JPH02127994U - - Google Patents
Info
- Publication number
- JPH02127994U JPH02127994U JP3460589U JP3460589U JPH02127994U JP H02127994 U JPH02127994 U JP H02127994U JP 3460589 U JP3460589 U JP 3460589U JP 3460589 U JP3460589 U JP 3460589U JP H02127994 U JPH02127994 U JP H02127994U
- Authority
- JP
- Japan
- Prior art keywords
- circuit
- function
- pyrotechnics
- ignition
- outputs
- 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.)
- Pending
Links
- 238000012790 confirmation Methods 0.000 claims description 6
- 230000008878 coupling Effects 0.000 claims 3
- 238000010168 coupling process Methods 0.000 claims 3
- 238000005859 coupling reaction Methods 0.000 claims 3
- 239000004020 conductor Substances 0.000 claims 2
- 230000001934 delay Effects 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 2
- WABPQHHGFIMREM-UHFFFAOYSA-N lead(0) Chemical compound [Pb] WABPQHHGFIMREM-UHFFFAOYSA-N 0.000 description 1
Landscapes
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Description
第１図はこの考案の一実施例を示す点火装置の
構成図、第２図は従来の点火装置を示す構成図で
ある。
図において、１は誘導弾機能確認回路、２は発
射機機能確認回路、３は論理積回路、４は発射指
令回路、５は論理積回路、６は誘導制御部火工品
点火回路、７は遅延回路、８はロケツトモータ点
火回路、９はコネクタ結合確認導線、１０は論理
積回路である。なお、図中、同一符号は同一また
は相当部分を示す。
FIG. 1 is a block diagram of an ignition system showing an embodiment of this invention, and FIG. 2 is a block diagram showing a conventional ignition system. In the figure, 1 is a guided missile function confirmation circuit, 2 is a launcher function confirmation circuit, 3 is an AND circuit, 4 is a launch command circuit, 5 is an AND circuit, 6 is a guidance control section pyrotechnics ignition circuit, and 7 is a 8 is a delay circuit, 8 is a rocket motor ignition circuit, 9 is a connector connection confirmation lead wire, and 10 is an AND circuit. In addition, in the figures, the same reference numerals indicate the same or corresponding parts.
Claims (1)
、発射機の機能を確認する発射機能確認回路と、
二つの機能確認回路の出力に設けられる論理積回
路と、発射指令を出力する発射指令回路と、上記
、論理積回路と発射指令回路の出力に設けられる
論理積回路と、この論理積回路の出力信号により
誘導弾の誘導制御部火工品を活性化させる誘導制
御部火工品点火回路と、この火工品が点火された
後に火工品点火回路より出力されるミサイル確認
信号を遅延させる遅延回路と、遅延回路の信号に
よりロケツトモータを点火させるロケツトモータ
点火回路と、ロケツトモータのコネクタの結合を
確認するコネクタ結合導線と、コネクタ結合確認
導線と上記、発射指令回路の出力に設けられる論
理積回路を備えた点火装置。 A guided missile function check circuit that checks the function of the guided missile, a launch function check circuit that checks the function of the launcher,
An AND circuit provided at the outputs of the two function confirmation circuits, a launch command circuit that outputs a launch command, an AND circuit provided at the outputs of the AND circuit and the launch command circuit, and the output of this AND circuit. A guidance control unit pyrotechnic ignition circuit that activates the guidance control unit pyrotechnics of a guided missile by a signal, and a delay that delays the missile confirmation signal output from the pyrotechnics ignition circuit after the pyrotechnics are ignited. a rocket motor ignition circuit that ignites the rocket motor with a signal from a delay circuit, a connector coupling conductor that confirms the coupling of the rocket motor connector, a logical product provided between the connector coupling confirmation conductor and the output of the above launch command circuit. Ignition device with circuit.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3460589U JPH02127994U (en) | 1989-03-27 | 1989-03-27 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3460589U JPH02127994U (en) | 1989-03-27 | 1989-03-27 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH02127994U true JPH02127994U (en) | 1990-10-22 |
Family
ID=31539226
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP3460589U Pending JPH02127994U (en) | 1989-03-27 | 1989-03-27 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH02127994U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104895700A (en) * | 2015-04-15 | 2015-09-09 | 北京航天自动控制研究所 | Low delay ignition confirmation system and confirmation method applied to rocket ground information fusion |
-
1989
- 1989-03-27 JP JP3460589U patent/JPH02127994U/ja active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104895700A (en) * | 2015-04-15 | 2015-09-09 | 北京航天自动控制研究所 | Low delay ignition confirmation system and confirmation method applied to rocket ground information fusion |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| DE3684185D1 (en) | ZENDER. | |
| CA2242237A1 (en) | Detonators having multiple-line input leads | |
| SE8703157L (en) | LIGHTING SYSTEM AND WAY TO INITIATE THE SAME | |
| US4183302A (en) | Sequential burst system | |
| US3973499A (en) | Safe rocket motor igniter using sequenced initiation to an explosive logic network | |
| JPH02127994U (en) | ||
| SE9202149D0 (en) | ELECTRONIC CONTROL SYSTEM FOR BLASTING CHARGES | |
| SE8304814D0 (en) | TENDROR | |
| SE7714509L (en) | CONNECTING DEVICE BETWEEN THE STEP IN A SELF-POWERED MISSILE | |
| SE8403738D0 (en) | AMMUNITION UNIT | |
| US3855934A (en) | Blind mating connector for missile sections | |
| EP0318996A3 (en) | Pyrotechnical initiator for projectiles, rockets, bomblets and mines | |
| RU96120588A (en) | ANTI-AREA MANAGED ANTI-UTILIZED ROCKET | |
| WO1999006276A3 (en) | Rocket launching system employing thermal-acoustic detection for rocket ignition | |
| JPH0167500U (en) | ||
| JPS63121300U (en) | ||
| JPS6196199U (en) | ||
| JPS6139300U (en) | detonator | |
| JPS60170600U (en) | proximity fuse | |
| JPH0216158Y2 (en) | ||
| JPS6032699U (en) | Let's fly | |
| JPS6118399U (en) | guided missile | |
| JPH01123100U (en) | ||
| JPH0717991Y2 (en) | Minefield processing equipment | |
| JPH03121400U (en) |