IT1002569B - IMPROVEMENT IN FLEECE FOR ROCKETS AND SIMILAR - Google Patents

IMPROVEMENT IN FLEECE FOR ROCKETS AND SIMILAR

Info

Publication number
IT1002569B
IT1002569B IT54663/73A IT5466373A IT1002569B IT 1002569 B IT1002569 B IT 1002569B IT 54663/73 A IT54663/73 A IT 54663/73A IT 5466373 A IT5466373 A IT 5466373A IT 1002569 B IT1002569 B IT 1002569B
Authority
IT
Italy
Prior art keywords
rockets
fleece
improvement
similar
Prior art date
Application number
IT54663/73A
Other languages
Italian (it)
Inventor
R Schoffl
Original Assignee
Dynamit Nobel Ag
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 Dynamit Nobel Ag filed Critical Dynamit Nobel Ag
Application granted granted Critical
Publication of IT1002569B publication Critical patent/IT1002569B/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/02Stabilising arrangements
    • F42B10/14Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/20Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel deployed by combustion gas pressure, or by pneumatic or hydraulic forces
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/02Stabilising arrangements
    • F42B10/14Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/18Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel using a longitudinally slidable support member

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Engines (AREA)
  • Toys (AREA)
IT54663/73A 1972-12-30 1973-12-28 IMPROVEMENT IN FLEECE FOR ROCKETS AND SIMILAR IT1002569B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2264338A DE2264338A1 (en) 1972-12-30 1972-12-30 FOLD-OUT TAIL, ESPECIALLY FOR MISSILE

Publications (1)

Publication Number Publication Date
IT1002569B true IT1002569B (en) 1976-05-20

Family

ID=5865891

Family Applications (1)

Application Number Title Priority Date Filing Date
IT54663/73A IT1002569B (en) 1972-12-30 1973-12-28 IMPROVEMENT IN FLEECE FOR ROCKETS AND SIMILAR

Country Status (4)

Country Link
US (1) US3861627A (en)
DE (1) DE2264338A1 (en)
FR (1) FR2212528B1 (en)
IT (1) IT1002569B (en)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE444612B (en) * 1984-12-13 1986-04-21 Ffv Affersverket GUIDELINES FOR FENOR EXPOSURE OF PROJECTIL
DE3712704A1 (en) * 1987-04-14 1988-11-03 Diehl Gmbh & Co MISSILE WITH FOLD-OUT WINGS
US5417139A (en) * 1993-10-01 1995-05-23 Unisys Corporation Delivery system and method for flexible array
FR2721702B1 (en) * 1994-06-28 1996-08-14 Luchaire Defense Sa Device for deploying a projectile fin.
US5671899A (en) * 1996-02-26 1997-09-30 Lockheed Martin Corporation Airborne vehicle with wing extension and roll control
US5927643A (en) * 1997-11-05 1999-07-27 Atlantic Research Corporation Self-deploying airfoil for missile or the like
US6224013B1 (en) * 1998-08-27 2001-05-01 Lockheed Martin Corporation Tail fin deployment device
DE19960738C1 (en) * 1999-12-16 2001-08-23 Lfk Gmbh Rudder connection for guided missiles
SE518656C2 (en) * 2000-07-03 2002-11-05 Bofors Defence Ab Fine stabilized artillery grenade
US7513454B2 (en) * 2003-09-05 2009-04-07 Selex Sensors And Airborne Systems Limited Drag-producing devices
US7262394B2 (en) * 2004-03-05 2007-08-28 The Boeing Company Mortar shell ring tail and associated method
US7475846B2 (en) * 2005-10-05 2009-01-13 General Dynamics Ordnance And Tactical Systems, Inc. Fin retention and deployment mechanism
ES2532733T3 (en) * 2009-07-31 2015-03-31 Raytheon Company Folding fairing and method to reduce aerodynamic drag in an artillery projectile launched by cannon
US8754352B2 (en) * 2010-04-07 2014-06-17 Bae Systems Information And Electronic Systems Integration Inc. Compression spring wing deployment initiator
CN104833276B (en) * 2015-05-18 2016-09-14 中国船舶重工集团公司第七○二研究所 Lattice fin synchronous expansion mechanism
CN105424314B (en) * 2015-12-18 2018-02-09 中国航天空气动力技术研究院 Free flight model rudder face deploys flow tunnel testing device
CN107421403A (en) * 2017-09-20 2017-12-01 成都云鼎智控科技有限公司 A kind of more bar coordinated type fold mechanisms for longitudinal folding missile wing
CN109141143A (en) * 2018-07-26 2019-01-04 重庆长安工业(集团)有限责任公司 A kind of folded surface locking mechanism
CN109696088B (en) * 2018-12-07 2021-06-08 上海机电工程研究所 Compact missile wing contraction and expansion mechanism and missile
US11340052B2 (en) 2019-08-27 2022-05-24 Bae Systems Information And Electronic Systems Integration Inc. Wing deployment initiator and locking mechanism
CN110906807B (en) * 2019-12-13 2021-11-16 北京中科宇航探索技术有限公司 Embedded pneumatic control surface for rocket
US11852211B2 (en) 2020-09-10 2023-12-26 Bae Systems Information And Electronic Systems Integration Inc. Additively manufactured elliptical bifurcating torsion spring
CN114216647B (en) * 2021-12-16 2024-06-14 中国航天空气动力技术研究院 A rudder wing transient extension and retraction device for wind tunnel test

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1187193A (en) * 1957-11-15 1959-09-08 Hotchkiss Brandt Deployable stabilizer for projectile
NL266892A (en) * 1960-07-11
FR1418696A (en) * 1963-12-28 1965-11-19 Breda Mecc Bresciana Folding wing rudder for rockets
CH493819A (en) * 1968-07-11 1970-07-15 Oerlikon Buehrle Ag Twist-free projectile with launch tube
DE1906028C3 (en) * 1969-02-07 1973-12-06 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Tail unit for projectiles and missiles with a device for moving the fins of the tail unit into their effective position

Also Published As

Publication number Publication date
US3861627A (en) 1975-01-21
DE2264338A1 (en) 1974-07-04
FR2212528B1 (en) 1977-08-19
FR2212528A1 (en) 1974-07-26

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