FR1485580A - Advanced tail for rocket - Google Patents

Advanced tail for rocket

Info

Publication number
FR1485580A
FR1485580A FR53419A FR53419A FR1485580A FR 1485580 A FR1485580 A FR 1485580A FR 53419 A FR53419 A FR 53419A FR 53419 A FR53419 A FR 53419A FR 1485580 A FR1485580 A FR 1485580A
Authority
FR
France
Prior art keywords
rocket
advanced tail
tail
advanced
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
FR53419A
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.)
Hotchkiss Brandt SA
Original Assignee
Hotchkiss Brandt 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 Hotchkiss Brandt SA filed Critical Hotchkiss Brandt SA
Priority to FR53419A priority Critical patent/FR1485580A/en
Application granted granted Critical
Publication of FR1485580A publication Critical patent/FR1485580A/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

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
FR53419A 1966-03-15 1966-03-15 Advanced tail for rocket Expired FR1485580A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR53419A FR1485580A (en) 1966-03-15 1966-03-15 Advanced tail for rocket

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR53419A FR1485580A (en) 1966-03-15 1966-03-15 Advanced tail for rocket

Publications (1)

Publication Number Publication Date
FR1485580A true FR1485580A (en) 1967-06-23

Family

ID=8603763

Family Applications (1)

Application Number Title Priority Date Filing Date
FR53419A Expired FR1485580A (en) 1966-03-15 1966-03-15 Advanced tail for rocket

Country Status (1)

Country Link
FR (1) FR1485580A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1981000908A1 (en) * 1979-09-27 1981-04-02 K Andersson Projectile,adapted to be given a rotation on firing,which makes the projectile spin-stabilized
WO1988005898A1 (en) * 1987-02-02 1988-08-11 Eskam, Armin Finned projectile or missile
FR2655720A1 (en) * 1989-12-08 1991-06-14 Thomson Brandt Armements WING GALBEE DEPLOYABLE FOR FLYING ENGINE.
WO1995031689A1 (en) * 1994-05-13 1995-11-23 Hughes Aircraft Company Missile with deployable control fins
WO2006081226A1 (en) * 2005-01-26 2006-08-03 Raytheon Company Single-axis fin deployment system

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1981000908A1 (en) * 1979-09-27 1981-04-02 K Andersson Projectile,adapted to be given a rotation on firing,which makes the projectile spin-stabilized
US4546940A (en) * 1979-09-27 1985-10-15 Kurt Andersson Projectile, adapted to be given a rotation on firing, which makes the projectile spin-stabilized
WO1988005898A1 (en) * 1987-02-02 1988-08-11 Eskam, Armin Finned projectile or missile
FR2655720A1 (en) * 1989-12-08 1991-06-14 Thomson Brandt Armements WING GALBEE DEPLOYABLE FOR FLYING ENGINE.
WO1995031689A1 (en) * 1994-05-13 1995-11-23 Hughes Aircraft Company Missile with deployable control fins
WO2006081226A1 (en) * 2005-01-26 2006-08-03 Raytheon Company Single-axis fin deployment system
US7642492B2 (en) 2005-01-26 2010-01-05 Raytheon Company Single-axis fin deployment system

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