TR200002553T2 - Sheathed air bomb. - Google Patents
Sheathed air bomb.Info
- Publication number
- TR200002553T2 TR200002553T2 TR2000/02553T TR200002553T TR200002553T2 TR 200002553 T2 TR200002553 T2 TR 200002553T2 TR 2000/02553 T TR2000/02553 T TR 2000/02553T TR 200002553 T TR200002553 T TR 200002553T TR 200002553 T2 TR200002553 T2 TR 200002553T2
- Authority
- TR
- Turkey
- Prior art keywords
- bomb
- existing
- penetrating
- weight
- penetrating body
- Prior art date
Links
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
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/44—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information of incendiary type
-
- 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
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/56—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing discrete solid bodies
- F42B12/58—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles
- F42B12/62—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile
- F42B12/625—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile a single submissile arranged in a carrier missile for being launched or accelerated coaxially; Coaxial tandem arrangement of missiles which are active in the target one after the other
-
- 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
- F42B12/06—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 hard or heavy core; Kinetic energy penetrators
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B25/00—Fall bombs
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Chemical & Material Sciences (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Magnetic Resonance Imaging Apparatus (AREA)
- Arc Welding In General (AREA)
- Pens And Brushes (AREA)
- Laminated Bodies (AREA)
- Toys (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Jet Pumps And Other Pumps (AREA)
- X-Ray Techniques (AREA)
- Respiratory Apparatuses And Protective Means (AREA)
Abstract
A target penetrating aerial bomb including a penetrating body (24) shaped for improved target penetration, having a narrower impact profile at approximately the same weight as an existing bomb. An aerodynamic shroud (40) encases the penetrating body (24) and emulates the aerodynamic shape of the existing bomb, and the weight, center of gravity, and moments of inertia of the bomb closely approximate those properties of the existing bomb. The bomb according to the invention may be qualified for flight by similarity to the existing bomb, and thus avoid lengthy and costly qualification procedures.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/US1997/023112 WO1999030106A1 (en) | 1997-12-11 | 1997-12-11 | Shrouded aerial bomb |
Publications (1)
Publication Number | Publication Date |
---|---|
TR200002553T2 true TR200002553T2 (en) | 2000-11-21 |
Family
ID=22262294
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
TR2000/02553T TR200002553T2 (en) | 1997-12-11 | 1997-12-11 | Sheathed air bomb. |
Country Status (15)
Country | Link |
---|---|
EP (1) | EP1038152B1 (en) |
JP (1) | JP2001526378A (en) |
KR (2) | KR100549486B1 (en) |
AT (2) | ATE273502T1 (en) |
AU (1) | AU748098B2 (en) |
DE (1) | DE69730252T2 (en) |
DK (2) | DK1367358T3 (en) |
EG (1) | EG22193A (en) |
ES (1) | ES2226012T3 (en) |
IL (1) | IL136676A (en) |
NO (1) | NO318816B1 (en) |
PT (1) | PT1038152E (en) |
TR (1) | TR200002553T2 (en) |
TW (1) | TW381164B (en) |
WO (1) | WO1999030106A1 (en) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6408762B1 (en) | 1997-12-11 | 2002-06-25 | Lockheed Martin Corporation | Clamp assembly for shrouded aerial bomb |
US6374744B1 (en) * | 2000-05-25 | 2002-04-23 | Lockheed Martin Corporation | Shrouded bomb |
FR2845763B1 (en) * | 2002-10-11 | 2006-12-01 | Tda Armements Sas | AUTONOMOUS GUIDING SYSTEM FOR ARTILLERY MUNITION AND GUIDED ARTILLERY MUNITION |
DE102005039902A1 (en) * | 2005-02-04 | 2006-08-10 | Rheinmetall Waffe Munition Gmbh | Device for increasing the precision of tail-wing stabilized ammunition |
WO2008118235A2 (en) * | 2006-12-20 | 2008-10-02 | Ruhlman James D | Reduced collateral damage bomb (rcdb) including fuse system with shaped charges and a system and method of making same |
FR2910613B1 (en) * | 2006-12-21 | 2009-10-02 | Ateliers Mecaniques De Pont Su | GUIDE PROJECTILE HAVING A SLEEVE FOR MOUNTING A GUIDE SYSTEM |
DE102008023678B4 (en) * | 2008-05-15 | 2012-11-29 | Diehl Bgt Defence Gmbh & Co. Kg | bomb |
EP2496908B1 (en) | 2009-11-04 | 2013-09-11 | Diehl BGT Defence GmbH & Co.KG | Aircraft bomb |
FR2958391B1 (en) * | 2010-03-30 | 2012-07-27 | Nexter Munitions | PENETRATEUR WITH KINETIC ENERGY. |
US8985026B2 (en) * | 2011-11-22 | 2015-03-24 | Alliant Techsystems Inc. | Penetrator round assembly |
US9587921B2 (en) | 2013-05-31 | 2017-03-07 | Robert T. Faxon | Warhead casings and methods of manufacture |
KR101593426B1 (en) | 2015-07-20 | 2016-02-18 | 이순태 | Bonding device for the band a bomb airdrop |
KR101638958B1 (en) | 2015-12-23 | 2016-07-12 | 이순태 | Folding device for the safety pins a bomb airdrop |
US11067372B2 (en) * | 2019-12-04 | 2021-07-20 | Bae Systems Information And Electronic Systems Integration Inc. | Ordnance nose cone |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3224334A (en) * | 1964-02-05 | 1965-12-21 | Curtis Roman | Retrofit lugs for bombs |
FR2519753B1 (en) * | 1982-01-08 | 1986-02-21 | Matra | STAGE BODY PENETRATION BOMB |
US4597333A (en) * | 1983-07-08 | 1986-07-01 | Rheinmetall G.M.B.H. | Two-part armor-piercing projectile |
US4656943A (en) * | 1984-12-07 | 1987-04-14 | Motorola, Inc. | Low profile, pivoted generator |
US4638737A (en) * | 1985-06-28 | 1987-01-27 | The United States Of America As Represented By The Secretary Of The Army | Multi-warhead, anti-armor missile |
DE3635361A1 (en) * | 1986-10-17 | 1988-04-21 | Diehl Gmbh & Co | Artillery shell with submunitions |
FR2615937B1 (en) * | 1987-05-27 | 1989-09-08 | Ladriere Serge | IMPROVEMENTS TO PERFORATING PROJECTILES |
FR2616217B1 (en) * | 1987-06-02 | 1993-02-05 | Thomson Brandt Armements | SYSTEM FOR HOLDING MULTIPLE LOADS ON BOARD IN A PROJECTILE ROTATING AROUND ITS LONGITUDINAL AXIS |
DE3737232A1 (en) * | 1987-11-03 | 1989-05-18 | Rheinmetall Gmbh | EXERCISE FLOOR WITH SHORTENED RANGE |
FR2656081B1 (en) * | 1989-12-19 | 1992-02-28 | Thomson Brandt Armements | PERIPHERAL COVER FOR A GUIDED AMMUNITION DRAWN BY CANON EFFECT. |
US5056408A (en) * | 1990-07-31 | 1991-10-15 | Techteam, Inc. | Self-retracting, drag-free lug for bombs |
USH959H (en) * | 1991-02-19 | 1991-09-03 | The United States Of America As Represented By The Secretary Of The Navy | Projectile terminal delivery vehicle assembly |
DE19535218C1 (en) * | 1995-09-22 | 1997-02-27 | Diehl Gmbh & Co | Ballistic projectile |
-
1997
- 1997-12-11 TR TR2000/02553T patent/TR200002553T2/en unknown
- 1997-12-11 KR KR1020007006391A patent/KR100549486B1/en not_active IP Right Cessation
- 1997-12-11 WO PCT/US1997/023112 patent/WO1999030106A1/en active IP Right Grant
- 1997-12-11 DK DK03019851T patent/DK1367358T3/en active
- 1997-12-11 EP EP97955029A patent/EP1038152B1/en not_active Expired - Lifetime
- 1997-12-11 AU AU70971/98A patent/AU748098B2/en not_active Ceased
- 1997-12-11 ES ES97955029T patent/ES2226012T3/en not_active Expired - Lifetime
- 1997-12-11 AT AT97955029T patent/ATE273502T1/en not_active IP Right Cessation
- 1997-12-11 JP JP2000524626A patent/JP2001526378A/en not_active Withdrawn
- 1997-12-11 KR KR1020027014634A patent/KR100549487B1/en not_active IP Right Cessation
- 1997-12-11 IL IL13667697A patent/IL136676A/en not_active IP Right Cessation
- 1997-12-11 AT AT03019851T patent/ATE408801T1/en not_active IP Right Cessation
- 1997-12-11 PT PT97955029T patent/PT1038152E/en unknown
- 1997-12-11 DK DK97955029T patent/DK1038152T3/en active
- 1997-12-11 DE DE69730252T patent/DE69730252T2/en not_active Expired - Fee Related
-
1998
- 1998-10-20 TW TW087117276A patent/TW381164B/en not_active IP Right Cessation
- 1998-10-29 EG EG132498A patent/EG22193A/en active
-
2000
- 2000-06-13 NO NO20003019A patent/NO318816B1/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
TW381164B (en) | 2000-02-01 |
NO20003019L (en) | 2000-08-10 |
EP1038152A1 (en) | 2000-09-27 |
EP1038152A4 (en) | 2003-01-22 |
ATE408801T1 (en) | 2008-10-15 |
EP1038152B1 (en) | 2004-08-11 |
NO20003019D0 (en) | 2000-06-13 |
KR20010033035A (en) | 2001-04-25 |
ES2226012T3 (en) | 2005-03-16 |
KR100549486B1 (en) | 2006-02-08 |
DK1367358T3 (en) | 2009-02-02 |
IL136676A0 (en) | 2001-06-14 |
DK1038152T3 (en) | 2004-12-13 |
EG22193A (en) | 2002-10-31 |
PT1038152E (en) | 2004-11-30 |
DE69730252T2 (en) | 2004-12-30 |
JP2001526378A (en) | 2001-12-18 |
IL136676A (en) | 2003-03-12 |
ATE273502T1 (en) | 2004-08-15 |
AU7097198A (en) | 1999-06-28 |
KR100549487B1 (en) | 2006-02-08 |
AU748098B2 (en) | 2002-05-30 |
DE69730252D1 (en) | 2004-09-16 |
KR20020089577A (en) | 2002-11-29 |
NO318816B1 (en) | 2005-05-09 |
WO1999030106A1 (en) | 1999-06-17 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
TR200002553T2 (en) | Sheathed air bomb. | |
ES2088999T3 (en) | SUPERSONIC MISSILES PILOTED IN PAIR THROUGH ESPOILERS. | |
NO874474L (en) | WINGS FOR SUPERSONIC WEIGHT OR COMPRESSOR. | |
EP1367358A3 (en) | Shrouded aerial bomb | |
GB2227818A (en) | Warhead | |
FI860455A0 (en) | PANSARGENOMTRAENGANDE PROJEKTIL. | |
ATE70237T1 (en) | AIRPLANE. | |
US4589342A (en) | Rocket-powered training missile with impact motor splitting device | |
IT9047997A0 (en) | SYSTEM FOR THE DEPLOYMENT OF AERODYNAMIC SURFACES (AEROFOIL) ON PROJECTILES, MISSILES OR SIMILAR | |
RU2077697C1 (en) | Guided rocket of aerodynamic scheme utka | |
FI881543A (en) | Armored explosive shell | |
GB2418871A (en) | Tossable flier | |
RU99107834A (en) | METHOD OF PROTECTION AGAINST MILITARY AIR HITS | |
RU20087U1 (en) | LAUNCHED AIRCRAFT | |
GOBELTZ | Effects of airframe design on spin characteristics | |
Warwick | Targeted training | |
HABERCOM | Bird strikes and aviation safety. Citations from the NTIS data base[Progress Report, 1964- Jun. 1980] | |
LEGER et al. | Parachute opening shocks during high speed ejections: Normalization(CHOCS A L'OUVERTURE LORS DES EJECTIONS A GRANDE VITESSE? QUELLES NORMES?) | |
Donaldson | Seahawk evolution | |
Shane | The role of the test pilot in UAV development | |
SVENSSON | Kinematic model of a beam riding air-to-air missile(Kinematisk modell foer kollimationsstyrd jaktrobot, metodrapport) | |
HABERCOM | Bird strikes and aviation safety. A bibliography with abstracts[Progress Report, 1964- Jun. 1978] | |
MA | Numerical simulation of the heavy weight Orbiter GRTLS abort((Glide Return To Launch Site)) | |
ONDA et al. | The concept of an unmanned flying vehicle at high altitude | |
IT8424222A0 (en) | WEAPON SIMULATION EQUIPMENT FOR EXERCISE IN SHOOTING PROJECTILES, LAUNCHING ROCKETS AND MISSILES, OR THE SIMILAR. |