JPS62148898U - - Google Patents
Info
- Publication number
- JPS62148898U JPS62148898U JP3541586U JP3541586U JPS62148898U JP S62148898 U JPS62148898 U JP S62148898U JP 3541586 U JP3541586 U JP 3541586U JP 3541586 U JP3541586 U JP 3541586U JP S62148898 U JPS62148898 U JP S62148898U
- Authority
- JP
- Japan
- Prior art keywords
- bullet
- propellant
- training
- predetermined period
- time
- 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.)
- Granted
Links
- 239000003380 propellant Substances 0.000 claims description 4
- 238000010304 firing Methods 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
- F42B10/48—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding
- F42B10/50—Brake flaps, e.g. inflatable
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
- F42B10/38—Range-increasing arrangements
- F42B10/40—Range-increasing arrangements with combustion of a slow-burning charge, e.g. fumers, base-bleed projectiles
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Description
第1図は訓練弾に対する実弾の一例をこれを飛
ばす薬莢の一例とともに示す図、第2図は本考案
の第一の実施例に係る訓練弾を示す断面図、第3
図はこの訓練弾の薬莢への組付状態を示す断面図
、第4図は訓練弾の作用を示す図、第5図は本考
案の第二の実施例に係る訓練弾を示す断面図、第
6図は内面燃焼型推進薬の別の例を示した断面図
、第7図は従来の訓練弾の一例を示す図である。
1,K1,K2…訓練弾、B…実弾、20,5
0…弾体、30,60…ロケツトモータ(ロケツ
ト推進手段)、31,62,100…推進薬、w
b1,wb2,wb3…ウエツブ、S1,S2…
燃焼面積。
FIG. 1 is a diagram showing an example of a live bullet for a training bullet, along with an example of a cartridge that shoots it, FIG. 2 is a sectional view showing a training bullet according to the first embodiment of the present invention, and FIG.
The figure is a sectional view showing the training bullet assembled into the cartridge case, FIG. 4 is a diagram showing the action of the training bullet, and FIG. 5 is a sectional view showing the training bullet according to the second embodiment of the present invention. FIG. 6 is a sectional view showing another example of an internal combustion propellant, and FIG. 7 is a view showing an example of a conventional training bullet. 1, K1, K2...Training bullet, B...Live bullet, 20,5
0...Bullet body, 30,60...Rocket motor (rocket propulsion means), 31,62,100...Propellant, w
b1, wb2, wb3... web, S1, S2...
Burning area.
Claims (1)
、その後は急減速させるようにした訓練弾におい
て、 実弾に比較して空力抵抗が増加する構成にする
とともに、推進薬によるロケツト推進手段を附設
し、空力抵抗の増加分に相応する推力を発生しか
つ所定時間の経過後には焼失するように推進薬の
薬量及び形状を設定した訓練弾。[Scope of Claim for Utility Model Registration] A training bullet that follows a trajectory similar to that of a live bullet for a predetermined period of time after firing and then rapidly decelerates, with a configuration that increases aerodynamic drag compared to the live bullet, and A training bullet that is equipped with a rocket propulsion means using propellant, and the amount and shape of the propellant are set so that it generates thrust corresponding to the increase in aerodynamic resistance and burns out after a predetermined period of time.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP3541586U JPH045915Y2 (en) | 1986-03-13 | 1986-03-13 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP3541586U JPH045915Y2 (en) | 1986-03-13 | 1986-03-13 |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS62148898U true JPS62148898U (en) | 1987-09-19 |
JPH045915Y2 JPH045915Y2 (en) | 1992-02-19 |
Family
ID=30844884
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP3541586U Expired JPH045915Y2 (en) | 1986-03-13 | 1986-03-13 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH045915Y2 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2006145131A (en) * | 2004-11-22 | 2006-06-08 | Ihi Aerospace Co Ltd | Training projectile for sub projectile loaded type rocket |
-
1986
- 1986-03-13 JP JP3541586U patent/JPH045915Y2/ja not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2006145131A (en) * | 2004-11-22 | 2006-06-08 | Ihi Aerospace Co Ltd | Training projectile for sub projectile loaded type rocket |
JP4521758B2 (en) * | 2004-11-22 | 2010-08-11 | 株式会社Ihiエアロスペース | Training bullets for rocket ammunition |
Also Published As
Publication number | Publication date |
---|---|
JPH045915Y2 (en) | 1992-02-19 |
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