NO170952C - Anordning for aa feste et missil til en utskytningsenhet - Google Patents

Anordning for aa feste et missil til en utskytningsenhet

Info

Publication number
NO170952C
NO170952C NO882805A NO882805A NO170952C NO 170952 C NO170952 C NO 170952C NO 882805 A NO882805 A NO 882805A NO 882805 A NO882805 A NO 882805A NO 170952 C NO170952 C NO 170952C
Authority
NO
Norway
Prior art keywords
missile
achieving
deploying unit
deploying
unit
Prior art date
Application number
NO882805A
Other languages
English (en)
Other versions
NO170952B (no
NO882805D0 (no
NO882805L (no
Inventor
Henry August
Original Assignee
Hughes Aircraft Co
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 Aircraft Co filed Critical Hughes Aircraft Co
Publication of NO882805D0 publication Critical patent/NO882805D0/no
Publication of NO882805L publication Critical patent/NO882805L/no
Publication of NO170952B publication Critical patent/NO170952B/no
Publication of NO170952C publication Critical patent/NO170952C/no

Links

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

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)
NO882805A 1987-06-26 1988-06-24 Anordning for aa feste et missil til en utskytningsenhet NO170952C (no)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/066,449 US4809929A (en) 1987-06-26 1987-06-26 Splitter plates for alleviation of missile hook drag

Publications (4)

Publication Number Publication Date
NO882805D0 NO882805D0 (no) 1988-06-24
NO882805L NO882805L (no) 1988-12-27
NO170952B NO170952B (no) 1992-09-21
NO170952C true NO170952C (no) 1992-12-30

Family

ID=22069569

Family Applications (1)

Application Number Title Priority Date Filing Date
NO882805A NO170952C (no) 1987-06-26 1988-06-24 Anordning for aa feste et missil til en utskytningsenhet

Country Status (4)

Country Link
US (1) US4809929A (no)
EP (1) EP0296735B1 (no)
DE (1) DE3886106T2 (no)
NO (1) NO170952C (no)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6659396B1 (en) 2002-07-22 2003-12-09 The Boeing Company Arch wing and forward steering for an advanced air vehicle
GB2394029A (en) * 2002-09-03 2004-04-14 Bae Systems Plc Drag reduction devices for projectiles and the like
US8502126B2 (en) * 2010-05-27 2013-08-06 Raytheon Company System and method for navigating an object

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3695556A (en) * 1970-08-03 1972-10-03 Us Navy Hinged stability and control fin assembly
US3759466A (en) * 1972-01-10 1973-09-18 Us Army Cruise control for non-ballistic missiles by a special arrangement of spoilers
DE2342783C2 (de) * 1973-08-24 1983-12-22 Rheinmetall GmbH, 4000 Düsseldorf Mit einem Leitwerk versehenes Geschoß
US4411398A (en) * 1981-04-20 1983-10-25 General Dynamics, Pomona Division Double fabric retractable wing construction
US4709878A (en) * 1984-04-17 1987-12-01 British Aerospace Plc Fin assembly deployment spring

Also Published As

Publication number Publication date
EP0296735A3 (en) 1990-10-24
DE3886106D1 (de) 1994-01-20
EP0296735A2 (en) 1988-12-28
EP0296735B1 (en) 1993-12-08
DE3886106T2 (de) 1994-04-14
NO170952B (no) 1992-09-21
NO882805D0 (no) 1988-06-24
US4809929A (en) 1989-03-07
NO882805L (no) 1988-12-27

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Free format text: LAPSED IN DECEMBER 2003