SE8306496L - Improvements in missile and other fuselages - Google Patents

Improvements in missile and other fuselages

Info

Publication number
SE8306496L
SE8306496L SE8306496A SE8306496A SE8306496L SE 8306496 L SE8306496 L SE 8306496L SE 8306496 A SE8306496 A SE 8306496A SE 8306496 A SE8306496 A SE 8306496A SE 8306496 L SE8306496 L SE 8306496L
Authority
SE
Sweden
Prior art keywords
missile
fuselages
symmetricaly
strakes
fuselage
Prior art date
Application number
SE8306496A
Other languages
Unknown language ( )
English (en)
Other versions
SE467206B (sv
SE8306496D0 (sv
Inventor
D H Peckham
Original Assignee
Secr Defence Brit
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 Secr Defence Brit filed Critical Secr Defence Brit
Publication of SE8306496D0 publication Critical patent/SE8306496D0/sv
Publication of SE8306496L publication Critical patent/SE8306496L/sv
Publication of SE467206B publication Critical patent/SE467206B/sv

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
    • F42B10/02—Stabilising arrangements
    • F42B10/04—Stabilising arrangements using fixed fins

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)
  • Toys (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
SE8306496A 1982-11-26 1983-11-24 Flytkropp med ett roterbart nosparti foersedd med fenor SE467206B (sv)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8233864 1982-11-26

Publications (3)

Publication Number Publication Date
SE8306496D0 SE8306496D0 (sv) 1983-11-24
SE8306496L true SE8306496L (sv) 1991-11-22
SE467206B SE467206B (sv) 1992-06-15

Family

ID=10534568

Family Applications (1)

Application Number Title Priority Date Filing Date
SE8306496A SE467206B (sv) 1982-11-26 1983-11-24 Flytkropp med ett roterbart nosparti foersedd med fenor

Country Status (7)

Country Link
US (1) US5139215A (sv)
CA (1) CA1314764C (sv)
DE (1) DE3342861A1 (sv)
FR (1) FR2666786B1 (sv)
GB (1) GB2244968B (sv)
IT (1) IT1235222B (sv)
SE (1) SE467206B (sv)

Families Citing this family (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5322243A (en) * 1992-06-25 1994-06-21 Northrop Corporation Separately banking maneuvering aerodynamic control surfaces, system and method
US5271579A (en) * 1992-07-10 1993-12-21 Luca Nicholas J De Recreational and sport rocket construction
US5417393A (en) * 1993-04-27 1995-05-23 Hughes Aircraft Company Rotationally mounted flexible band wing
DE4337850A1 (de) * 1993-11-05 1995-05-18 Fritz Hausser Flugkörper die an der vorderen Seite die Seitenruder, Querruder und Höhenruder plaziert haben als einzige oder als Verstärkung der hinteren Ruder
US5449131A (en) * 1994-01-28 1995-09-12 Eidetics International, Inc. Vertical nose strake for aircraft stability and control
US5794887A (en) * 1995-11-17 1998-08-18 Komerath; Narayanan M. Stagnation point vortex controller
DE19837800C2 (de) * 1998-08-20 2000-06-21 Daimler Chrysler Ag Rumpfnase zur Steuerung von Fluggeräten
AUPR583001A0 (en) * 2001-06-20 2001-07-12 Kusic, Tom Aircraft spiralling mechanism
US7637453B2 (en) * 2001-06-22 2009-12-29 Tom Kusic Aircraft spiraling mechanism with jet assistance - A
US7165742B2 (en) * 2001-06-22 2007-01-23 Tom Kusic Aircraft spiralling mechanism - B
US7635104B1 (en) * 2001-06-22 2009-12-22 Tom Kusic Aircraft spiraling mechanism with jet assistance—B
US7093791B2 (en) * 2001-06-22 2006-08-22 Tom Kusic Aircraft spiralling mechanism—c
AUPR982702A0 (en) 2002-01-03 2002-01-31 Pax Fluid Systems Inc. Vortex ring generator to reduce drag on a fuselage
AUPR982502A0 (en) * 2002-01-03 2002-01-31 Pax Fluid Systems Inc. A heat exchanger
AUPR982302A0 (en) * 2002-01-03 2002-01-31 Pax Fluid Systems Inc. A fluid flow controller
AU2003201182B2 (en) * 2002-01-03 2008-05-01 Pax Scientific, Inc. Vortex ring generator
US6796532B2 (en) * 2002-12-20 2004-09-28 Norman D. Malmuth Surface plasma discharge for controlling forebody vortex asymmetry
US6685143B1 (en) * 2003-01-03 2004-02-03 Orbital Research Inc. Aircraft and missile forebody flow control device and method of controlling flow
AU2003903386A0 (en) * 2003-07-02 2003-07-17 Pax Scientific, Inc Fluid flow control device
CA2544516C (en) * 2003-11-04 2014-04-29 Pax Scientific, Inc. Fluid circulation system
CA2554808A1 (en) 2004-01-30 2005-08-11 Pax Scientific, Inc. Housing for a centrifugal fan, pump or turbine
CN1985093A (zh) * 2004-01-30 2007-06-20 百思科技公司 用于离心通风机、泵或涡轮机的机罩
USD570996S1 (en) 2006-09-25 2008-06-10 Pax Scientific, Inc. Rotor
US8328522B2 (en) 2006-09-29 2012-12-11 Pax Scientific, Inc. Axial flow fan
USD570999S1 (en) 2006-11-22 2008-06-10 Pax Scientific, Inc. Rotor
US7963442B2 (en) * 2006-12-14 2011-06-21 Simmonds Precision Products, Inc. Spin stabilized projectile trajectory control
US7642491B2 (en) * 2007-03-19 2010-01-05 Tom Kusic Aircraft spiraling mechanism with jet assistance—D
GB0803282D0 (en) 2008-02-22 2008-04-02 Qinetiq Ltd Control of projectiles or the like
US20090308472A1 (en) * 2008-06-15 2009-12-17 Jayden David Harman Swirl Inducer
WO2015198093A1 (en) * 2014-06-24 2015-12-30 Peter Ireland Efficiency improvements for flow control body and system shocks
USD729896S1 (en) 2013-12-19 2015-05-19 Elio Martinez Air vehicle rotatable wind-driven sleeve
US9857154B2 (en) * 2014-07-30 2018-01-02 The United States Of America As Represented By The Secretary Of The Army Steerable munitions projectile

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR522506A (fr) * 1918-06-19 1921-08-01 Gaston Charrasse Système de cone de pénétration placé à l'extrémité antérieure des obus employés par les canons à grande portée et ne participant pas au mouvement de rotation de l'obus
US2747816A (en) * 1950-05-11 1956-05-29 Ben O Howard Canard type airplane and controls therefor
BE552464A (sv) * 1955-11-10
US3196794A (en) * 1959-06-18 1965-07-27 Robert C Meade Piezo-electric fuse device
US3067681A (en) * 1960-01-04 1962-12-11 Telecomputing Corp Guided missile
DE1149641B (de) * 1960-06-08 1963-05-30 Pye Ltd Gelenktes Geschoss
US3195462A (en) * 1961-05-17 1965-07-20 Aerojet General Co Pull rocket shroud
US3262655A (en) * 1963-12-26 1966-07-26 Jr Warren Gillespie Alleviation of divergence during rocket launch
SE381016B (sv) * 1973-05-04 1975-11-24 S E Larson Inbordes geometrisk placering av nosvinge och huvudvinge vid flygplan eller annan farkost
IL46548A (en) * 1975-02-03 1978-06-15 Drori Mordeki Stabilized projectile with pivotable fins
US4176813A (en) * 1977-10-05 1979-12-04 Northrop Corporation Shark nose for aircraft
GB2019335A (en) * 1978-03-01 1979-10-31 Bristol Aerojet Ltd Rocket vehicles
US4198016A (en) * 1978-06-12 1980-04-15 The United States Of America As Represented By The Secretary Of The Navy Floating canard with geared tab
US4378922A (en) * 1980-04-18 1983-04-05 The Secretary Of State For Defence In Her Brittannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland Aircraft having improved strake configuration
US4373688A (en) * 1981-01-19 1983-02-15 The United States Of America As Represented By The Secretary Of The Army Canard drive mechanism latch for guided projectile

Also Published As

Publication number Publication date
FR2666786A1 (fr) 1992-03-20
SE467206B (sv) 1992-06-15
SE8306496D0 (sv) 1983-11-24
FR2666786B1 (fr) 1995-05-12
IT1235222B (it) 1992-06-26
DE3342861A1 (de) 1992-05-07
IT8349374A0 (it) 1983-11-22
US5139215A (en) 1992-08-18
GB2244968B (en) 1992-05-13
CA1314764C (en) 1993-03-23
GB2244968A (en) 1991-12-18

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