CH385678A - Rocket projectile with spreading tail - Google Patents

Rocket projectile with spreading tail

Info

Publication number
CH385678A
CH385678A CH846761A CH846761A CH385678A CH 385678 A CH385678 A CH 385678A CH 846761 A CH846761 A CH 846761A CH 846761 A CH846761 A CH 846761A CH 385678 A CH385678 A CH 385678A
Authority
CH
Switzerland
Prior art keywords
rocket projectile
spreading
tail
spreading tail
rocket
Prior art date
Application number
CH846761A
Other languages
German (de)
Inventor
Apotheloz Robert
Original Assignee
Oerlikon Buehrle 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 Oerlikon Buehrle Ag filed Critical Oerlikon Buehrle Ag
Priority to CH846761A priority Critical patent/CH385678A/en
Priority to DEV21119A priority patent/DE1148913B/en
Priority to FR903152A priority patent/FR1329159A/en
Priority to GB26862/62A priority patent/GB968639A/en
Priority to FI1348/62A priority patent/FI41125B/fi
Priority to US210115A priority patent/US3174430A/en
Publication of CH385678A publication Critical patent/CH385678A/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
    • 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)
  • Testing Of Engines (AREA)
CH846761A 1961-07-19 1961-07-19 Rocket projectile with spreading tail CH385678A (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
CH846761A CH385678A (en) 1961-07-19 1961-07-19 Rocket projectile with spreading tail
DEV21119A DE1148913B (en) 1961-07-19 1961-08-02 Rocket projectile with spreading tail
FR903152A FR1329159A (en) 1961-07-19 1962-07-06 Rocket projectile with deployable tail
GB26862/62A GB968639A (en) 1961-07-19 1962-07-12 Rocket projectile
FI1348/62A FI41125B (en) 1961-07-19 1962-07-13
US210115A US3174430A (en) 1961-07-19 1962-07-16 Rocket projectile with spreadable empennage

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH846761A CH385678A (en) 1961-07-19 1961-07-19 Rocket projectile with spreading tail

Publications (1)

Publication Number Publication Date
CH385678A true CH385678A (en) 1964-12-15

Family

ID=4340821

Family Applications (1)

Application Number Title Priority Date Filing Date
CH846761A CH385678A (en) 1961-07-19 1961-07-19 Rocket projectile with spreading tail

Country Status (5)

Country Link
US (1) US3174430A (en)
CH (1) CH385678A (en)
DE (1) DE1148913B (en)
FI (1) FI41125B (en)
GB (1) GB968639A (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH480612A (en) * 1967-09-06 1969-10-31 Oerlikon Buehrle Ag Rocket with folding tail and braking device
US4175720A (en) * 1978-04-05 1979-11-27 The United States Of America As Represented By The Secretary Of The Navy Retainer/release mechanism for use on fin stabilized gun fired projectiles
US4523728A (en) * 1983-03-07 1985-06-18 Ford Aerospace & Communications Corporation Passive auto-erecting alignment wings for long rod penetrator
DE3721512C1 (en) * 1987-06-30 1989-03-30 Diehl Gmbh & Co Missile with over-caliber tail unit
CN106640893A (en) * 2016-12-18 2017-05-10 内蒙古航天红峡化工有限公司 Guide pin for assembling jet pipe of solid rocket engine

Family Cites Families (5)

* 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
GB634090A (en) * 1946-07-15 1950-03-15 William Alexander Onslow Marti Improvements in and connected with stabilizing fins for projectiles
US2773424A (en) * 1951-06-01 1956-12-11 Mordica O Johnston Gun perforator
BE565999A (en) * 1953-02-06
FR896562A (en) * 1958-12-23 1945-02-26 Electrical connection by plug with pressure connection springs

Also Published As

Publication number Publication date
US3174430A (en) 1965-03-23
DE1148913B (en) 1963-05-16
FI41125B (en) 1969-04-30
GB968639A (en) 1964-09-02

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