NO955323L - Enhetlig missil antenne-skrog anordning - Google Patents

Enhetlig missil antenne-skrog anordning

Info

Publication number
NO955323L
NO955323L NO955323A NO955323A NO955323L NO 955323 L NO955323 L NO 955323L NO 955323 A NO955323 A NO 955323A NO 955323 A NO955323 A NO 955323A NO 955323 L NO955323 L NO 955323L
Authority
NO
Norway
Prior art keywords
hull
missile
antenna
bmi
uniform
Prior art date
Application number
NO955323A
Other languages
English (en)
Other versions
NO955323D0 (no
Inventor
Andrew B Facciano
Ronald N Hopkins
Rodney H Krebs
James L Neumann
Oscar K Ohanian
Original Assignee
Hughes Missile Systems
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 Hughes Missile Systems filed Critical Hughes Missile Systems
Publication of NO955323D0 publication Critical patent/NO955323D0/no
Publication of NO955323L publication Critical patent/NO955323L/no

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)

Abstract

En enhetlig missilantenne-skroganordning (50) er tilveiebragt for integrering i et våpenmissil (12) som bærer primære missillaster, rommer innvendige elektronikk- sammenstillinger, gir monteringsoverflatesoner for eksterne sensorantenner (71), og beskytter følsomme antennekomponenter mot overlyds aerodynamisk oppvarming. Hver ende av skroganordningen (50) er dannet av en festering (52, 54) som har en omkretsmessig fordypning (84, 86) som mottar en filamentviklet hovedkonstruksjon (60) til å danne missilets skrogrør. Fortrinnsvis blir en titanforing (58) først sammen- føyet med hver festering med en trinn-stykkesammenføyning (94, 96) langs hvilken den er klebemessig bundet. Foringen (58) og hosliggende festeringpartier (52, 57) til- veiebringer en spindel på hvilken et forsterkningsmateriale av grafitt/ Bismaleimide (BMI) harpiks filamentvikles og samherdes til å danne den enhetlige skrogkonstruksjon (60). Et flertall av Grafitt/BMI tilleggslag (62, 63, 64, 65) er aksisymmetrisk plassert på skrogets utvendige overflate til å danne fire antennehulrom (66, 67, 68, 69) som mottar antenner (71) deri. Deretter omslutter avstandsorganer (72, 73, 74, 75) antennene (71) om hvilke en kuppeloverpakking (70) filamentvikles med et Quarts/BMI forsterknings- materiale. Hele konstruksjonen (70) blir så enhetlig herdet til den innvendige skrog- konstruksjon (60) og antenneavstandsorganene (72, 73, 74, 75), hvoretter den overflate- behandles (76) og gis ytterbelegg (78).
NO955323A 1994-12-27 1995-12-27 Enhetlig missil antenne-skrog anordning NO955323L (no)

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
NO955323D0 NO955323D0 (no) 1995-12-27
NO955323L true NO955323L (no) 1996-06-28

Family

ID=23436612

Family Applications (1)

Application Number Title Priority Date Filing Date
NO955323A NO955323L (no) 1994-12-27 1995-12-27 Enhetlig missil antenne-skrog anordning

Country Status (6)

Country Link
US (1) US5483894A (no)
EP (1) EP0720210A2 (no)
AU (1) AU686484B2 (no)
CA (1) CA2166007A1 (no)
IL (1) IL116555A (no)
NO (1) NO955323L (no)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
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
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)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
AU686484B2 (en) 1998-02-05
US5483894A (en) 1996-01-16
IL116555A0 (en) 1996-03-31
NO955323D0 (no) 1995-12-27
AU4072595A (en) 1996-07-04
EP0720210A2 (en) 1996-07-03
IL116555A (en) 1999-09-22
CA2166007A1 (en) 1996-06-28

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