JPH0442000U - - Google Patents
Info
- Publication number
- JPH0442000U JPH0442000U JP8203890U JP8203890U JPH0442000U JP H0442000 U JPH0442000 U JP H0442000U JP 8203890 U JP8203890 U JP 8203890U JP 8203890 U JP8203890 U JP 8203890U JP H0442000 U JPH0442000 U JP H0442000U
- Authority
- JP
- Japan
- Prior art keywords
- section
- attached
- propulsion
- control section
- warhead
- 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
- 238000002485 combustion reaction Methods 0.000 claims 1
- 239000003380 propellant Substances 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 3
- 239000003721 gunpowder Substances 0.000 description 1
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Description
第１図はこの考案の一実施例を示す図、第２図
はこの考案の一実施例の動作図、第３図は従来の
誘導飛しよう体の構成図である。図において１は
誘導飛しよう体、２は誘導制御部、３は弾頭部、
４は推進部、５は前翼、６は後翼、７は剥離流、
８は整流板、９は火薬、１０は整流された流れで
ある。なお、各図中同一符号は同一または相当部
分を示す。
FIG. 1 is a diagram showing an embodiment of this invention, FIG. 2 is an operational diagram of an embodiment of this invention, and FIG. 3 is a diagram showing the configuration of a conventional guided flying object. In the figure, 1 is a guided flying object, 2 is a guidance control unit, 3 is a warhead,
4 is a propulsion section, 5 is a front wing, 6 is a rear wing, 7 is a separated flow,
8 is a rectifying plate, 9 is gunpowder, and 10 is a rectified flow. Note that the same reference numerals in each figure indicate the same or corresponding parts.
Claims (1)
操舵翼と、前記誘導制御部後方に取付けられた弾
頭部と、前記弾頭部の後方に取付けられた推進部
と前記推進部に取付けられた後翼を備えている誘
導飛しよう体において、前記推進部の推薬燃焼後
に、整流板を前記推進部の後方より大気中に展開
する機構を具備した事を特徴とする誘導飛しよう
体。 a guidance control section, a steering blade attached to the guidance control section, a warhead attached to the rear of the guidance and control section, a propulsion section attached to the rear of the warhead, and a rear end attached to the propulsion section. A guided flying object equipped with wings, characterized in that the guided flying object is equipped with a mechanism for deploying a baffle plate into the atmosphere from behind the propulsion section after propellant combustion in the propulsion section.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP8203890U JPH0442000U (en) | 1990-08-01 | 1990-08-01 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP8203890U JPH0442000U (en) | 1990-08-01 | 1990-08-01 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0442000U true JPH0442000U (en) | 1992-04-09 |
Family
ID=31628501
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP8203890U Pending JPH0442000U (en) | 1990-08-01 | 1990-08-01 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0442000U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH07136689A (en) * | 1993-11-13 | 1995-05-30 | Nisshoku Corp | Water purification method |
-
1990
- 1990-08-01 JP JP8203890U patent/JPH0442000U/ja active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH07136689A (en) * | 1993-11-13 | 1995-05-30 | Nisshoku Corp | Water purification method |
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