IT7867752A0 - Dispositivo per conferire un motodi rotazione ad un proietto durante il lancio - Google Patents

Dispositivo per conferire un motodi rotazione ad un proietto durante il lancio

Info

Publication number
IT7867752A0
IT7867752A0 IT7867752A IT6775278A IT7867752A0 IT 7867752 A0 IT7867752 A0 IT 7867752A0 IT 7867752 A IT7867752 A IT 7867752A IT 6775278 A IT6775278 A IT 6775278A IT 7867752 A0 IT7867752 A0 IT 7867752A0
Authority
IT
Italy
Prior art keywords
giving
motion
rotation
during launch
project during
Prior art date
Application number
IT7867752A
Other languages
English (en)
Other versions
IT1156944B (it
Inventor
Detalle Bernard
Original Assignee
Europ Propulsion
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 Europ Propulsion filed Critical Europ Propulsion
Publication of IT7867752A0 publication Critical patent/IT7867752A0/it
Application granted granted Critical
Publication of IT1156944B publication Critical patent/IT1156944B/it

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
    • F42B10/26—Stabilising arrangements using spin
    • F42B10/28—Stabilising arrangements using spin induced by gas action
    • F42B10/30—Stabilising arrangements using spin induced by gas action using rocket motor nozzles

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Nozzles (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
IT67752/78A 1977-04-21 1978-04-05 Dispositivo per conferire un moto di rotazione ad un proietto durante il lancio IT1156944B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7712070A FR2388243A1 (fr) 1977-04-21 1977-04-21 Dispositif pour conferer un mouvement de rotation a un engin lors de son lancement

Publications (2)

Publication Number Publication Date
IT7867752A0 true IT7867752A0 (it) 1978-04-05
IT1156944B IT1156944B (it) 1987-02-04

Family

ID=9189744

Family Applications (1)

Application Number Title Priority Date Filing Date
IT67752/78A IT1156944B (it) 1977-04-21 1978-04-05 Dispositivo per conferire un moto di rotazione ad un proietto durante il lancio

Country Status (7)

Country Link
US (1) US4194706A (it)
JP (1) JPS53130900A (it)
CA (1) CA1104877A (it)
DE (1) DE2813645A1 (it)
FR (1) FR2388243A1 (it)
GB (1) GB1603944A (it)
IT (1) IT1156944B (it)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4307651A (en) * 1979-09-04 1981-12-29 The United States Of America As Represented By The Secretary Of The Army Rocket in-tube spin device and rear sabot
US4497460A (en) * 1983-03-25 1985-02-05 The United States Of America As Represented By The Secretary Of The Navy Erodale spin turbine for tube-launched missiles
US5078336A (en) * 1989-07-21 1992-01-07 Carter Gregory E Spin-stabilized missile with plug nozzle
GB9925193D0 (en) * 1999-10-26 1999-12-22 Rolls Royce Plc Gas turbine engine exhaust nozzle
US6612106B2 (en) 2000-05-05 2003-09-02 The Boeing Company Segmented mixing device having chevrons for exhaust noise reduction in jet engines
US6676072B1 (en) 2002-11-13 2004-01-13 Steven S. Kim Short duration, high-torque rocket nozzle
US6691948B1 (en) * 2003-04-10 2004-02-17 The United States Of America As Represented By The Secretary Of The Navy High torque rocket nozzle
EP2297544B1 (en) * 2008-05-21 2017-06-21 Raytheon Company Integral thrust vector and roll control system
US8581160B1 (en) 2010-03-31 2013-11-12 The United States Of America As Represented By The Secretary Of The Navy Gyroscopic stabilizer
JP7369505B2 (ja) * 2019-12-03 2023-10-26 株式会社Ｉｈｉエアロスペース 推進装置

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US308944A (en) * 1884-12-09 bartlett
US1141042A (en) * 1913-09-30 1915-05-25 Ordnance Dev Company Contour-base for projectiles.
NL106348C (it) * 1959-03-09
US3430900A (en) * 1967-06-29 1969-03-04 United Aircraft Corp Tube launched rocket with detaching spin vanes
US3862603A (en) * 1972-11-21 1975-01-28 Us Navy Light weight sabot

Also Published As

Publication number Publication date
FR2388243A1 (fr) 1978-11-17
IT1156944B (it) 1987-02-04
GB1603944A (en) 1981-12-02
DE2813645A1 (de) 1978-10-26
US4194706A (en) 1980-03-25
FR2388243B1 (it) 1981-01-16
JPS53130900A (en) 1978-11-15
CA1104877A (en) 1981-07-14

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