EP0763706B1 - Tandem warhead with secondary projectile - Google Patents
Tandem warhead with secondary projectile Download PDFInfo
- Publication number
- EP0763706B1 EP0763706B1 EP96114076A EP96114076A EP0763706B1 EP 0763706 B1 EP0763706 B1 EP 0763706B1 EP 96114076 A EP96114076 A EP 96114076A EP 96114076 A EP96114076 A EP 96114076A EP 0763706 B1 EP0763706 B1 EP 0763706B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- secondary projectile
- tandem warhead
- protection
- tubular section
- fumes
- 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
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/04—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
- F42B12/10—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge
- F42B12/16—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge in combination with an additional projectile or charge, acting successively on the target
Definitions
- the invention relates to a tandem warhead with a secondary floor as known from DE-C-3 544 528 (see the preamble of Claim 1)
- a tapered vapor protection deflecting fragments of detonation is from the DE-C-3 544 528 known. In a tandem charging system, this covers a guide tube mouth for a margin load. Between the steam protection and an annular gap is provided for the additional charge. This does largely penetration of friction-increasing particles is achieved, but not prevents explosive swaths between the guide tube and the additional charge reach.
- the invention has for its object a reliable arrangement of a Propose secondary floor in a tandem warhead.
- Secondary storey designed as a frag grenade with detonator. This means that Danger of explosive swaths breaking open the back of the secondary floor and lead to irreversible damage to the secondary floor.
- the invention solves this problem according to the characterizing features of claim 1.
- the secondary storey is positively and non-positively connected via a threaded connection a tube piece of the tandem warhead designed as a holding tube.
- a steam protection secures the secondary storey directly at the threaded connection.
- the steam protection in the ring space narrowing backwards compressed into it, thereby achieving the actual sealing effect.
- a second phase takes place simultaneously with a feed movement of the secondary floor due to its inertia, breaking open one with the pipe section integrally connected cone section of the housing of the tandem warhead. This leads to a break in the threaded connection, so that Secondary storey due to its inertia its free flight phase until Arrival in a crater of a bullet channel caused by the shaped charge.
- the fastening parts and the steam protection are simple and inexpensive producible. The functional safety of these parts is also available.
- FIG. 1 is a secondary floor 1 in a pipe section 2 of a housing 3 of a tandem warhead 4 mounted and with a threaded connection 5 with connected to the housing 3.
- a steam protection is designated 6.
- the front part of the tandem warhead 4 has a detonator 7 and a shaped charge 8 with an igniter 9.
- the secondary floor 1 consists of two, screwed together via a thread 35 Housing parts 10, 11. On the housing parts 10, 11 there are ogives 44, 45 intended. Both ogives 44, 45 have a splinter charge 23, 24. The fragments 23, 24 are by sleeves 67, 68 against, consisting of explosives Active charges 13, 14 covered. An igniter 20 separates the two active charges 13, 14 from each other.
- the housing 3 has a conical section 87 with the part arranged thereon cylindrical pipe section 2.
- This pipe section 2 is a floor 88 with a recess 89 corresponding to the ogive 46 via a threaded connection 90 screwed.
- the ogive 46 is therefore in contact with a very large area on the floor 88.
- the threaded connection 5 sets so-called counter lock. It guarantees the during transport secure attachment of the secondary storey 1 in the tandem warhead 4.
- the threaded connection 5 between the pipe section 2 and the secondary floor 1 is secured against loosening in a conventional manner, for example by a security lacquer.
- the steam protection 6 is wedge-shaped in the direction of the shaped charge 8.
- an end face 91 lies at an acute angle 102 to the main axis 92 of the Tandem warhead 4.
- the rear surfaces 93, 94 lie on a conical surface 95 and on a bottom surface 96 lying at right angles to the main axis 92 on.
- This angle 102 extends between 30 ° and 50 °, preferably 45 °, as drawn.
- the steam protection 6 lies in a wedge-shaped bottom that shrinks on the bottom Annulus 101 through the conical section 87 of the housing 3 and the secondary floor 1 is formed.
- the inner contour of the vapor protection 6 is composed of one on the secondary floor 1 adjacent sealing lip 97 and also a ring-shaped Support surface 98.
- the thread 86 of the threaded connection 5 lies at the beginning of the pipe section 2. This is followed by a free annular space 99 in the direction of the bottom 88. This Annular space 99 is delimited in the rear part by floor 88. The gap 100 of the annular space 99 is on average one to two millimeters. The length of the Annular space 99 is approximately one third of the length of the secondary storey 1.
- the vapor protection 6 When viewed in a stretched manner over time, the vapor protection 6 is compressed due to the high pressure of the explosive vapor within the still existing housing 3, so that the explosive vapor cannot reach the floor 88 through the threaded connection.
- the sealing lip 97 is pressed on the secondary floor 4 in the corresponding direction on the circumference.
- the vapor protection 6 naturally does not keep off the explosive vapor in the long term, but only in the crucial microsecond range. In this time range, the conical end face 91 guides the pressure maximum slightly outwards, that is to say away from the threaded connection 5.
- the housing 3 breaks together with the threaded connection 5, the secondary storey 1 already being in a forward movement due to its inertia. Due to the opening of the housing 3, there is a pressure relief with respect to the secondary storey 1, so that there is no longer a risk of the secondary storey 1 being broken open due to the explosive vapor.
- the pipe section 2 remains stable due to the vapor protection, i. that is, he will not destroyed by the detonation swaths. This takes place during the forward movement of the secondary storey 1 is stabilized due to the annular space 99 of the secondary floor 1. This ensures that the secondary floor 1 receives a certain guidance in order to carry out a stable free flight phase to be able to do so until it hits the crater of the bullet canal.
- the steam protection consists of an elastic, compressible art material. PVC and also PP, PA, PE, POM or PTFE are suitable for this.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Buildings Adapted To Withstand Abnormal External Influences (AREA)
- Radar Systems Or Details Thereof (AREA)
Description
Die Erfindung bezieht sich auf einen Tandemgefechtskopf mit einem Sekundärgeschoß wie aus DE-C-3 544 528 bekannt (siehe den Oberbegriff des Anspruchs 1)The invention relates to a tandem warhead with a secondary floor as known from DE-C-3 544 528 (see the preamble of Claim 1)
Bei einem Tandemgefechtskopf mit einem Sekundärgeschoß entsprechend der US-A1-4,803,928 ist eine kopfseitige Hohlladung über abscherbare Schrauben in einer Rohrhülse gehalten, wobei diese Rohrhülse mit einem Abschußrohr für ein abschießbares Sekundärgeschoß verschraubt ist. Das Sekundärgeschoß ist bodenseitig mit einer Treibladungshülse abscherbar verstiftet. Ein spezieller Schwadenschutz zum Schutz der Sekundärladung ist nicht vorgesehen. Die Ursache dafür liegt darin, daß die Anzündung der Hohlladung bzw. Bohrladung durch das, sich in Bewegung befindende Sekundärgeschoß eingeleitet wird. Und außerdem das Sekundärgeschoß im Bereich seines Zünders eine sehr große Wanddicke aufweist.In a tandem warhead with a secondary floor according to US-A1-4,803,928 is a hollow charge at the head using shearable screws in one Tube sleeve held, this tube sleeve with a launch tube for a shootable Secondary floor is screwed. The secondary floor is on the floor side pinned with a propellant charge shearable. A special steam protection to protect the secondary charge is not provided. The cause of that is that the ignition of the shaped charge or drilling charge by the, in Moving secondary floor is initiated. And also the secondary floor has a very large wall thickness in the area of its detonator.
Anders sieht es bei einem Gefechtskopf nach der FR-A1 1.002.092 aus. Bei dem in Figur 1 dargestellten Geschoß ist eine kopfseitige Hohlladung durch einen Schwadenschutz gegenüber einem nachfolgenden Wuchtgeschoß getrennt. Der Schwadenschutz ist als etwa kalibergroße Scheibe ausgebildet und sitzt auf der Geschoßogive des Wuchtgeschosses auf. Damit soll die Ogive des Wuchtgeschosses geschützt werden, während die Hohlladung einen Durchschußkanal im Ziel erzeugt. Der Werkstoff des Schwadenschutzes ist nicht angegeben.The situation is different for a warhead according to FR-A1 1.002.092. At the in Figure 1 shown floor is a hollow charge on the head side by a vapor protection separated from a subsequent balancing projectile. The steam protection is designed as an approximately caliber-sized disc and sits on the floor arch of the balancing bullet. This is to protect the ogive of the balancing bullet while the shaped charge creates a bullet channel in the target. The material of the steam protection is not specified.
Ein kegeliger, Detonationsfragmente ablenkender Schwadenschutz ist aus der DE-C-3 544 528 bekannt. Dieser deckt bei einem Tandemladungssystem eine Führungsrohrmündung für eine Nachschußladung ab. Zwischen dem Schwadenschutz und der Nachschußladung ist ein Ringspalt vorgesehen. Dadurch wird zwar weitgehend ein Eindringen von reibungserhöhenden Partikeln erreicht, jedoch nicht verhindert, daß Sprengstoffschwaden zwischen Führungsrohr und Nachschußladung gelangen. A tapered vapor protection deflecting fragments of detonation is from the DE-C-3 544 528 known. In a tandem charging system, this covers a guide tube mouth for a margin load. Between the steam protection and an annular gap is provided for the additional charge. This does largely penetration of friction-increasing particles is achieved, but not prevents explosive swaths between the guide tube and the additional charge reach.
Der Erfindung liegt die Aufgabe zugrunde, eine funktionssichere Anordnung eines Sekundärgeschosses in einem Tandemgefechtskopf vorzuschlagen. Hierbei ist das Sekundärgeschoß als Splittergranate mit Zünder ausgebildet. Dadurch besteht die Gefahr, daß Sprengstoffschwaden die Rückseite des Sekundärgeschosses aufbrechen und zu einer irreversiblen Beschädigung des Sekundärgeschosses führen. The invention has for its object a reliable arrangement of a Propose secondary floor in a tandem warhead. Here is that Secondary storey designed as a frag grenade with detonator. This means that Danger of explosive swaths breaking open the back of the secondary floor and lead to irreversible damage to the secondary floor.
Die Erfindung löst diese Aufgabe entsprechend den kennzeichnenden Merkmalen
des Anspruches 1.The invention solves this problem according to the characterizing features
of
Vorteilhafte Weiterbildungen der Erfindung sind den Unteransprüchen zu entnehmen.Advantageous developments of the invention can be found in the subclaims.
Das Sekundärgeschoß ist über eine Gewindeverbindung form- und kraftschlüssig in einem, als Halterohr ausgebildeten Rohrstück des Tandemgefechtskopfes gehalten. Ein Schwadenschutz sichert das Sekundärgeschoß unmittelbar an der Gewindeverbindung. Bei auftretenden Detonationsschwaden der bereits gezündeten Hohlladung wird der Schwadenschutz in den sich nach rückwärts verengenden Ringraum hinein komprimiert und dadurch die eigentliche Dichtwirkung erzielt. In einer zweiten Phase erfolgt gleichzeitig mit einer Vorschubbewegung des Sekundärgeschosses aufgrund seiner Massenträgheit das Aufbrechen eines, mit dem Rohrabschnitt einstückig verbundenen Konusabschnittes des Gehäuses des Tandemgefechtskopfes. Dies führt zu einem Aufbrechen der Gewindeverbindung, so daß das Sekundärgeschoß aufgrund seiner Massenträgheit seine Freiflugphase bis zum Eintreffen in einen, von der Hohlladung bewirkten Krater eines Durchschußkanales.The secondary storey is positively and non-positively connected via a threaded connection a tube piece of the tandem warhead designed as a holding tube. A steam protection secures the secondary storey directly at the threaded connection. In the event of detonation swaths of the already ignited shaped charge the steam protection in the ring space narrowing backwards compressed into it, thereby achieving the actual sealing effect. In a second phase takes place simultaneously with a feed movement of the secondary floor due to its inertia, breaking open one with the pipe section integrally connected cone section of the housing of the tandem warhead. This leads to a break in the threaded connection, so that Secondary storey due to its inertia its free flight phase until Arrival in a crater of a bullet channel caused by the shaped charge.
Die Befestigungsteile und der Schwadenschutz sind einfach und kostengünstig herstellbar. Die Funktionssicherheit dieser Teile liegt ebenfalls vor.The fastening parts and the steam protection are simple and inexpensive producible. The functional safety of these parts is also available.
Ein Ausführungsbeispiel der Erfindung ist in der Zeichnung dargestellt. Es zeigt:
- Fig. 1
- einen Tandemgefechtskopf mit einem Sekundärgeschoß im Teilschnitt und
- Fig. 2
- das Sekundärgeschoß nach Fig. 1 im Schnitt sowie die benachbarten Gehäuseteile.
- Fig. 1
- a tandem warhead with a secondary floor in partial section and
- Fig. 2
- 1 in section and the adjacent housing parts.
Nach Figur 1 ist eine Sekundärgeschoß 1 in einem Rohrabschnitt 2 eines Gehäuses
3 eines Tandemgefechtskopfes 4 gelagert und über eine Gewindeverbindung 5 mit
dem Gehäuse 3 verbunden. Ein Schwadenschutz ist mit 6 bezeichnet.According to Figure 1 is a
Der vordere Teil des Tandemgefechtskopfes 4 weist einen Abstandszünder 7 und
eine Hohlladung 8 mit einem Zünder 9 auf. The front part of the tandem warhead 4 has a
Das Sekundärgeschoß 1 besteht aus zwei, über ein Gewinde 35 miteinander verschraubten
Gehäuseteilen 10, 11. An den Gehäuseteilen 10, 11 sind Ogiven 44, 45
vorgesehen. Beide Ogiven 44, 45 weisen eine Splitterladung 23, 24 auf. Die Splitterladungen
23, 24 sind durch Hüllen 67, 68 gegen, aus Sprengstoff bestehenden
Wirkladungen 13, 14 abgedeckt. Ein Zünder 20 trennt die beiden Wirkladungen
13, 14 voneinander.The
Das, gegenüber der Hohlladung 8 im Kaliber kleinere Sekundärgeschoß 1 besitzt
an seinem Umfang ein Gewinde 85 und dazu entsprechend der Rohrabschnitt 2 ein
Innengewinde 86.That, compared to the
Das Gehäuse 3 weist einen konischen Abschnitt 87 mit dem daran einstückig angeordneten
zylindrisch Rohrabschnitt 2 auf. Mit diesem Rohrabschnitt 2 ist ein Boden
88 mit einer der Ogive 46 entsprechenden Ausnehmung 89 über eine Gewindeverbindung
90 verschraubt. Die Ogive 46 liegt also mit einem sehr großen Flächenkontakt
an dem Boden 88 auf. Demzufolge stellt die Gewindeverbindung 5 eine
sogenannte Kontersicherung dar. Sie gewährleistet während des Transports die
sichere Befestigung des Sekundärgeschosses 1 im Tandemgefechtskopf4.The housing 3 has a
Die Gewindeverbindung 5 zwischen dem Rohrabschnitt 2 und dem Sekundärgeschoß
1 ist in herkömmlicher Weise gegen Lösen gesichert, beispielsweise durch
einen Sicherungslack.The threaded
Der Schwadenschutz 6 ist in Richtung auf die Hohlladung 8 keilförmig ausgebildet.
Hierzu liegt eine Stirnfläche 91 in einem spitzen Winkel 102 zur Hauptachse 92 des
Tandemgefechtskopfes 4. Die rückwärtigen Flächen 93, 94 liegen an einer Konusfläche
95 und an einer rechtwinklig zur Hauptachse 92 liegenden Bodenfläche 96
an. Dieser Winkel 102 erstreckt sich zwischen 30° und 50°, vorzugsweise 45°, wie
gezeichnet.The
Der Schwadenschutz 6 liegt in einem keilförmigen bodenseitig sich verkleinernden
Ringraum 101, der durch den konischen Abschnitt 87 des Gehäuses 3 und das Sekundärgeschoß
1 gebildet ist. The
Die Innenkontur des Schwadenschutzes 6 setzt sich zusammen aus einer, am Sekundärgeschoß
1 anliegenden Dichtlippe 97 und aus einer ebenfalls ringförmigen
Stützfläche 98.The inner contour of the
Das Gewinde 86 der Gewindeverbindung 5 liegt zu Beginn des Rohrabschnittes 2.
Daran schließt sich in Richtung auf den Boden 88 ein freier Ringraum 99 an. Dieser
Ringraum 99 ist im rückwärtigen Teil durch den Boden 88 begrenzt. Der Spalt
100 des Ringraumes 99 beträgt im Mittel ein bis zwei Millimeter. Die Länge des
Ringraumes 99 beträgt etwa ein Drittel der Länge des Sekundärgeschosses 1.The
Bei Aufschlag des Tandemgefechtskopfes 4 auf eine nicht dargestellte, feindliche
Deckung wird durch die Hohlladung 8 eine Krater mit anschließendem Durchschußkanal
in der Deckung erzeugt. Bei Detonation der Hohlladung 8 beeinflussen
die rückwärtigen Sprengstoffschwaden sowohl den Schwadenschutz 6 als auch das
Gehäuse 3.Upon impact of the tandem warhead 4 on a hostile, not shown
Coverage is through the
Bei zeitlich gestreckter Betrachtungsweise wird der Schwadenschutz 6 aufgrund
des hohen Druckes der Sprengstoffschwaden innerhalb des noch bestehenden Gehäuses
3 komprimiert, so daß die Sprengstoffschwaden nicht durch die Gewindeverbindung
zum Boden 88 gelangen können. Hierbei wird die Dichtlippe 97 in entsprechender
Richtung umfangsseitig auf das Sekundärgeschoß 4 gepreßt. Auch
liegt ein erhöhter Anpreßdruck des Schwadenschutzes 6 an den Flächen 95, 96 und
am Gewinde 85 vor. Der Schwadenschutz 6 hält die Sprengstoffschwaden natürlich
nicht auf Dauer ab, sondern nur im entscheidenden Mikrosekunden-Bereich. In
diesem Zeitbereich lenkt die konische Stirnfläche 91 das Druckmaximum geringfügig
nach außen, also weg von der Gewindeverbindung 5.
In einer zweiten Phase bricht das Gehäuse 3 zusammen mit der Gewindeverbindung
5, wobei sich das Sekundärgeschoß 1 aufgrund seiner Massenträgheit bereits
in einer Vorwärtsbewegung befindet. Aufgrund des aufbrechenden Gehäuses 3
liegt eine Druckentlastung bezüglich des Sekundärgeschosses 1 vor, so daß eine
Gefahr des Aufbrechens des Sekundärgeschosses 1 aufgrund der Sprengstoffschwaden
nicht mehr besteht.When viewed in a stretched manner over time, the
In a second phase, the housing 3 breaks together with the threaded
Der Rohrabschnitt 2 bleibt aufgrund des Schwadenschutzes stabil, d. h., er wird
durch die Detonationsschwaden nicht zerstört. Damit erfolgt bei der Vorwärtsbewegung
des Sekundärgeschosses 1 aufgrund des Ringraumes 99 eine Lagestabilisierung
des Sekundärgeschosses 1. Dadurch ist gewährleistet, daß das Sekundärgeschoß
1 eine gewisse Führung erhält um eine stabile freie Flugphase durchführen
zu können und zwar bis zum Auftreffen in den Krater des Durchschußkanales.The
Der Schwadenschutz besteht aus einem elastischen, also komprimierbaren Kunst stoff. Es eignen sich hierfür PVC und auch PP, PA, PE, POM oder PTFE.The steam protection consists of an elastic, compressible art material. PVC and also PP, PA, PE, POM or PTFE are suitable for this.
Claims (8)
- Tandem warhead (4) with a secondary projectile (1), the secondary projectile (1) being fixed in a tubular section (2) of a casing (3) of the tandem warhead (4),characterized in thatand protection (6), against the gases and fumes produced on detonation, shielding the secondary projectile (1) from a hollow charge (8) mounted ahead of the secondary projectile (1),the casing (3) has a conical section (87) with the tubular section (2) which is smaller in diameter being disposed on it,a base (88) being provided on the tubular section (2),and in that the secondary projectile (1), which is of a smaller calibre than the hollow charge (8), has a circumferential thread (85) in which a thread (86) of the tubular section (2) engages, the secondary projectile (1) resting with initial tension against the base (88),and the protection (6) against detonation fumes, in a wedge-shaped annular space (101) formed by the conical section (87) of the casing (3) and by the secondary projectile (1) projecting from the tubular section (2) into this annular space (101), seals the secondary projectile (1), on occurrence of detonation fumes and gases, against the tubular section (2),the protection (6) against detonation fumes consisting of a compressible material.
- Tandem warhead according to Claim 1,
characterized in that
the protection (6) against detonation fumes consists of an elastic plastic, such as PVC, PP, PA, PE, POM or PTFE. - Tandem warhead according to Claim 1,
characterized in that
the protection (6) against detonation fumes, for compressing and improving the sealing effect, takes the Form of a wedge in direction of the hollow charge (8). - Tandem warhead according to Claim 1,
characterized in that
the protection (6) against detonation fumes rests with its surfaces (93, 94, 98) on the cone surface (95) and on a base surface (96) - lying at right angles to the principal axis (92) of the tandem warhead (4) - of the conical section (87) of the casing (3) and also encircles the secondary projectile (1) by way of an annular sealing lip (97) and an annular supporting surface (98). - Tandem warhead according to Claim 1,
characterized in that
the secondary projectile (1) rests against the base (88) with its rear ogive (46) supported over a large area with positive fit. - Tandem warhead according to Claim 1,
characterized in that
the thread (86) of the tubular section (2) is provided at the beginning of this tubular section (2), i.e. in the region of the protection (6) against detonation fumes. - Tandem warhead according to Claim 1,
characterized in thatthe thread (85) of the threaded connection (5) of the casing (3) is located approximately halfway along the length of the secondary projectile (1),a narrow annular space (99) following on from the rear of the threaded connection (5), this annular space (99) having a length which is approximately one third of the length of the secondary projectile (1) and being limited at the rear by the base (88). - Tandem warhead according to Claim 1,
characterized in that
the casing (3) is formed in one piece with the tubular section (2).
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19534217A DE19534217A1 (en) | 1995-09-15 | 1995-09-15 | Tandem warhead with a secondary floor |
| DE19534217 | 1995-09-15 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| EP0763706A2 EP0763706A2 (en) | 1997-03-19 |
| EP0763706A3 EP0763706A3 (en) | 1997-03-26 |
| EP0763706B1 true EP0763706B1 (en) | 1998-12-02 |
Family
ID=7772243
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP96114076A Expired - Lifetime EP0763706B1 (en) | 1995-09-15 | 1996-09-03 | Tandem warhead with secondary projectile |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US5561261A (en) |
| EP (1) | EP0763706B1 (en) |
| DE (2) | DE19534217A1 (en) |
| ES (1) | ES2127597T3 (en) |
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| DE19634457B3 (en) * | 1996-08-26 | 2007-06-06 | Diehl Stiftung & Co.Kg | Tandem warhead |
| US6105505A (en) | 1998-06-17 | 2000-08-22 | Lockheed Martin Corporation | Hard target incendiary projectile |
| US6904749B2 (en) * | 2002-10-18 | 2005-06-14 | Physical Sciences, Inc. | Polyoxymethylene as structural support member and propellant |
| US7530315B2 (en) * | 2003-05-08 | 2009-05-12 | Lone Star Ip Holdings, Lp | Weapon and weapon system employing the same |
| US8661980B1 (en) | 2003-05-08 | 2014-03-04 | Lone Star Ip Holdings, Lp | Weapon and weapon system employing the same |
| US7078603B2 (en) * | 2005-01-31 | 2006-07-18 | Pioneer Hi-Bred International, Inc. | Hybrid maize 32R38 |
| US7363862B2 (en) * | 2005-05-27 | 2008-04-29 | United States Of America As Represented By The Secretary Of The Army | Multi-purpose single initiated tandem warhead |
| US7044060B1 (en) * | 2005-07-07 | 2006-05-16 | The United States Of America As Represented By The Secretary Of The Army | Missile-borne explosive activated grenade release device |
| US7690304B2 (en) | 2005-09-30 | 2010-04-06 | Lone Star Ip Holdings, Lp | Small smart weapon and weapon system employing the same |
| US7895946B2 (en) | 2005-09-30 | 2011-03-01 | Lone Star Ip Holdings, Lp | Small smart weapon and weapon system employing the same |
| US8541724B2 (en) | 2006-09-29 | 2013-09-24 | Lone Star Ip Holdings, Lp | Small smart weapon and weapon system employing the same |
| US8117955B2 (en) | 2006-10-26 | 2012-02-21 | Lone Star Ip Holdings, Lp | Weapon interface system and delivery platform employing the same |
| USH2259H1 (en) | 2008-11-26 | 2011-07-05 | The United States Of America As Represented By The Secretary Of The Navy | Yield enhancing device and method of use |
| US9068803B2 (en) | 2011-04-19 | 2015-06-30 | Lone Star Ip Holdings, Lp | Weapon and weapon system employing the same |
| US8640623B2 (en) * | 2011-04-22 | 2014-02-04 | Donald B. Eckstein | Multiple purpose tandem nested projectile |
| US8800448B2 (en) * | 2012-02-08 | 2014-08-12 | Dynamic Solutions Llc | Stand-off door breaching device |
| DE102013010256B4 (en) * | 2013-06-18 | 2015-01-15 | Junghans Microtec Gmbh | Method for sealing a projectile |
| US20220065597A1 (en) * | 2018-12-19 | 2022-03-03 | Bae Systems Plc | Munitions and projectiles |
| CN113847428B (en) * | 2021-08-30 | 2023-01-17 | 西安近代化学研究所 | Balanced pressure sealing device |
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| GB1605340A (en) * | 1976-01-21 | 1992-01-02 | Messerschmitt Boelkow Blohm | Bombs and projectiles |
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| DE3544528C1 (en) * | 1985-12-17 | 1987-04-09 | Messerschmitt Boelkow Blohm | Tandem charge system having integrated protection elements |
| US4803928A (en) * | 1986-08-02 | 1989-02-14 | Stefan Kramer | Tandem charge projectile |
| US5107766A (en) * | 1991-07-25 | 1992-04-28 | Schliesske Harold R | Follow-thru grenade for military operations in urban terrain (MOUT) |
| DE4135392C2 (en) * | 1991-10-26 | 1995-05-18 | Deutsche Aerospace | Warhead |
| DE4225704A1 (en) * | 1992-08-04 | 1994-02-10 | Diehl Gmbh & Co | Warhead with a tandem charge |
| DE4436107A1 (en) * | 1994-10-10 | 1996-04-11 | Hoechst Ag | Polyacetal moulding materials with a high melt flow index |
| DE4437042A1 (en) * | 1994-10-17 | 1996-04-18 | Hoechst Ag | Polyacetal moulding material prodn. for low residual monomer content |
-
1995
- 1995-09-15 DE DE19534217A patent/DE19534217A1/en not_active Withdrawn
- 1995-10-11 US US08/540,942 patent/US5561261A/en not_active Expired - Fee Related
-
1996
- 1996-09-03 ES ES96114076T patent/ES2127597T3/en not_active Expired - Lifetime
- 1996-09-03 EP EP96114076A patent/EP0763706B1/en not_active Expired - Lifetime
- 1996-09-03 DE DE59600896T patent/DE59600896D1/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| DE59600896D1 (en) | 1999-01-14 |
| ES2127597T3 (en) | 1999-04-16 |
| EP0763706A2 (en) | 1997-03-19 |
| DE19534217A1 (en) | 1997-03-20 |
| EP0763706A3 (en) | 1997-03-26 |
| US5561261A (en) | 1996-10-01 |
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