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
Application number
TR2000/02553T
Other languages
Turkish (tr)
Inventor
E. Schmaker Bruce
L. Wooten Ronald
Original Assignee
Lockheed-Martin Corporation
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Lockheed-Martin Corporation filed Critical Lockheed-Martin Corporation
Publication of TR200002553T2 publication Critical patent/TR200002553T2/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/36Projectiles, 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
    • F42B12/44Projectiles, 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/36Projectiles, 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
    • F42B12/56Projectiles, 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
    • F42B12/58Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles
    • F42B12/62Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile
    • F42B12/625Cluster 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/04Projectiles, 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
    • F42B12/06Projectiles, 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B25/00Fall 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)
  • Pens And Brushes (AREA)
  • Arc Welding In General (AREA)
  • X-Ray Techniques (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Toys (AREA)
  • Laminated Bodies (AREA)
  • Respiratory Apparatuses And Protective Means (AREA)
  • Jet Pumps And Other Pumps (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.
TR2000/02553T 1997-12-11 1997-12-11 Sheathed air bomb. TR200002553T2 (en)

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) KR100549487B1 (en)
AT (2) ATE408801T1 (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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
KR20020089577A (en) 2002-11-29
EP1038152A1 (en) 2000-09-27
DK1367358T3 (en) 2009-02-02
EG22193A (en) 2002-10-31
ATE273502T1 (en) 2004-08-15
EP1038152A4 (en) 2003-01-22
NO20003019D0 (en) 2000-06-13
DE69730252D1 (en) 2004-09-16
IL136676A (en) 2003-03-12
AU748098B2 (en) 2002-05-30
TW381164B (en) 2000-02-01
DK1038152T3 (en) 2004-12-13
NO20003019L (en) 2000-08-10
NO318816B1 (en) 2005-05-09
KR20010033035A (en) 2001-04-25
JP2001526378A (en) 2001-12-18
KR100549486B1 (en) 2006-02-08
EP1038152B1 (en) 2004-08-11
WO1999030106A1 (en) 1999-06-17
ES2226012T3 (en) 2005-03-16
AU7097198A (en) 1999-06-28
ATE408801T1 (en) 2008-10-15
DE69730252T2 (en) 2004-12-30
IL136676A0 (en) 2001-06-14
PT1038152E (en) 2004-11-30
KR100549487B1 (en) 2006-02-08

Similar Documents

Publication Publication Date Title
TR200002553T2 (en) Sheathed air bomb.
ES2088999T3 (en) SUPERSONIC MISSILES PILOTED IN PAIR THROUGH ESPOILERS.
EP1367358A3 (en) Shrouded aerial bomb
GB2227818A (en) Warhead
FI860455A (en) PANSARGENOMTRAENGANDE PROJEKTIL.
US4589342A (en) Rocket-powered training missile with impact motor splitting device
WO2004025041A3 (en) Passive aerial protection system
US2879999A (en) Aerial tow target
IT9047997A0 (en) SYSTEM FOR THE DEPLOYMENT OF AERODYNAMIC SURFACES (AEROFOIL) ON PROJECTILES, MISSILES OR SIMILAR
RU2077697C1 (en) Guided rocket of aerodynamic scheme utka
ATE85114T1 (en) ARMORED SHELL.
GB594517A (en) Improvements in or relating to aeroplane and other bombs or projectiles
RU99107834A (en) METHOD OF PROTECTION AGAINST MILITARY AIR HITS
RU20087U1 (en) LAUNCHED AIRCRAFT
WO2004112922A3 (en) Tossable flier
GOBELTZ Effects of airframe design on spin characteristics
BABA et al. Guidance law for a flight vehicle with constant acceleration
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
JP2001116493A (en) Guided missile launcher
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]
LEHMAN Helmets and head protection in USAF ejections 1968-1972