US3926120A - Rain impact sensing proximity fuze - Google Patents
Rain impact sensing proximity fuze Download PDFInfo
- Publication number
- US3926120A US3926120A US090211A US9021170A US3926120A US 3926120 A US3926120 A US 3926120A US 090211 A US090211 A US 090211A US 9021170 A US9021170 A US 9021170A US 3926120 A US3926120 A US 3926120A
- Authority
- US
- United States
- Prior art keywords
- firing
- impact
- fuze
- signal
- rain
- 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
- 238000010304 firing Methods 0.000 claims abstract description 72
- 239000013078 crystal Substances 0.000 claims abstract description 5
- 230000035939 shock Effects 0.000 claims abstract description 5
- 230000003750 conditioning effect Effects 0.000 claims description 4
- 230000003213 activating effect Effects 0.000 claims description 2
- 238000005474 detonation Methods 0.000 claims description 2
- 230000003111 delayed effect Effects 0.000 abstract description 2
- 230000000694 effects Effects 0.000 description 10
- 238000013459 approach Methods 0.000 description 2
- 102220005306 rs33926796 Human genes 0.000 description 2
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 1
- 230000002159 abnormal effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 230000003116 impacting effect Effects 0.000 description 1
- 239000003112 inhibitor Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000737 periodic effect Effects 0.000 description 1
- 210000002966 serum Anatomy 0.000 description 1
- 229910052709 silver Inorganic materials 0.000 description 1
- 239000004332 silver Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C15/00—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
- F42C15/40—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein the safety or arming action is effected electrically
-
- 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
Definitions
- ABSTRACT Apparatus for momentarily desensitizing a proximity fuze in response to an impact with a raindrop.
- a rain impact sensor located in the nose cone of the fuze generates an electronic cut-off signal when the fuze hits a raindrop while in flight.
- the impact with the raindrop may also generate a spurious firing signal which can cause the firing circuit of the fuze to prefunction.
- the cut-off signal generated by the rain impact sensor is amplified, stretched and delivered to the firing circuit to effectively blank out any spurious firing signal received therein.
- the rain impact sensor may be embodied by a piezoelectric crystal mounted in the nose cone of the fuze, or a mechanical switch for sensing the shock wave generated by the impact of the raindrop, or a capacitive measuring bridge circuit that becomes unbalanced in response to the impact of the raindrop.
- the spurious firing signal is delayed before it reaches the firing circuit in order that the cutoff signal generated by the rain impact sensor will reach the firing circuit prior to any such spurious firing signal.
- This invention relates to proximity fuzes and, more particularly, to an arrangement within a proximity fuze for negating the effects of spurious firing signals caused by impacts with raindrops while in flight.
- a primary object of the present invention to provide a rain impact sensing proximity fuze that minimizes the electrical and/or mechanical effects of a fuze hitting a raindrop.
- a further object of the present invention is to provide a simple, low-cost arrangement for momentarily desensitizing a proximity fuze upon impact with a raindrop that is easily incorporated into existing fuzes.
- An additional object of the present invention is to provide a proximity fuze designed for optimum fair weather performance that contains a rain impact inhibitor that does not affect normal fuze operation.
- FIG. 1 is a block diagram of a circuit arrangement embodying the present invention.
- FIG. 2 illustrates typical wave forms generated in the circuit of FIG. 1 in accordance with the teachings of the present invention.
- the rain impact sensing proximity fuze of the present invention is illustrated generally at 10.
- a firing signal is generated at 20 when the fuze approaches a predetermined distance from the target.
- Such a firing signal is sensed by signal conditioner -22 to ensure that it is of the proper band width and frequency.
- a small delay 24 is provided in the firing signal path prior to its receipt in the firing circuit 18.
- firing circuit 18 Upon the receipt of a proper firing signal, firing circuit 18 initiates a detonator to function the explosive in the fuze.
- a spurious firing signal may be generated at 20 and may possibly be passed through signal conditioner 22 and delay 24 to firing circuit 18 and, if it be of sufficient duration and amplitude, will cause a prefunction of the fuze. Negating the effect of such spurious firing signals is a rain impact sensor 12 that generates an electronic cut-off signal in response to the impact of the fuze with the raindrop.
- the cut-off signal generated thereby is passed through an amplifier l4 and a pulse stretcher 16 to firing circuit 18.
- the receipt in firing circuit 18 of the amplified and stretched cutoff signal momentarily desensitizes firing circuit 18 so that any spurious firing signal generated at 20 will have no effect upon the firing circuit.
- wave form 26 represents a spurious rain pulse firing signal that was generated at 20 upon the impact of the nose cone of the fuze with a raindrop and was passed through signal conditioner 22 and delay 24 to firing circuit 18.
- the cut-off signal 28 is seen to have blanked out the effect of rain pulse firing signal 26 within firing circuit 18.
- rain impact sensor 12 can sense abnormal flight conditions and desensitize the fuze before the firing circuit is affected by the spurious firing signal due to the delay 24 in the normal firing signal path. Normal fuze action is restored after sveral milliseconds and the remainder of fuze operation is as if no rain were present.
- Rain impact sensor 12 may also be a quick acting, very sensitive mechanical switch mounted on or near the nose cone of the fuze so that the shock wave generated by the impact of the raindrop is sensed prior to attenuation. Such a switch would initiate an electronic circuit that blanks firing circuit 18 for a predetermined time interval.
- Rain impact impact sensor 12 may also take the form of a capacitive measuring bridge circuit that becomes unbalanced in response to the impact of the nose cone of the fuze with a raindrop impacting near the sensor.
- a normal proximity firing signal will not be inhibited in the presence of rain since the rain impact sensor generates a cut-off signal of limited duration and only upon the impact of the fuze with a raindrop, which at most can be a periodic but not continuous action. This approach to reducing the effects of rain is seen to be simple, low cost, and easily incorporated into existing fuze designs, having no effect on normal fuze operation.
- a rain impact sensing proximity fuze comprising:
- a firing circuit that initiates the detonation of said fuze
- rain impact sensing means for momentarily desensitizing said firing circuit against unwanted firing signals generated by said proximity sensing means upon the impact of a raindrop with said fuze.
- said rain impact sensing means comprises:
- a rain impact sensor for generating an electrical cut-off signal in response to the impact of said fuze with a raindrop
- said proximity sensing means includes means for delaying the receipt of said firing signal by said firing circuit whereby said momentary inhibit signal reaches said firing circuit prior to the receipt therein of a firing signal.
- said conditioning means includes an amplifier and a pulse stretcher.
- said rain impact sensor comprises a piezoelectric crystal mounted on the nose cone of said fuze.
- said rain impact sensor comprises a mechanical switch for sensing the shock wave generated by the impact of said raindrop.
- said rain impact sensor comprises a capacitive measuring bridge circuit that becomes unbalanced in response to the impact of said raindrop.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Measurement Of Length, Angles, Or The Like Using Electric Or Magnetic Means (AREA)
Abstract
Apparatus for momentarily desensitizing a proximity fuze in response to an impact with a raindrop. A rain impact sensor located in the nose cone of the fuze generates an electronic cutoff signal when the fuze hits a raindrop while in flight. The impact with the raindrop may also generate a spurious firing signal which can cause the firing circuit of the fuze to prefunction. The cut-off signal generated by the rain impact sensor is amplified, stretched and delivered to the firing circuit to effectively blank out any spurious firing signal received therein. The rain impact sensor may be embodied by a piezoelectric crystal mounted in the nose cone of the fuze, or a mechanical switch for sensing the shock wave generated by the impact of the raindrop, or a capacitive measuring bridge circuit that becomes unbalanced in response to the impact of the raindrop. The spurious firing signal is delayed before it reaches the firing circuit in order that the cut-off signal generated by the rain impact sensor will reach the firing circuit prior to any such spurious firing signal.
Description
United States Patent Williams et al.
RAIN IMPACT SENSING PROXIMITY FUZE Inventors: David Williams, Bethesda; George K. Lucey, Jr., Silver Spring, both of Md.
The United States of America as represented by the Secretary of the Army, Washington, DC.
Filed: Oct. 30, 1970 Appl. No.2 90,211
US. Cl. l02/70.2 P; 102/70.2 R;
102/702 GA Int. Cl. F42C 13/00; F42C 11/02 Field of Search... 102/702 P, 70.2 R, 70.2 GA
[56] References Cited UNITED STATES PATENTS 11/1966 Winston 102/702 R 12/1968 Resnick et al. 102/702 R 11/1970 Juliano et a1 102/702 R [57] ABSTRACT Apparatus for momentarily desensitizing a proximity fuze in response to an impact with a raindrop. A rain impact sensor located in the nose cone of the fuze generates an electronic cut-off signal when the fuze hits a raindrop while in flight. The impact with the raindrop may also generate a spurious firing signal which can cause the firing circuit of the fuze to prefunction. The cut-off signal generated by the rain impact sensor is amplified, stretched and delivered to the firing circuit to effectively blank out any spurious firing signal received therein. The rain impact sensor may be embodied by a piezoelectric crystal mounted in the nose cone of the fuze, or a mechanical switch for sensing the shock wave generated by the impact of the raindrop, or a capacitive measuring bridge circuit that becomes unbalanced in response to the impact of the raindrop. The spurious firing signal is delayed before it reaches the firing circuit in order that the cutoff signal generated by the rain impact sensor will reach the firing circuit prior to any such spurious firing signal.
7. Claims, 2 Drawing Figures RAN \MPACT PULQE SENSOR STRETCHER F\\Z\NG 8 cuzcun' 'l.0 /'I.'Z /'2 4 NORMALFllZlNC: serum.
31GNAL COND\T\ONER DELAY 1. Field of the Invention This invention relates to proximity fuzes and, more particularly, to an arrangement within a proximity fuze for negating the effects of spurious firing signals caused by impacts with raindrops while in flight.
2. Description of the Prior Art The reliability of many low cost, proximity fuzes decreases in the presence of rain. Fuzes will occasionally prefunction because of the electrical and/or mechanical effects of an impact with a raindrop For example, a loop fuze hitting a high dielectric raindrop will shift frequency momentarily and may produce a firing signal. Additionally, the mechanical impact may involve more than 100 g forces, thereby causing microphonism from which firing pulses may be generated. Certain types of fuzes may also be prefunctioned if they impact with charged raindrops. Previous attempts to minimize these effects have been largely unsuccessful due to the high cost and complexity of incorporating the necessary circuitry with existing fuze designs.
It is, therefore, a primary object of the present invention to provide a rain impact sensing proximity fuze that minimizes the electrical and/or mechanical effects of a fuze hitting a raindrop.
It is another object to provide a simple and low-cost arrangement within a proximity fuze for negating the effect of spurious firing signals in the fuze caused by impacts with raindrops while in flight.
A further object of the present invention is to provide a simple, low-cost arrangement for momentarily desensitizing a proximity fuze upon impact with a raindrop that is easily incorporated into existing fuzes.
An additional object of the present invention is to provide a proximity fuze designed for optimum fair weather performance that contains a rain impact inhibitor that does not affect normal fuze operation.
SUMMARY OF THE INVENTION Briefly, in accordance with the invention, a rain impact sensing proximity fuze is provided for momen- BRIEF DESCRIPTION OF THE DRAWINGS The specific nature of the invention as well as other objects, aspects, uses, and advantages thereof will clearly appear from the following description and from the accompanying drawings, in which:
FIG. 1 is a block diagram of a circuit arrangement embodying the present invention; and
FIG. 2 illustrates typical wave forms generated in the circuit of FIG. 1 in accordance with the teachings of the present invention.
DESCRIPTION OF THE PREFERRED EMBODIMENT Referring now to FIG. 1, the rain impact sensing proximity fuze of the present invention is illustrated generally at 10. During normal operation a firing signal is generated at 20 when the fuze approaches a predetermined distance from the target. Such a firing signal is sensed by signal conditioner -22 to ensure that it is of the proper band width and frequency. A small delay 24 is provided in the firing signal path prior to its receipt in the firing circuit 18. Upon the receipt of a proper firing signal, firing circuit 18 initiates a detonator to function the explosive in the fuze. As hereinbefore described, when a raindrop or a series of raindrops strikes the fuze while in flight, a spurious firing signal may be generated at 20 and may possibly be passed through signal conditioner 22 and delay 24 to firing circuit 18 and, if it be of sufficient duration and amplitude, will cause a prefunction of the fuze. Negating the effect of such spurious firing signals is a rain impact sensor 12 that generates an electronic cut-off signal in response to the impact of the fuze with the raindrop. The cut-off signal generated thereby is passed through an amplifier l4 and a pulse stretcher 16 to firing circuit 18. The receipt in firing circuit 18 of the amplified and stretched cutoff signal momentarily desensitizes firing circuit 18 so that any spurious firing signal generated at 20 will have no effect upon the firing circuit.
A typical desensitizing situation that occurs within firing circuit 18 is illustrated in FIG. 2 in which wave form 26 represents a spurious rain pulse firing signal that was generated at 20 upon the impact of the nose cone of the fuze with a raindrop and was passed through signal conditioner 22 and delay 24 to firing circuit 18. The same raindrop activated rain impact sensor 12, which, for example, can be a piezoelectric crystal, and produced a cut-off signal that was amplified by amplifier l4 and lengthened by pulse stretcher 16 before being fed to the gate circuit of the firing SCR within firing circuit 18. The cut-off signal 28 is seen to have blanked out the effect of rain pulse firing signal 26 within firing circuit 18. It is seen that rain impact sensor 12 can sense abnormal flight conditions and desensitize the fuze before the firing circuit is affected by the spurious firing signal due to the delay 24 in the normal firing signal path. Normal fuze action is restored after sveral milliseconds and the remainder of fuze operation is as if no rain were present.
We wish it to be understood that we do not desire to be limited to the exact details of construction shown and described, for obvious modifications will occur to a person skilled in the art.
We claim as our invention:
1. A rain impact sensing proximity fuze, comprising:
a. a firing circuit that initiates the detonation of said fuze;
b. proximity sensing means for delivering a firing signal to said firing circuit; and
c. rain impact sensing means for momentarily desensitizing said firing circuit against unwanted firing signals generated by said proximity sensing means upon the impact of a raindrop with said fuze.
2. The invention according to claim 1, wherein said rain impact sensing means comprises:
a. a rain impact sensor for generating an electrical cut-off signal in response to the impact of said fuze with a raindrop; and
b. means for conditioning said electrical cut-off signal recieved from said rain impact sensor and for delivering a momentary inhibit signal to said firing circuit that renders said firing circuit inoperative whereby any firing signal generated in response to the impact with the rain will be prevented from activating said firing circuit.
3. The invention according to claim 2 wherein said proximity sensing means includes means for delaying the receipt of said firing signal by said firing circuit whereby said momentary inhibit signal reaches said firing circuit prior to the receipt therein of a firing signal.
4. The invention according to claim 3 wherein said conditioning means includes an amplifier and a pulse stretcher.
5. The invention according to claim 3 wherein said rain impact sensor comprises a piezoelectric crystal mounted on the nose cone of said fuze.
6. The invention according to claim 3 wherein said rain impact sensor comprises a mechanical switch for sensing the shock wave generated by the impact of said raindrop.
7. The invention according to claim 3 wherein said rain impact sensor comprises a capacitive measuring bridge circuit that becomes unbalanced in response to the impact of said raindrop.
Claims (7)
1. A rain impact sensing proximity fuze, comprising: a. a firing circuit that initiates the detonation of said fuze; b. proximity sensing means for delivering a firing signal to said firing circuit; and c. rain impact sensing means for momentarily desensitizing said firing circuit against unwanted firing signals generated by said proximity sensing means upon the impact of a raindrop with said fuze.
2. The invention according to claim 1, wherein said rain impact sensing means comprises: a. a rain impact sensor for generating an electrical cut-off signal in response to the impact of said fuze with a raindrop; and b. means for conditioning said electrical cut-off signal recieved from said rain impact sensor and for delivering a momentary inhibit signal to said firing circuit that renders said firing circuit inoperative whereby any firing signal generated in response to the impact with the rain will be prevented from activating said firing circuit.
3. The invention according to claim 2 wherein said proximity sensing means includes means for delaying the receipt of said firing signal by said firing circuit whereby said momentary inhibit signal reaches said firing circuit prior to the receipt therein of a firing signal.
4. The invention according to claim 3 wherein said conditioning means includes an amplifier and a pulse stretcher.
5. The invention according to claim 3 wherein said rain impact sensor comprises a piezoelectric crystal mounted on the nose cone of said fuze.
6. The invention according to claim 3 wherein said rain impact sensor comprises a mechanical switch for sensing the shock wave generated by the impact of said raindrop.
7. The invention according to claim 3 wherein said rain impact sensor comprises a capacitive measuring bridge circuit that becomes unbalanced in response to the impact of said raindrop.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US090211A US3926120A (en) | 1970-10-30 | 1970-10-30 | Rain impact sensing proximity fuze |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US090211A US3926120A (en) | 1970-10-30 | 1970-10-30 | Rain impact sensing proximity fuze |
Publications (1)
Publication Number | Publication Date |
---|---|
US3926120A true US3926120A (en) | 1975-12-16 |
Family
ID=22221801
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US090211A Expired - Lifetime US3926120A (en) | 1970-10-30 | 1970-10-30 | Rain impact sensing proximity fuze |
Country Status (1)
Country | Link |
---|---|
US (1) | US3926120A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4019440A (en) * | 1975-07-10 | 1977-04-26 | General Dynamics, Pomona Division | Impact discriminating apparatus for missiles and the like, and method for impact discrimination |
DE3011230A1 (en) * | 1980-03-22 | 1981-10-01 | Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt | CIRCUIT ARRANGEMENT FOR AN IMPELLER |
DE3011231A1 (en) * | 1980-03-22 | 1981-10-01 | Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt | CIRCUIT ARRANGEMENT OF A COMBINED PROXIMITY AND IMPACT FUZE |
US4527105A (en) * | 1982-09-02 | 1985-07-02 | Nissan Motor Company, Limited | Automatic windshield wiper speed control with piezoelectric sensor |
US4542325A (en) * | 1983-01-28 | 1985-09-17 | Nissan Motor Company, Limited | Rain condition dependent wiper control system for an automotive vehicle |
US4584508A (en) * | 1983-01-28 | 1986-04-22 | Nissan Motor Company, Limited | Rain sensor in an automatic wiper drive control system for an automotive vehicle |
DE4034619A1 (en) * | 1990-10-31 | 1992-05-07 | Diehl Gmbh & Co | SPACING EQUIPMENT FOR A STOREY, ESPECIALLY FOR A PANZER DEFENSE FLOOR |
DE3518469B3 (en) * | 1985-05-23 | 2013-12-05 | Diehl Stiftung & Co.Kg | Method for obtaining ignition information and multi-channel detector arrangement for carrying out the method |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3282211A (en) * | 1963-10-07 | 1966-11-01 | Edward T Winston | Foliage-sensitive bomb fuze |
US3419861A (en) * | 1956-06-26 | 1968-12-31 | Navy Usa | Random frequency modulation correlation fuze system |
US3540377A (en) * | 1968-10-09 | 1970-11-17 | Magnavox Co | Power supply for electrically actuated fuse |
-
1970
- 1970-10-30 US US090211A patent/US3926120A/en not_active Expired - Lifetime
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3419861A (en) * | 1956-06-26 | 1968-12-31 | Navy Usa | Random frequency modulation correlation fuze system |
US3282211A (en) * | 1963-10-07 | 1966-11-01 | Edward T Winston | Foliage-sensitive bomb fuze |
US3540377A (en) * | 1968-10-09 | 1970-11-17 | Magnavox Co | Power supply for electrically actuated fuse |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4019440A (en) * | 1975-07-10 | 1977-04-26 | General Dynamics, Pomona Division | Impact discriminating apparatus for missiles and the like, and method for impact discrimination |
DE3011230A1 (en) * | 1980-03-22 | 1981-10-01 | Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt | CIRCUIT ARRANGEMENT FOR AN IMPELLER |
DE3011231A1 (en) * | 1980-03-22 | 1981-10-01 | Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt | CIRCUIT ARRANGEMENT OF A COMBINED PROXIMITY AND IMPACT FUZE |
US4382408A (en) * | 1980-03-22 | 1983-05-10 | Licentia Patent-Verwaltungs-Gmbh | Circuit arrangement for an impact fuze |
US4388867A (en) * | 1980-03-22 | 1983-06-21 | Licentia Patent-Verwaltungs-Gmbh | Circuit arrangement for a combined proximity and impact fuse |
US4527105A (en) * | 1982-09-02 | 1985-07-02 | Nissan Motor Company, Limited | Automatic windshield wiper speed control with piezoelectric sensor |
USRE33848E (en) * | 1982-09-02 | 1992-03-17 | Nissan Motor Company, Limited | Automatic windshield wiper speed control with piezoelectric sensor |
US4542325A (en) * | 1983-01-28 | 1985-09-17 | Nissan Motor Company, Limited | Rain condition dependent wiper control system for an automotive vehicle |
US4584508A (en) * | 1983-01-28 | 1986-04-22 | Nissan Motor Company, Limited | Rain sensor in an automatic wiper drive control system for an automotive vehicle |
DE3518469B3 (en) * | 1985-05-23 | 2013-12-05 | Diehl Stiftung & Co.Kg | Method for obtaining ignition information and multi-channel detector arrangement for carrying out the method |
DE4034619A1 (en) * | 1990-10-31 | 1992-05-07 | Diehl Gmbh & Co | SPACING EQUIPMENT FOR A STOREY, ESPECIALLY FOR A PANZER DEFENSE FLOOR |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3870894A (en) | Electronic sensor for triggering safety devices during the crash of vehicles | |
US3926120A (en) | Rain impact sensing proximity fuze | |
US4477732A (en) | Sensor for acceleration | |
US3225695A (en) | Pyrotechnic bridge detonating circuit with zener diode circuit controlling switching of scr | |
GB1317977A (en) | Firing of projectile fuses or igniters | |
US4020765A (en) | Light activated fuze | |
US4480550A (en) | Relative velocity sensor for void sensing fuzes and the like | |
GB1453106A (en) | Piezoelectric fuses | |
GB1493104A (en) | Projectile fuses | |
US2894457A (en) | Detonation delay device | |
KR930016291A (en) | Vehicle safety trip device | |
US4799427A (en) | Projectile ignition device | |
GB1503718A (en) | Electronic firing device for projectiles | |
US2892411A (en) | Crystal point detonation fuze | |
US3017832A (en) | Echo firing device for a depth charge | |
GB1500686A (en) | Firing device for an electrical detonator for a mine | |
GB1479411A (en) | Self-destruction type delayed-action fuse for spinning projectiles | |
US4215633A (en) | Acoustic emission contact fuze with signal processing capability | |
US4019440A (en) | Impact discriminating apparatus for missiles and the like, and method for impact discrimination | |
CA1208748A (en) | Impact fuze with flight time-dependent detonation delay | |
EP0434243A2 (en) | Proximity fuzing system | |
GB1450968A (en) | Proximity fuse | |
US3905298A (en) | Electronic proximity fuse incorporating means for preventing premature detonation by electronic counter measures | |
US3786758A (en) | Rain discriminating fast acting impact switch | |
US3747531A (en) | Overriding impact proximity fuze |