DE1925055C3 - Flugkörper mit mindestens einer schwenkbar gelagerten Leitflache - Google Patents

Flugkörper mit mindestens einer schwenkbar gelagerten Leitflache

Info

Publication number
DE1925055C3
DE1925055C3 DE1925055A DE1925055A DE1925055C3 DE 1925055 C3 DE1925055 C3 DE 1925055C3 DE 1925055 A DE1925055 A DE 1925055A DE 1925055 A DE1925055 A DE 1925055A DE 1925055 C3 DE1925055 C3 DE 1925055C3
Authority
DE
Germany
Prior art keywords
missile
ball
guide surface
guide surfaces
shaft
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
DE1925055A
Other languages
German (de)
English (en)
Other versions
DE1925055A1 (de
DE1925055B2 (OSRAM
Inventor
William F. Inglewood Calif. Alexander (V.St.A.)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Co
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 DE1925055A1 publication Critical patent/DE1925055A1/de
Publication of DE1925055B2 publication Critical patent/DE1925055B2/de
Application granted granted Critical
Publication of DE1925055C3 publication Critical patent/DE1925055C3/de
Expired legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B26/00—Optical devices or arrangements for the control of light using movable or deformable optical elements
    • G02B26/08—Optical devices or arrangements for the control of light using movable or deformable optical elements for controlling the direction of light
    • G02B26/10—Scanning systems
    • G02B26/105—Scanning systems with one or more pivoting mirrors or galvano-mirrors
    • 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
    • F42B10/02—Stabilising arrangements
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Optics & Photonics (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)
  • Pivots And Pivotal Connections (AREA)
  • Transmission Devices (AREA)
DE1925055A 1968-05-23 1969-05-16 Flugkörper mit mindestens einer schwenkbar gelagerten Leitflache Expired DE1925055C3 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US73166168A 1968-05-23 1968-05-23

Publications (3)

Publication Number Publication Date
DE1925055A1 DE1925055A1 (de) 1970-09-24
DE1925055B2 DE1925055B2 (OSRAM) 1975-04-10
DE1925055C3 true DE1925055C3 (de) 1975-11-20

Family

ID=24940456

Family Applications (1)

Application Number Title Priority Date Filing Date
DE1925055A Expired DE1925055C3 (de) 1968-05-23 1969-05-16 Flugkörper mit mindestens einer schwenkbar gelagerten Leitflache

Country Status (6)

Country Link
US (1) US3515360A (OSRAM)
JP (1) JPS4817039B1 (OSRAM)
BE (1) BE732786A (OSRAM)
DE (1) DE1925055C3 (OSRAM)
NL (1) NL143338B (OSRAM)
SE (1) SE341709B (OSRAM)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3790104A (en) * 1973-03-12 1974-02-05 Us Navy High/low aspect ratio dual-mode fin design
US4655420A (en) * 1983-06-09 1987-04-07 The United States Of America As Represented By The Secretary Of The Air Force Low height fin control actuator
DE3441533A1 (de) * 1984-11-14 1986-05-15 Diehl GmbH & Co, 8500 Nürnberg Kopplungseinrichtung zwischen einem linear-stellglied und einem schwenkelement, insbesondere einem steuerruder
DE19827278A1 (de) * 1998-06-19 1999-12-23 Diehl Stiftung & Co Lenkbarer Flugkörper
US7083140B1 (en) * 2004-09-14 2006-08-01 The United States Of America As Represented By The Secretary Of The Army Full-bore artillery projectile fin development device and method
JP5626768B2 (ja) * 2010-05-28 2014-11-19 株式会社Ｉｈｉエアロスペース 飛翔体
US8946607B2 (en) * 2011-12-13 2015-02-03 The Boeing Company Mechanisms for deploying and actuating airfoil-shaped bodies on unmanned aerial vehicles

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1121616A (en) * 1914-06-19 1914-12-22 Paul Drocar Parachute.
US1277225A (en) * 1918-05-18 1918-08-27 Hans Lauesen Self-steering bomb.
US2465401A (en) * 1943-09-23 1949-03-29 Leslie A Skinner Rocket fin assembly
US3273500A (en) * 1965-01-25 1966-09-20 Kongelbeck Sverre Self-erecting folding fin

Also Published As

Publication number Publication date
JPS4817039B1 (OSRAM) 1973-05-26
SE341709B (OSRAM) 1972-01-10
NL6907893A (OSRAM) 1969-11-25
NL143338B (nl) 1974-09-16
DE1925055A1 (de) 1970-09-24
BE732786A (OSRAM) 1969-10-16
US3515360A (en) 1970-06-02
DE1925055B2 (OSRAM) 1975-04-10

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Legal Events

Date Code Title Description
SH Request for examination between 03.10.1968 and 22.04.1971
C3 Grant after two publication steps (3rd publication)
E77 Valid patent as to the heymanns-index 1977