IL116555A - Integral missile antenna-fuselage assembly - Google Patents
Integral missile antenna-fuselage assemblyInfo
- Publication number
- IL116555A IL116555A IL11655595A IL11655595A IL116555A IL 116555 A IL116555 A IL 116555A IL 11655595 A IL11655595 A IL 11655595A IL 11655595 A IL11655595 A IL 11655595A IL 116555 A IL116555 A IL 116555A
- Authority
- IL
- Israel
- Prior art keywords
- fuselage assembly
- missile antenna
- integral
- integral missile
- antenna
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Details Of Aerials (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US08/364,905 US5483894A (en) | 1994-12-27 | 1994-12-27 | Integral missile antenna-fuselage assembly |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| IL116555A0 IL116555A0 (en) | 1996-03-31 |
| IL116555A true IL116555A (en) | 1999-09-22 |
Family
ID=23436612
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IL11655595A IL116555A (en) | 1994-12-27 | 1995-12-26 | Integral missile antenna-fuselage assembly |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US5483894A (fr) |
| EP (1) | EP0720210A2 (fr) |
| AU (1) | AU686484B2 (fr) |
| CA (1) | CA2166007A1 (fr) |
| IL (1) | IL116555A (fr) |
| NO (1) | NO955323L (fr) |
Families Citing this family (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6863279B2 (en) | 2001-12-05 | 2005-03-08 | Conoco Investments Norge Ad | Redundant seal design for composite risers with metal liners |
| US6719058B2 (en) | 2001-12-05 | 2004-04-13 | Deepwater Composites As | Multiple seal design for composite risers and tubing for offshore applications |
| US20040086341A1 (en) * | 2002-11-05 | 2004-05-06 | Conoco Inc. | Metal lined composite risers in offshore applications |
| US7090006B2 (en) | 2002-11-05 | 2006-08-15 | Conocophillips Company | Replaceable liner for metal lined composite risers in offshore applications |
| NO322237B1 (no) * | 2004-09-27 | 2006-09-04 | Aker Subsea As | Komposittrør og fremgangsmåte for fremstilling av et komposittrør |
| US7509903B2 (en) * | 2005-04-08 | 2009-03-31 | Raytheon Company | Separable structure material |
| US7681834B2 (en) | 2006-03-31 | 2010-03-23 | Raytheon Company | Composite missile nose cone |
| US8074516B2 (en) * | 2008-06-26 | 2011-12-13 | Raytheon Company | Methods and apparatus for non-axisymmetric radome |
| US20130280470A1 (en) | 2012-04-20 | 2013-10-24 | Julian Norly | Thermal Management For Aircraft Composites |
| US9541364B2 (en) | 2014-09-23 | 2017-01-10 | Raytheon Company | Adaptive electronically steerable array (AESA) system for interceptor RF target engagement and communications |
| CN105987651B (zh) * | 2015-01-30 | 2018-11-30 | 北京临近空间飞行器系统工程研究所 | 一种蓄热式火箭共形天线构型 |
| CN111045437A (zh) * | 2018-10-12 | 2020-04-21 | 北京理工大学 | 抗高过载的一体化制导控制系统 |
| FR3099132B1 (fr) * | 2019-07-26 | 2022-01-28 | Mbda France | Capot pour vehicule, en particulier pour vehicule supersonique ou hypersonique |
| DE102020001153C5 (de) * | 2020-02-21 | 2026-03-26 | Diehl Defence Gmbh & Co. Kg | Flugkörper, insbesondere Lenkflugkörper, mit einer Radarsensoreinheit |
| US11650034B1 (en) * | 2021-03-25 | 2023-05-16 | The United States Of America As Represented By The Secretary Of The Army | Internal captive collar joint for projectile |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4485740A (en) * | 1981-12-23 | 1984-12-04 | Ford Aerospace & Communications Corporation | Coupling assembly for joining tubular sections |
| US4665792A (en) * | 1985-08-06 | 1987-05-19 | The United States Of America As Represented By The Secretary Of The Air Force | Missile longitudinal support assembly |
| FR2656081B1 (fr) * | 1989-12-19 | 1992-02-28 | Thomson Brandt Armements | Enveloppe peripherique pour une munition guidee tiree par effet canon. |
| US5394803A (en) * | 1994-02-14 | 1995-03-07 | Bel Electronics, Inc. | Joint construction between military rocket motor and warhead and releasable by melting of fusible eutectic wedging ring for operating flexible locking fingers |
-
1994
- 1994-12-27 US US08/364,905 patent/US5483894A/en not_active Expired - Lifetime
-
1995
- 1995-12-22 CA CA002166007A patent/CA2166007A1/fr not_active Abandoned
- 1995-12-26 IL IL11655595A patent/IL116555A/xx not_active IP Right Cessation
- 1995-12-27 EP EP95309472A patent/EP0720210A2/fr not_active Withdrawn
- 1995-12-27 NO NO955323A patent/NO955323L/no unknown
- 1995-12-28 AU AU40725/95A patent/AU686484B2/en not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| IL116555A0 (en) | 1996-03-31 |
| AU4072595A (en) | 1996-07-04 |
| US5483894A (en) | 1996-01-16 |
| NO955323D0 (no) | 1995-12-27 |
| EP0720210A2 (fr) | 1996-07-03 |
| CA2166007A1 (fr) | 1996-06-28 |
| AU686484B2 (en) | 1998-02-05 |
| NO955323L (no) | 1996-06-28 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FF | Patent granted | ||
| KB | Patent renewed | ||
| KB | Patent renewed | ||
| KB | Patent renewed | ||
| MM9K | Patent not in force due to non-payment of renewal fees |