FR1418696A - Gouvernail à ailettes pliantes pour fusées - Google Patents

Gouvernail à ailettes pliantes pour fusées

Info

Publication number
FR1418696A
FR1418696A FR999953A FR999953A FR1418696A FR 1418696 A FR1418696 A FR 1418696A FR 999953 A FR999953 A FR 999953A FR 999953 A FR999953 A FR 999953A FR 1418696 A FR1418696 A FR 1418696A
Authority
FR
France
Prior art keywords
rockets
folding wing
wing rudder
rudder
folding
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
FR999953A
Other languages
English (en)
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.)
Breda Meccanica Bresciana SpA
Original Assignee
Breda Meccanica Bresciana SpA
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 Breda Meccanica Bresciana SpA filed Critical Breda Meccanica Bresciana SpA
Priority to FR999953A priority Critical patent/FR1418696A/fr
Application granted granted Critical
Publication of FR1418696A publication Critical patent/FR1418696A/fr
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/02Stabilising arrangements
    • F42B10/14Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/18Stabilising 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)
FR999953A 1963-12-28 1964-12-24 Gouvernail à ailettes pliantes pour fusées Expired FR1418696A (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR999953A FR1418696A (fr) 1963-12-28 1964-12-24 Gouvernail à ailettes pliantes pour fusées

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IT2663163 1963-12-28
FR999953A FR1418696A (fr) 1963-12-28 1964-12-24 Gouvernail à ailettes pliantes pour fusées

Publications (1)

Publication Number Publication Date
FR1418696A true FR1418696A (fr) 1965-11-19

Family

ID=26212051

Family Applications (1)

Application Number Title Priority Date Filing Date
FR999953A Expired FR1418696A (fr) 1963-12-28 1964-12-24 Gouvernail à ailettes pliantes pour fusées

Country Status (1)

Country Link
FR (1) FR1418696A (fr)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2175133A1 (fr) * 1972-03-08 1973-10-19 Sarmag Sa
US3819132A (en) * 1973-02-21 1974-06-25 Sarmac Sa Self propelled projectile with fins
FR2212528A1 (fr) * 1972-12-30 1974-07-26 Dynamit Nobel Ag
US3946969A (en) * 1974-07-30 1976-03-30 The United States Of America As Represented By The Secretary Of The Army Folding tail fins
US3952970A (en) * 1974-08-28 1976-04-27 The United States Of America As Represented By The Secretary Of The Navy Means for improving rocket missile accuracy
FR3037390A1 (fr) * 2015-06-09 2016-12-16 Nexter Munitions Dispositif de stabilisation et projectile equipe d'un tel dispositif
CN109141143A (zh) * 2018-07-26 2019-01-04 重庆长安工业(集团)有限责任公司 一种折叠翼面卡锁机构
CN113804066A (zh) * 2021-09-18 2021-12-17 天津爱思达航天科技有限公司 一种带有同步旋转折叠翼的尾舱结构
CN114278465A (zh) * 2021-12-03 2022-04-05 西北工业大学太仓长三角研究院 一种具有可调式稳定尾翼的微小型火箭推进装置

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2175133A1 (fr) * 1972-03-08 1973-10-19 Sarmag Sa
FR2212528A1 (fr) * 1972-12-30 1974-07-26 Dynamit Nobel Ag
US3819132A (en) * 1973-02-21 1974-06-25 Sarmac Sa Self propelled projectile with 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
US3952970A (en) * 1974-08-28 1976-04-27 The United States Of America As Represented By The Secretary Of The Navy Means for improving rocket missile accuracy
FR3037390A1 (fr) * 2015-06-09 2016-12-16 Nexter Munitions Dispositif de stabilisation et projectile equipe d'un tel dispositif
CN109141143A (zh) * 2018-07-26 2019-01-04 重庆长安工业(集团)有限责任公司 一种折叠翼面卡锁机构
CN113804066A (zh) * 2021-09-18 2021-12-17 天津爱思达航天科技有限公司 一种带有同步旋转折叠翼的尾舱结构
CN114278465A (zh) * 2021-12-03 2022-04-05 西北工业大学太仓长三角研究院 一种具有可调式稳定尾翼的微小型火箭推进装置

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