CH332850A - Self-propelled projectile with retractable tail - Google Patents

Self-propelled projectile with retractable tail

Info

Publication number
CH332850A
CH332850A CH332850DA CH332850A CH 332850 A CH332850 A CH 332850A CH 332850D A CH332850D A CH 332850DA CH 332850 A CH332850 A CH 332850A
Authority
CH
Switzerland
Prior art keywords
self
propelled projectile
retractable tail
retractable
tail
Prior art date
Application number
Other languages
French (fr)
Original Assignee
Brevets Aero Mecaniques
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 Brevets Aero Mecaniques filed Critical Brevets Aero Mecaniques
Publication of CH332850A publication Critical patent/CH332850A/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
    • F42B10/18—Stabilising 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)
  • Toys (AREA)
CH332850D 1955-07-21 1956-07-07 Self-propelled projectile with retractable tail CH332850A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
LU332850X 1955-07-21

Publications (1)

Publication Number Publication Date
CH332850A true CH332850A (en) 1958-09-30

Family

ID=19732594

Family Applications (1)

Application Number Title Priority Date Filing Date
CH332850D CH332850A (en) 1955-07-21 1956-07-07 Self-propelled projectile with retractable tail

Country Status (4)

Country Link
CH (1) CH332850A (en)
DE (1) DE1027561B (en)
FR (1) FR1155665A (en)
LU (1) LU33739A1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1191519A (en) * 1958-02-13 1959-10-20 Hotchkiss Brandt Deploying tail for artillery projectile
NL295319A (en) * 1960-07-11
SE433882B (en) * 1979-10-09 1984-06-18 Bofors Ab FALL-OUT FINE FOR A WINDOW STABILIZED AMMUNITION UNIT IN THE FORM OF A GRANATE
DE3328520C1 (en) * 1983-08-06 1985-03-07 Diehl GmbH & Co, 8500 Nürnberg Tailplane for missiles
FR2812936A1 (en) * 1986-08-12 2002-02-15 Aerospatiale Missile with variable wing configuration has moving wings extending from slots in hollow fixed wings on missile body
DE102008007432A1 (en) * 2008-02-01 2009-08-06 Deutsch Französisches Forschungsinstitut Saint Louis Spin-stabilized projectile, has mass element locked with stop element in prestressed position to form nose-lateral stop for mass element, so that spring force of spring moves mass element from drilling while decreasing acceleration

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR502394A (en) * 1915-07-17 1920-05-12 Louis Vincent Montesino Flying shell
FR715385A (en) * 1931-08-10 1931-12-02 Folding tail for aviation bombs
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
GB634090A (en) * 1946-07-15 1950-03-15 William Alexander Onslow Marti Improvements in and connected with stabilizing fins for projectiles

Also Published As

Publication number Publication date
FR1155665A (en) 1958-05-07
LU33739A1 (en)
DE1027561B (en) 1958-04-03

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