun | |
US2947255A (en) | Projectile choke | |
US2999179A (en) | Vibration sensitive diode | |
US4063513A (en) | Target sensing device | |
GB2033553A (en) | Electric priming devices | |
US2994042A (en) | Radio frequency oscillation system | |
US2324557A (en) | Gaseous electrical discharge device |