JPS6149600B2 - - Google Patents
Info
- Publication number
- JPS6149600B2 JPS6149600B2 JP56142566A JP14256681A JPS6149600B2 JP S6149600 B2 JPS6149600 B2 JP S6149600B2 JP 56142566 A JP56142566 A JP 56142566A JP 14256681 A JP14256681 A JP 14256681A JP S6149600 B2 JPS6149600 B2 JP S6149600B2
- Authority
- JP
- Japan
- Prior art keywords
- projectile
- armor
- piercing
- stabilizing
- bullet
- 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
Links
- 230000000087 stabilizing effect Effects 0.000 claims description 24
- 238000005476 soldering Methods 0.000 claims description 6
- 230000000717 retained effect Effects 0.000 claims description 2
- 239000000853 adhesive Substances 0.000 claims 1
- 230000001070 adhesive effect Effects 0.000 claims 1
- 230000035515 penetration Effects 0.000 description 7
- 238000004026 adhesive bonding Methods 0.000 description 5
- 230000001133 acceleration Effects 0.000 description 4
- 229910052782 aluminium Inorganic materials 0.000 description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 238000010304 firing Methods 0.000 description 4
- 230000000149 penetrating effect Effects 0.000 description 3
- 239000003381 stabilizer Substances 0.000 description 2
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- 239000010937 tungsten Substances 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000008034 disappearance Effects 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 229910001385 heavy metal Inorganic materials 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 230000002940 repellent Effects 0.000 description 1
- 239000005871 repellent Substances 0.000 description 1
- 230000001846 repelling effect Effects 0.000 description 1
- 239000010959 steel Substances 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
- F42B10/02—Stabilising arrangements
- F42B10/04—Stabilising arrangements using fixed fins
- F42B10/06—Tail fins
-
- 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
- F42B10/02—Stabilising arrangements
- F42B10/04—Stabilising arrangements using fixed fins
- F42B10/06—Tail fins
- F42B10/08—Flechette-type 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)
- Powder Metallurgy (AREA)
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は安定翼付きの高性能弾、すなわち、徹
甲弾（あるいは破甲弾）に関する。本発明は、さ
らに詳しく述べると、長さ／直径の比が大きくか
つ密度が高い、弾体の後部を安定翼の支持部とし
て構成してなる安定翼付きの徹甲弾に関する。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a high-performance projectile with stabilized wings, that is, an armor-piercing projectile (or armor-piercing projectile). More specifically, the present invention relates to an armor-piercing bullet with stable wings, which has a large length/diameter ratio and high density, and in which the rear part of the bullet serves as a support for the stabilizing wings.
上記したタイプの砲弾は米国特許第4098194号
明細書から公知である。この公知砲弾は、アルミ
ニウム製円筒体の内部にタングステン鋼から成る
弾心部を具備し、前記円筒体にはサーボ（弾体）
を軸線方向に着脱自在に係合するための溝が形成
されている。砲弾の後部は安定翼の支持部として
構成されている。
A shell of the type mentioned above is known from US Pat. No. 4,098,194. This known shell has a bullet core made of tungsten steel inside an aluminum cylinder, and the cylinder has a servo (bullet).
A groove is formed for removably engaging in the axial direction. The rear part of the shell is configured as a support for the stabilizing wing.
上記の砲弾では、しかし、アルミニウム円筒体
が係合手段を形成するから、そのアルミニウム円
筒にかなりの壁厚が必要となり、したがつて、ア
ルミニウムの占める割合が大きくなり、その分だ
け全体としての密度が低くなるという欠点があつ
た。 In the above-mentioned shell, however, since the aluminum cylinder forms the engagement means, the aluminum cylinder must have a considerable wall thickness, and therefore the proportion of aluminum becomes large, correspondingly increasing the overall density. The disadvantage was that the value was low.
上記米国特許の欠点を解消してできるだけ高い
密度を得るため、徹甲弾の材料として好ましくは
タングステンをベースとする重金属焼結合金を利
用する方法が提案された。しかし、この種の砲弾
は、それを多目的用として使用した場合にできる
だけ高い貫徹力を発揮させるため、標的の補助装
甲板を貫通した後もその背後に位置する主装甲板
に命中するではなおできるだけ大きい波壊質量
を、従つてできるだけ大きい運動エネルギーを維
持していなければならない。 In order to overcome the drawbacks of the above-mentioned US patent and to obtain as high a density as possible, it has been proposed to use a heavy metal sintered alloy, preferably based on tungsten, as the material for the armor-piercing projectile. However, in order to achieve the highest possible penetration power when used for multi-purpose use, this type of shell should not be able to hit the main armor plate located behind it even after penetrating the target's auxiliary armor plate. A large wave breaking mass and therefore as high a kinetic energy as possible must be maintained.
本発明の目的は、安定翼の支持部として構全さ
れた徹甲弾後部の質量をも補助装甲板貫通後にな
おも必要とされる主装甲板貫徹力に利用し得るよ
うな徹甲弾を提供することにある。
The object of the present invention is to develop an armor-piercing projectile capable of utilizing the mass of the rear part of the armor-piercing projectile, which is constructed as a support part of the stabilizing wing, for the main armor plate penetration force that is still required after penetrating the auxiliary armor plate. It is about providing.
上記した目的は、本発明によれば、長さ／直径
の比が大きくかつ密度が高い、弾体の後部を安定
翼の支持部として構成してなる安定翼付き徹甲弾
であつて、
前記支持部が弾体の後部の円周領域を含み、こ
の円周領域において前記支持部と前記安定翼とが
一時的取り付け手段によつて一緒に固定されてお
り、したがつて、前記弾体が標的に命中するま
で、前記安定翼が前記弾体上に十分に保持されて
いることを特徴とする安定翼付き徹甲弾によつて
達成することができる。
The above-mentioned object is, according to the present invention, an armor-piercing projectile with stable wings, which has a large length/diameter ratio and high density, and in which the rear part of the projectile body is configured as a supporting part of the stabilizing wing. A support includes a circumferential region at the rear of the projectile body, in which the support and the stabilizing wing are secured together by temporary attachment means, so that the projectile body This can be achieved by an armor-piercing bullet with stabilized wings, characterized in that the stabilized wings are sufficiently retained on the projectile until it hits the target.
本発明の徹甲弾は、好ましい１態様によれば、
安定翼のひれが弾体の後部の外径に相当する内径
をもつた円筒形スリーブ上に取り付けられてお
り、そして前記スリーブが前記円周領域に固定さ
れている。 According to a preferred embodiment, the armor-piercing bullet of the present invention includes:
The stabilizing wing fin is mounted on a cylindrical sleeve with an inner diameter corresponding to the outer diameter of the rear part of the projectile, and said sleeve is fixed to said circumferential region.
別の好ましい態様によると、支持部の円周領域
に前記ひれのそれぞれに対応する溝が設けられて
おり、そして前記ひれの一部が前記溝内に固定さ
れている。また、前記溝の面は、弾体の長手方向
の軸線に関して傾斜しており、そしてそれに対応
するひれの対向面を支持するように機能してい
る。また、前記溝の傾斜面は、好ましくは、それ
に対応するひれの対向面に対する反撥面として作
用している。 According to another preferred embodiment, a groove corresponding to each of the fins is provided in the circumferential area of the support, and a part of the fin is fixed in the groove. Furthermore, the surfaces of the grooves are inclined with respect to the longitudinal axis of the bullet and function to support the corresponding opposing surfaces of the fins. Furthermore, the inclined surface of the groove preferably acts as a repelling surface against the corresponding opposing surface of the fin.
安定翼の支持部への固定は、好ましくは、はん
だ付けによつて行なわれているかもしくは接着に
よつて行なわれている。 The stabilizing wing is preferably fastened to the support by soldering or gluing.
本発明により二重の効果が達成される。即ち、
安定翼のみが徹甲弾から離脱するから、従来支持
部としての徹甲弾部分がちぎれることに原因して
発生した質量損失が防止されるだけでなく、貫徹
時、徹甲弾と結合したままの状態の安定翼が標的
貫徹孔を無用に広げたことに原因して起こつた速
度損失もまた防止される。総合的に評価して、本
発明によれば、従来の安定翼付き徹甲弾に比較し
て15％までの範囲で性能アツプを実現することが
できる。
A dual effect is achieved by the invention. That is,
Since only the stabilizing wing detaches from the armor-piercing projectile, it not only prevents the loss of mass that would normally occur when the armor-piercing projectile part, which served as a supporting part, breaks off, but also remains attached to the armor-piercing projectile during penetration. Velocity losses caused by the stabilizing wing in the condition unnecessarily widening the target penetration hole are also prevented. Comprehensive evaluation shows that according to the present invention, performance can be increased by up to 15% compared to conventional armor-piercing bullets with stabilized wings.
以下、添付図面に略示した４つの実施例を参照
しながら本発明の構成、そして作用効果をさらに
説明する。
Hereinafter, the configuration and effects of the present invention will be further explained with reference to four embodiments schematically illustrated in the accompanying drawings.
第１図に示す本発明の実施例では、徹甲弾１
は、円周領域８及び後端面９を有する断面が円形
の後部６を有している。後部６は安定翼１０の支
持部として形成されている。半径方向に外方に延
在しかつ長手方向の軸線Ａに平行な安定翼１０の
ひれ１２は、薄い円筒形スリーブ１４に一体的に
結合せしめられている。スリーブ１４の内径は後
部６の外径に符合するから、その後部の円周領域
８にはんだ付けまたは接着によつてスリーブ１４
を固定することができる。なお、スリーブ１４と
円周領域８との固定部分の機械的強度は、高速飛
翔条件だけでなく、それよりもむしろ主として発
射時の加速度に耐えることを考慮して設定され
る。通常、発射時の加速度は標的に命中した場合
の制動効果よりもはるかに小さいから、徹甲弾１
が標的（図示せず）に命中する時点では極めて大
きい負の加速力の作用で安定翼１０と支持部（後
部６）との結合がゆるめられるかまたは解除され
ており、したがつて、遅くとも、安定翼１０が標
的の装甲板に衝突する瞬間には安定翼１０が支持
部から離脱し、従つて支持部が損傷することはな
い、空気抵抗を少さくしかつできるだけ死重を小
さくするため、安定翼１０構成部分１２及び１４
を極力薄く形成することが好ましい。なお“死
重”なるは、ここでそれを用いた場合、装甲板の
貫徹に関与しない、従つて、使用条件上定められ
た最小値を超えてはならない質量を意味する。安
定翼１０は、それが標的に命中した時には上述の
ように難脱するから、弾体の貫徹能力の妨げとな
る制動作用を有する障害物とはならない。標的命
中時の制動力を充分に考慮しないで安定翼１０を
固定した場合、弾体の後部６の全体がちぎれてし
まうことが多く、貫通に寄与すべき後部６の質量
が失われる結果となる。 In the embodiment of the invention shown in FIG.
has a rear part 6 which is circular in cross-section and has a circumferential area 8 and a rear end face 9 . The rear part 6 is designed as a support for the stabilizing wing 10. The fins 12 of the stabilizer blade 10 extending radially outward and parallel to the longitudinal axis A are integrally connected to a thin cylindrical sleeve 14 . Since the inner diameter of the sleeve 14 corresponds to the outer diameter of the rear part 6, the sleeve 14 is attached to the circumferential area 8 of the rear part by soldering or gluing.
can be fixed. Note that the mechanical strength of the fixed portion between the sleeve 14 and the circumferential region 8 is set in consideration not only of high-speed flight conditions but also of withstanding mainly the acceleration during launch. Normally, the acceleration at the time of firing is much smaller than the braking effect when it hits the target, so armor-piercing bullets
At the time when the blade hits a target (not shown), the connection between the stabilizing wing 10 and the support part (rear part 6) is loosened or released due to the action of an extremely large negative acceleration force, and therefore, at the latest, At the moment when the stabilizing wing 10 collides with the target's armor plate, the stabilizing wing 10 separates from the supporting part, so the supporting part is not damaged. Wing 10 components 12 and 14
It is preferable to form it as thin as possible. As used herein, "dead weight" refers to the mass that does not participate in the penetration of the armor plate and therefore must not exceed the minimum value determined by the conditions of use. Since the stabilizing wing 10 easily escapes as described above when it hits the target, it does not become an obstacle with a braking action that impedes the penetrating ability of the projectile. If the stabilizing wing 10 is fixed without giving sufficient consideration to the braking force upon hitting the target, the entire rear part 6 of the projectile often breaks off, resulting in a loss of mass of the rear part 6 that should contribute to penetration. .
第２図には本発明の第２実施例が示されてい
る。この実施例は、スリーブ１４が後端面９より
も後方へ突出し、よつて曳光剤など24の収容部２
２を形成するように安定翼１０の配置を行なつた
点で第１図の実施例と異なる。 FIG. 2 shows a second embodiment of the invention. In this embodiment, the sleeve 14 protrudes rearward beyond the rear end surface 9, and therefore the housing part 24 for the repellent etc.
This embodiment differs from the embodiment shown in FIG. 1 in that the stabilizing blades 10 are arranged so as to form a wing 2.
第３図に示す本発明の第３実施例では、徹甲弾
１の後部６の円周領域８が個々のひれ１２に対応
した溝４を有している。この溝４は弾体の軸線Ａ
と平行であり、同じく軸線Ａと平行な溝底４′を
有している。ひれ１２は、その境界面１３が溝底
４′と当接し、はんだ付けまたは接着により弾体
後部６の円周領域８に固定されるように溝４に挿
着されている。この場合、ひれ１２は、発射加速
時に発生する力には確実に耐えるが、そのひれ９
２が標的に命中する際には遅くとも弾体から離脱
するように、はんだ付けまたは接着によつて適切
な結合度を設定する。 In a third embodiment of the invention shown in FIG. 3, the circumferential area 8 of the rear part 6 of the armor-piercing projectile 1 has grooves 4 corresponding to the individual fins 12. This groove 4 is the axis line A of the bullet
It has a groove bottom 4' which is also parallel to the axis A. The fin 12 is inserted into the groove 4 in such a way that its boundary surface 13 abuts the groove bottom 4' and is fixed by soldering or gluing to the circumferential area 8 of the rear shell 6. In this case, the fin 12 will certainly withstand the forces generated during launch acceleration, but the fin 9
An appropriate degree of connection is set by soldering or gluing so that the bullet 2 separates from the bullet at the latest when it hits the target.
第４図に示す本発明の第４実施例では、安定翼
１０の各ひれ１２がほぼ三角形の部分１６を有し
ている。これらの部分１６は、はんだ付けまたは
接着によつて固定できるように、弾体後部６の円
周領域８の溝４と対応せしめられている。溝底
は、徹甲弾の長手方向軸線Ａに関して発射方向に
傾斜した面５を有し、また、この傾斜面５に連続
して、同じく徹甲弾の長手方向軸線Ａに関して発
射方向に比較的ゆるやかに、徹甲弾１の周面にむ
かつて上昇する傾斜面７を有している。溝４の面
５，７にひれ１２の一部分１６に於ける面１８，
２０がそれぞれ対応する。溝４の面５が発射時に
ひれ支持機能を果たすのに対し、面７は標的命中
時にひれの反撥面として作用する。詳しくは図示
しないが、ひれ１２は、徹甲弾１の後部６の周面
と対向するそのひれ１２の面１３に亘つて、例え
ば後端面９または位置８１の付近でも、補足的に
徹甲弾１の後部６に固定することができる。 In a fourth embodiment of the invention, shown in FIG. 4, each fin 12 of the stabilizer wing 10 has a generally triangular section 16. These parts 16 are matched with the grooves 4 in the circumferential area 8 of the rear part 6 of the bullet so that they can be fixed by soldering or gluing. The groove bottom has a surface 5 inclined in the firing direction with respect to the longitudinal axis A of the armor-piercing bullet, and, continuous with this inclined surface 5, also relatively in the firing direction with respect to the longitudinal axis A of the armor-piercing bullet. It has an inclined surface 7 that gently rises toward the circumferential surface of the armor-piercing projectile 1. Surfaces 5 and 7 of groove 4 and surface 18 of part 16 of fin 12,
20 correspond to each other. Surface 5 of groove 4 performs a fin support function during firing, whereas surface 7 acts as a repulsion surface for the fin when hitting the target. Although not shown in detail, the fin 12 can also be used for additional armor-piercing bullets over the surface 13 of the fin 12 facing the peripheral surface of the rear part 6 of the armor-piercing bullet 1, for example in the vicinity of the rear end face 9 or position 81. It can be fixed to the rear part 6 of 1.
徹甲弾１が標的に命中すると、溝４の面５がそ
の支持機能を失うから、ひれ１２は慣性に従つて
そのまま矢印Ｓの方向に運動する。固定効果が消
滅した結果、面１８は面５から離脱し、そして面
２０は面７に沿つて高速度で運動を開始する。半
径方向及び軸線方向の運動成分の働きによつてひ
れ１２が後部６から離脱するから、徹甲弾１の後
部６は妨げられることなく装甲板貫徹に寄与する
ことができる。 When the armor-piercing projectile 1 hits the target, the surface 5 of the groove 4 loses its supporting function, and the fin 12 continues to move in the direction of the arrow S according to inertia. As a result of the disappearance of the fixation effect, surface 18 separates from surface 5 and surface 20 begins to move along surface 7 at a high velocity. Since the fins 12 are separated from the rear part 6 by the action of the radial and axial components of motion, the rear part 6 of the armour-piercing projectile 1 can contribute unimpeded to the penetration of the armor plate.
第１図、第２図、第３図及び第４図は、それぞ
れ、本発明の好ましい実施例を示した徹甲弾後部
の断面図である。
図中、１は徹甲弾、６は後部、１０は安定翼、
１２はひれ、そして１４は円筒形スリーブであ
る。
1, 2, 3, and 4 are sectional views of the rear portion of an armor-piercing projectile, respectively, showing preferred embodiments of the present invention. In the diagram, 1 is an armor-piercing bullet, 6 is the rear part, 10 is the stabilizing wing,
12 is a fin, and 14 is a cylindrical sleeve.
Claims (1)
体の後部を安定翼の支持部として構成してなる安
定翼付き徹甲弾であつて、 前記支持部が弾体の後部の円周領域を含み、こ
の円周領域において前記支持部と前記安定翼とが
一時的取り付け手段によつて一緒に固定されてお
り、したがつて、前記弾体が標的に命中するま
で、前記安定翼が前記弾体上に十分に保持されて
いることを特徴とする安定翼付き徹甲弾。 ２ 安定翼のひれが弾体の後部の外径に相当する
内径をもつた円筒形スリーブ上に取り付けられて
おり、そして前記スリーブが前記円周領域に固定
されている。特許請求の範囲第１項に記載の徹甲
弾。 ３ 前記円周領域に前記ひれのそれぞれに対応す
る溝が設けられており、そして前記ひれの一部が
前記溝内に固定されている、特許請求の範囲第１
項に記載の徹甲弾。 ４ 前記溝の面が弾体の長手方向の軸線に関して
傾斜しており、それに対応するひれの対向面を支
持するように機能している、特許請求の範囲第３
項に記載の徹甲弾。 ５ 弾体の長手方向の軸線に関して傾斜して前記
溝の面がそれに対応するひれ対向面に対する反撥
面として作用している、特許請求の範囲第３項又
は第４項に記載の徹甲弾。 ６ 前記安定翼の前記支持部への固定がはんだ付
けによつて行なわれている、特許請求の範囲第１
項〜第５項のいずれか１項に記載の徹甲弾。 ７ 前記安定翼の前記支持部への固定が接着によ
つて行なわれている、特許請求の範囲第１項〜第
５項のいずれか１項に記載の徹甲弾。[Scope of Claims] 1. An armour-piercing projectile with stable wings, which has a large length/diameter ratio and high density, and in which the rear part of the projectile is configured as a support part for a stabilizing wing, wherein the support part is a support part for the projectile. a circumferential region at the rear of the body, in which the support and the stabilizing wing are fixed together by temporary attachment means, so that the projectile hits the target; An armor-piercing projectile with stabilizing wings, characterized in that the stabilizing wings are sufficiently retained on the projectile until the end of the projectile. 2. The stabilizing wing fin is mounted on a cylindrical sleeve with an inner diameter corresponding to the outer diameter of the rear part of the projectile, and said sleeve is fixed in said circumferential area. An armor-piercing bullet according to claim 1. 3. The circumferential region is provided with a groove corresponding to each of the fins, and a portion of the fin is fixed in the groove.
Armor-piercing bullets listed in section. 4. Claim 3, wherein the surface of the groove is inclined with respect to the longitudinal axis of the bullet and functions to support the corresponding opposing surface of the fin.
Armor-piercing bullets listed in section. 5. The armour-piercing bullet according to claim 3 or 4, wherein the groove surface is inclined with respect to the longitudinal axis of the bullet and acts as a repulsion surface for the corresponding fin-facing surface. 6. Claim 1, wherein the stabilizing blade is fixed to the support portion by soldering.
The armor-piercing bullet described in any one of Items 1 to 5. 7. The armor-piercing projectile according to any one of claims 1 to 5, wherein the stabilizing wing is fixed to the support portion by adhesive.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19803038087 DE3038087A1 (en) | 1980-10-09 | 1980-10-09 | ARROW-STABILIZED RIFLE BULLET (PENETRATOR) |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5787598A JPS5787598A (en) | 1982-06-01 |
| JPS6149600B2 true JPS6149600B2 (en) | 1986-10-30 |
Family
ID=6113956
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP56142566A Granted JPS5787598A (en) | 1980-10-09 | 1981-09-11 | High performance |
Country Status (3)
| Country | Link |
|---|---|
| EP (1) | EP0049738B1 (en) |
| JP (1) | JPS5787598A (en) |
| DE (2) | DE3038087A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH01150497U (en) * | 1988-04-06 | 1989-10-18 |
Families Citing this family (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0053658B1 (en) * | 1980-12-02 | 1984-10-31 | Contraves Ag | Radar reflector for an artillery projectile |
| DE3525356C1 (en) * | 1985-07-16 | 1993-07-01 | Deutsch Franz Forsch Inst | Sub-caliber arrow floor |
| DE3525854A1 (en) * | 1985-07-19 | 1989-01-05 | Mauser Werke Oberndorf | WING-STABILIZED ARROW BULLET |
| DE3719768A1 (en) * | 1987-06-13 | 1988-12-22 | Rheinmetall Gmbh | SUB-CALIBRATE WING-STABILIZED SHELL |
| DE3719770A1 (en) * | 1987-06-13 | 1988-12-22 | Rheinmetall Gmbh | SUB-CALIBRATE WING-STABILIZED SHELL |
| DE3843796A1 (en) * | 1988-12-24 | 1990-07-05 | Rheinmetall Gmbh | FLOOR WITH SIDE CONTROL |
| DE3927918A1 (en) * | 1989-08-24 | 1991-02-28 | Rheinmetall Gmbh | Armour piercing projectile guiding fins - lie close to projectile body so that fin tip is inside boundary layer |
| DE3932952A1 (en) * | 1989-10-03 | 1991-04-11 | Rheinmetall Gmbh | BULLET STOCK |
| DE3933442A1 (en) * | 1989-10-06 | 1991-04-18 | Rheinmetall Gmbh | Wing-stabilised impact projectile - with blast-off charge for guide wing system |
| DE19835175B3 (en) * | 1998-08-04 | 2005-12-22 | Rheinmetall Waffe Munition Gmbh | Fin stabilised projectile comprises a body with guide vanes, a detonator, and a separating charge located near the vanes so that vanes are blown off before impact |
| DE19837533C2 (en) * | 1998-08-19 | 2002-11-07 | Rheinmetall W & M Gmbh | Wing-stabilized balancing projectile |
| DE102020120747A1 (en) | 2020-08-06 | 2022-02-10 | Rheinmetall Waffe Munition Gmbh | Penetrator, use of a penetrator and projectile |
| FR3115358B1 (en) * | 2020-10-19 | 2023-11-24 | Nexter Munitions | ARTIFICIAL AND EXPLOSIVE PROJECTILE WITH A STABILIZING FLAT |
| DE102024128734A1 (en) * | 2024-10-04 | 2026-04-09 | Rheinmetall Waffe Munition Gmbh | Guide concept for a penetrator |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE146540C (en) * | ||||
| CH10770A (en) * | 1895-07-05 | 1896-02-15 | Hugo Borchardt | Armored core projectile |
| FR1307270A (en) * | 1961-06-08 | 1962-10-26 | Le Ministre Des Armees Terre D | Tailplane for projectile and method of assembly |
| US4098194A (en) * | 1977-06-01 | 1978-07-04 | The United States Of America As Represented By The Secretary Of The Army | Hypervelocity projectile with aluminum components of high resistance to thermodynamic ablation |
| DE3009775A1 (en) * | 1980-03-14 | 1981-10-01 | Mauser-Werke Oberndorf Gmbh, 7238 Oberndorf | WING-STABILIZED ARROW BULLET |
-
1980
- 1980-10-09 DE DE19803038087 patent/DE3038087A1/en not_active Withdrawn
-
1981
- 1981-07-08 EP EP81105273A patent/EP0049738B1/en not_active Expired
- 1981-07-08 DE DE8181105273T patent/DE3168468D1/en not_active Expired
- 1981-09-11 JP JP56142566A patent/JPS5787598A/en active Granted
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH01150497U (en) * | 1988-04-06 | 1989-10-18 |
Also Published As
| Publication number | Publication date |
|---|---|
| EP0049738A3 (en) | 1982-04-28 |
| EP0049738B1 (en) | 1985-01-23 |
| DE3038087A1 (en) | 1982-05-27 |
| EP0049738A2 (en) | 1982-04-21 |
| JPS5787598A (en) | 1982-06-01 |
| DE3168468D1 (en) | 1985-03-07 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JPS6149600B2 (en) | ||
| JP3065669B2 (en) | Aerodynamically stable bullet system for use against underwater targets. | |
| US6182574B1 (en) | Bullet | |
| CA1124136A (en) | Fin-stabilized projectile assembly | |
| CA1284061C (en) | Hunting ammunition comprising a bullet of increased effectiveness | |
| US3905299A (en) | Discarding sabot projectiles | |
| GB2033556A (en) | Dummy projectile | |
| JPS58148400A (en) | Cannonball | |
| EP0607227A1 (en) | Hunting bullet with reduced environmental lead exposure | |
| US4075946A (en) | Armor piercing projectile | |
| CN109323621A (en) | A projectile stock with responsive closed air loop and split wind resistance surface | |
| JP2015515597A (en) | Missile warhead | |
| US8222583B2 (en) | Drag-stabilized water-entry projectile and cartridge assembly | |
| US4209146A (en) | Device for extensible fin blade on shell or the like | |
| US6389977B1 (en) | Shrouded aerial bomb | |
| US4779536A (en) | Kinetic energy projectile | |
| SK84096A3 (en) | Telescoping arrow-type hunting bullet with a sub-projectile combined with a launching element | |
| US4939997A (en) | Article of ammunition | |
| IL104875A (en) | Subcaliber impact projectile | |
| US1833127A (en) | Projectile for small arms | |
| US4242964A (en) | Explosive fuse for projectile | |
| US4481886A (en) | Hollow charge | |
| US4237788A (en) | Explosive fuse for ballistic projectile | |
| US5092246A (en) | Small arms ammunition | |
| US20110259231A1 (en) | Drag Effect Trajectory Enhanced Projectile |