FR1155665A - Improvements made to self-propelled projectiles, in particular rockets, with retractable tail - Google Patents

Improvements made to self-propelled projectiles, in particular rockets, with retractable tail

Info

Publication number
FR1155665A
FR1155665A FR1155665DA FR1155665A FR 1155665 A FR1155665 A FR 1155665A FR 1155665D A FR1155665D A FR 1155665DA FR 1155665 A FR1155665 A FR 1155665A
Authority
FR
France
Prior art keywords
self
improvements made
retractable tail
propelled projectiles
particular rockets
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
Other languages
French (fr)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Brevets Aero Mecaniques SA
Original Assignee
Brevets Aero Mecaniques SA
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 SA filed Critical Brevets Aero Mecaniques SA
Application granted granted Critical
Publication of FR1155665A publication Critical patent/FR1155665A/en
Expired legal-status Critical Current

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)
FR1155665D 1955-07-21 1956-07-19 Improvements made to self-propelled projectiles, in particular rockets, with retractable tail Expired FR1155665A (en)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
FR1155665A true FR1155665A (en) 1958-05-07

Family

ID=19732594

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1155665D Expired FR1155665A (en) 1955-07-21 1956-07-19 Improvements made to self-propelled projectiles, in particular rockets, with retractable tail

Country Status (4)

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

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3031967A (en) * 1958-02-13 1962-05-01 Hotchkiss Brandt Fin arrangement for projectiles
DE1183834B (en) * 1960-07-11 1964-12-17 Hotchkiss Brandt Fa Stabilizing wing arrangement for a missile projectile
FR2510739A1 (en) * 1979-10-09 1983-02-04 Bofors Ab DEPLOYABLE STABILIZER FIN FOR PROJECTILE

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3031967A (en) * 1958-02-13 1962-05-01 Hotchkiss Brandt Fin arrangement for projectiles
DE1183834B (en) * 1960-07-11 1964-12-17 Hotchkiss Brandt Fa Stabilizing wing arrangement for a missile projectile
DE1195204B (en) * 1960-07-11 1965-06-16 Hotchkiss Brandt Fa Opening device for the stabilizing wing of a projectile
FR2510739A1 (en) * 1979-10-09 1983-02-04 Bofors Ab DEPLOYABLE STABILIZER FIN FOR PROJECTILE

Also Published As

Publication number Publication date
LU33739A1 (en)
CH332850A (en) 1958-09-30
DE1027561B (en) 1958-04-03

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