IL35596A - Fragmenting protective cover for the nose of a missile - Google Patents
Fragmenting protective cover for the nose of a missileInfo
- Publication number
- IL35596A IL35596A IL35596A IL3559670A IL35596A IL 35596 A IL35596 A IL 35596A IL 35596 A IL35596 A IL 35596A IL 3559670 A IL3559670 A IL 3559670A IL 35596 A IL35596 A IL 35596A
- Authority
- IL
- Israel
- Prior art keywords
- cover
- fragmenting
- missile
- nose
- fragmentable
- Prior art date
Links
- 230000001681 protective effect Effects 0.000 title claims description 7
- 239000000463 material Substances 0.000 claims description 20
- 238000013467 fragmentation Methods 0.000 claims description 10
- 238000006062 fragmentation reaction Methods 0.000 claims description 10
- 239000012634 fragment Substances 0.000 claims description 4
- 239000005345 chemically strengthened glass Substances 0.000 claims description 2
- 239000002245 particle Substances 0.000 description 5
- 230000005855 radiation Effects 0.000 description 5
- 241000238631 Hexapoda Species 0.000 description 3
- 238000011109 contamination Methods 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- 239000011521 glass Substances 0.000 description 3
- 150000002500 ions Chemical class 0.000 description 3
- 230000003287 optical effect Effects 0.000 description 3
- 239000002196 Pyroceram Substances 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 230000007613 environmental effect Effects 0.000 description 2
- 230000003628 erosive effect Effects 0.000 description 2
- 238000005342 ion exchange Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 230000003068 static effect Effects 0.000 description 2
- 239000006095 Cer-Vit Substances 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000006260 foam Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000036961 partial effect Effects 0.000 description 1
- 229920002635 polyurethane Polymers 0.000 description 1
- 239000004814 polyurethane Substances 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
- 230000035945 sensitivity Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 229920001059 synthetic polymer Polymers 0.000 description 1
- 238000012360 testing method 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
- F42B10/38—Range-increasing arrangements
- F42B10/42—Streamlined projectiles
- F42B10/46—Streamlined nose cones; Windshields; Radomes
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)
- Details Of Aerials (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US2491370A | 1970-03-23 | 1970-03-23 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| IL35596A0 IL35596A0 (en) | 1971-04-28 |
| IL35596A true IL35596A (en) | 1973-11-28 |
Family
ID=21823007
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IL35596A IL35596A (en) | 1970-03-23 | 1970-11-05 | Fragmenting protective cover for the nose of a missile |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US3674227A (de) |
| JP (1) | JPS5018718B1 (de) |
| CH (1) | CH525798A (de) |
| DE (1) | DE2059492A1 (de) |
| FR (1) | FR2074186A5 (de) |
| GB (1) | GB1320969A (de) |
| IL (1) | IL35596A (de) |
| SE (1) | SE357614B (de) |
Families Citing this family (40)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1383513A (en) * | 1971-06-10 | 1974-02-12 | Hawker Siddeley Aviation Ltd | Aircrew escape systems |
| JPS49131698U (de) * | 1973-03-12 | 1974-11-12 | ||
| GB2245050B (en) * | 1982-09-17 | 1992-05-13 | Short Brothers Ltd | Missile with proximity fuze |
| GB2129103A (en) * | 1982-10-18 | 1984-05-10 | Raytheon Co | Mortar round |
| GB2204668B (en) * | 1983-07-16 | 1989-05-17 | Barr & Stroud Ltd | Explosion ignition systems |
| US4515082A (en) * | 1983-09-22 | 1985-05-07 | Ford Aerospace & Communications Corporation | Guided projectile lens cover |
| US4649795A (en) * | 1984-05-16 | 1987-03-17 | Hi-Shear Corporation | Structural shroud system incorporating a pyrotechnic |
| US4593637A (en) * | 1984-06-04 | 1986-06-10 | The United States Of America As Represented By The Secretary Of The Navy | Combination frangible nose cap EMI shield |
| US4753169A (en) * | 1985-12-23 | 1988-06-28 | General Dynamics, Pomona Division | Ablating electromagnetic shield sheath |
| US5159151A (en) * | 1986-05-08 | 1992-10-27 | British Aerospace Public Limited Company | Missile nose fairing assembly |
| US4867357A (en) * | 1987-12-21 | 1989-09-19 | General Dynamics Corp., Pomona Division | Jettisonable protective cover device |
| DE3911576A1 (de) * | 1989-04-08 | 1990-10-11 | Rheinmetall Gmbh | Fluegelstabilisiertes geschoss |
| US5261629A (en) * | 1989-04-08 | 1993-11-16 | Rheinmetall Gmbh | Fin stabilized projectile |
| GB2250804B (en) * | 1990-11-07 | 1994-06-01 | Colebrand Ltd | Protective device for a sensing head |
| GB2253030A (en) * | 1991-02-21 | 1992-08-26 | British Aerospace | Missiles |
| US5167386A (en) * | 1992-01-21 | 1992-12-01 | Rockwell International Corporation | Pyrotechnic removal of a radome cover |
| DE4235266C1 (de) * | 1992-10-20 | 1993-10-21 | Bodenseewerk Geraetetech | Verbindungsanordnung zum Verbinden eines einen Suchkopf abdeckenden Domes mit der Struktur eines Flugkörpers |
| US5853149A (en) * | 1996-04-08 | 1998-12-29 | Raytheon Company | Stress-free dome mount missile design |
| FR2769975B1 (fr) * | 1997-10-20 | 2000-01-07 | Thomson Csf | Dispositif de retenue notamment de l'allumeur arriere d'un missile |
| RU2188779C2 (ru) * | 2000-07-20 | 2002-09-10 | Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр им.М.В.Хруничева" | Устройство для защиты оптических поверхностей космического аппарата |
| IL139891A (en) * | 2000-11-23 | 2004-07-25 | Rafael Armament Dev Authority | Protection element disconnected |
| DE10211493B3 (de) * | 2002-03-15 | 2004-02-26 | Lfk-Lenkflugkörpersysteme Gmbh | Absprengbare Abdeckhaube |
| FR2840029B1 (fr) * | 2002-05-27 | 2004-08-13 | Mbdam | Systeme d'obturation pour un orifice d'un conduit, en particulier pour un orifice d'une voie d'introduction d'air dans la chambre de combustion d'un statoreacteur |
| DE10240040A1 (de) * | 2002-08-27 | 2004-03-11 | BODENSEEWERK GERäTETECHNIK GMBH | Lenkflugkörper mit abwerfbarer Schutzkappe |
| DE102005030090B4 (de) * | 2005-06-27 | 2007-03-22 | Diehl Bgt Defence Gmbh & Co. Kg | Abwerfbare Vorsatzhaube sowie Flugkörper mit abwerfbarer Vorsatzhaube |
| US7766277B2 (en) * | 2006-01-19 | 2010-08-03 | The Boeing Company | Deformable forward pressure bulkhead for an aircraft |
| EP2002198B1 (de) * | 2006-03-30 | 2013-04-24 | Raytheon Company | Verfahren und vorrichtung für ein integriertes sperrverschlusssystem |
| WO2009105312A2 (en) * | 2008-01-31 | 2009-08-27 | The Penn State Research Foundation | Removable protective nose cover |
| DE102009003201B4 (de) | 2009-05-18 | 2013-07-25 | Airbus Operations Gmbh | Verfahren zum Schutz eines Teiles einer Oberfläche eines Flugzeuges vor Verunreinigung mit Insektenresten und/oder Vereisungen, Flugzeug mit einer Beschichtung auf einem Teil seiner Oberfläche, Verwendung einer Beschichtung sowie Verwendung einer Beschichtungsvorrichtung zum Beschichten eines Teiles einer Oberfläche eines Flugzeuges mit einer Beschichtung |
| FR2960055B1 (fr) * | 2010-05-12 | 2015-11-20 | Tda Armements Sas | Munition guidee protegee par une coiffe aerodynamique |
| FR2966919B1 (fr) * | 2010-10-29 | 2013-11-01 | Tda Armements Sas | Coiffe aerodynamique secable pour munition guidee et munition guidee comportant une telle coiffe. |
| FR2966920B1 (fr) * | 2010-10-29 | 2013-05-17 | Tda Armements Sas | Coiffe aerodynamique ejectable pour munition guidee et munition guidee comportant une telle coiffe. |
| US8445823B2 (en) * | 2010-11-02 | 2013-05-21 | Raytheon Company | Guided munition systems including combustive dome covers and methods for equipping guided munitions with the same |
| US8461501B2 (en) * | 2010-11-02 | 2013-06-11 | Raytheon Company | Guided munitions including self-deploying dome covers and methods for equipping guided munitions with the same |
| US8186260B2 (en) * | 2010-11-03 | 2012-05-29 | Raytheon Company | Translating adjacent-blast shield and method for protecting external slots of missiles in launcher tubes |
| US8497456B2 (en) * | 2011-03-30 | 2013-07-30 | Raytheon Company | Guided munitions including interlocking dome covers and methods for equipping guided munitions with the same |
| CN111391992A (zh) * | 2020-04-06 | 2020-07-10 | 西北工业大学 | 一种水下航行器高速入水缓冲头帽 |
| CN111392010B (zh) * | 2020-04-06 | 2021-09-17 | 西北工业大学 | 一种航行器高速入水非对称缓冲头帽 |
| FR3138203A1 (fr) * | 2022-07-21 | 2024-01-26 | Safran Electronics & Defense | Véhicule aérien à optique frontale protégée. |
| US20250136297A1 (en) * | 2023-10-31 | 2025-05-01 | Bae Systems Information And Electronic Systems Integration Inc. | Launch initiated low-drag seeker window cover |
-
1970
- 1970-03-23 US US24913A patent/US3674227A/en not_active Expired - Lifetime
- 1970-11-05 IL IL35596A patent/IL35596A/en unknown
- 1970-11-17 GB GB5461370A patent/GB1320969A/en not_active Expired
- 1970-12-03 DE DE19702059492 patent/DE2059492A1/de active Pending
- 1970-12-09 CH CH1818470A patent/CH525798A/de not_active IP Right Cessation
- 1970-12-22 FR FR7046333A patent/FR2074186A5/fr not_active Expired
- 1970-12-22 SE SE17459/70A patent/SE357614B/xx unknown
- 1970-12-23 JP JP45115948A patent/JPS5018718B1/ja active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| DE2059492A1 (de) | 1971-10-07 |
| US3674227A (en) | 1972-07-04 |
| JPS5018718B1 (de) | 1975-07-01 |
| SE357614B (de) | 1973-07-02 |
| IL35596A0 (en) | 1971-04-28 |
| GB1320969A (en) | 1973-06-20 |
| FR2074186A5 (de) | 1971-10-01 |
| CH525798A (de) | 1972-07-31 |
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