CH370677A - Deployable stabilizer for projectile intended to be fired in a launch tube - Google Patents

Deployable stabilizer for projectile intended to be fired in a launch tube

Info

Publication number
CH370677A
CH370677A CH778961A CH778961A CH370677A CH 370677 A CH370677 A CH 370677A CH 778961 A CH778961 A CH 778961A CH 778961 A CH778961 A CH 778961A CH 370677 A CH370677 A CH 370677A
Authority
CH
Switzerland
Prior art keywords
fired
launch tube
projectile intended
deployable
stabilizer
Prior art date
Application number
CH778961A
Other languages
French (fr)
Original Assignee
Hotchkiss Brandt
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 Hotchkiss Brandt filed Critical Hotchkiss Brandt
Publication of CH370677A publication Critical patent/CH370677A/en

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
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • 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
    • F42B10/20—Stabilising 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

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Discharge By Other Means (AREA)
CH778961A 1960-07-11 1961-07-03 Deployable stabilizer for projectile intended to be fired in a launch tube CH370677A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR832688A FR1270054A (en) 1960-07-11 1960-07-11 Deployable tail for self-propelled projectile
FR865095A FR79945E (en) 1960-07-11 1961-06-15 Deployable tail for self-propelled projectile

Publications (1)

Publication Number Publication Date
CH370677A true CH370677A (en) 1963-07-15

Family

ID=26186750

Family Applications (1)

Application Number Title Priority Date Filing Date
CH778961A CH370677A (en) 1960-07-11 1961-07-03 Deployable stabilizer for projectile intended to be fired in a launch tube

Country Status (9)

Country Link
US (1) US3098446A (en)
BE (1) BE605677A (en)
CH (1) CH370677A (en)
DE (2) DE1183834B (en)
ES (1) ES269713A1 (en)
FI (1) FI41122B (en)
FR (2) FR1270054A (en)
GB (2) GB952960A (en)
NL (3) NL113679C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0572803A3 (en) * 1992-05-08 1994-05-11 Rockwell International Corp Self propelled underwater device with steerable fin stabilizer

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3196793A (en) * 1963-01-16 1965-07-27 Milenkovic Veljko Folded fin rocket
US5439188A (en) * 1964-09-04 1995-08-08 Hughes Missile Systems Company Control system
US3378216A (en) * 1966-04-29 1968-04-16 Susquehama Corp Integral fin canister-nozzle exit cone
CH480613A (en) * 1967-09-11 1969-10-31 Oerlikon Buehrle Ag Bullet with brake wings
US3690595A (en) * 1970-11-19 1972-09-12 Sarmac Sa Self-propelled, vaned missile
DE2264338A1 (en) * 1972-12-30 1974-07-04 Dynamit Nobel Ag FOLD-OUT TAIL, ESPECIALLY FOR MISSILE
FR2221707B1 (en) * 1973-03-14 1976-04-30 France Etat
US3986685A (en) * 1974-07-30 1976-10-19 The United States Of America As Represented By The Secretary Of The Army Folding tail fins
US3986684A (en) * 1974-07-30 1976-10-19 The United States Of America As Represented By The Secretary Of The Army Folding tail fins
US3946969A (en) * 1974-07-30 1976-03-30 The United States Of America As Represented By The Secretary Of The Army Folding tail fins
US3998407A (en) * 1974-07-30 1976-12-21 The United States Of America As Represented By The Secretary Of The Army Folding tail fins
US4523728A (en) * 1983-03-07 1985-06-18 Ford Aerospace & Communications Corporation Passive auto-erecting alignment wings for long rod penetrator
SE8406351L (en) * 1984-12-13 1986-04-21 Ffv Affersverket GUIDELINES FOR FENOR EXPOSURE OF PROJECTIL
DE3447852A1 (en) * 1984-12-31 1986-08-28 Heide, Marion, 4030 Ratingen FOLDING ASSEMBLY FOR WING-STABILIZED ROCKET BULLETS
GB2274904A (en) * 1993-02-05 1994-08-10 British Aerospace Deployable wing
US6559370B1 (en) * 2002-08-06 2003-05-06 The United States Of America As Represented By The Secretary Of The Navy Submarine countermeasure vehicle with folding propeller
FR2863045B1 (en) * 2003-11-27 2006-01-06 Giat Ind Sa DEVICE FOR SECURELY DEPLOYING THE FINS OF A PROJECTILE
US7083141B2 (en) * 2003-12-02 2006-08-01 Edward Nitenson Self-propelled projectile
KR101074028B1 (en) 2009-02-12 2011-10-17 국방과학연구소 Flying object with fixing device for the deployed wing
FR2946423A1 (en) * 2009-06-05 2010-12-10 Tda Armements Sas DEVICE FOR OPENING AND LOCKING A MUNITION STACK
RU2427788C1 (en) * 2010-01-11 2011-08-27 Вячеслав Тихонович Копанев Firing method of rocket missiles from launcher facilities of valley fire systems
CN113237393A (en) * 2021-04-28 2021-08-10 北京星途探索科技有限公司 High-precision stabilizing device
US11796291B2 (en) * 2022-01-11 2023-10-24 Raytheon Company Effector having morphing airframe and method

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR896502A (en) * 1940-09-23 1945-02-23 Commerciale Caproni Comp Device for controlling the fins of a projectile fitted with a tail unit
US2365577A (en) * 1943-08-26 1944-12-19 Stephen A Moore Projectile
BE565999A (en) * 1953-02-06
BE552288A (en) * 1953-10-20
LU33739A1 (en) * 1955-07-21
FR1187193A (en) * 1957-11-15 1959-09-08 Hotchkiss Brandt Deployable stabilizer for projectile
LU36192A1 (en) * 1958-05-22
NL106348C (en) * 1959-03-09

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0572803A3 (en) * 1992-05-08 1994-05-11 Rockwell International Corp Self propelled underwater device with steerable fin stabilizer

Also Published As

Publication number Publication date
GB952960A (en) 1964-03-18
NL113679C (en)
NL295319A (en)
GB945409A (en) 1963-12-23
ES269713A1 (en) 1962-01-01
NL266892A (en)
FR79945E (en) 1963-02-15
FR1270054A (en) 1961-08-25
US3098446A (en) 1963-07-23
DE1195204B (en) 1965-06-16
FI41122B (en) 1969-04-30
BE605677A (en) 1961-11-03
DE1183834B (en) 1964-12-17

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