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FR1426963A - Perfectionnements apportés aux missiles - Google Patents

Perfectionnements apportés aux missiles

Info

Publication number
FR1426963A
FR1426963A FR989351A FR989351A FR1426963A FR 1426963 A FR1426963 A FR 1426963A FR 989351 A FR989351 A FR 989351A FR 989351 A FR989351 A FR 989351A FR 1426963 A FR1426963 A FR 1426963A
Authority
FR
France
Prior art keywords
missiles
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
FR989351A
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.)
Hawker Siddeley Dynamics Ltd
Original Assignee
Hawker Siddeley Dynamics Ltd
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 Hawker Siddeley Dynamics Ltd filed Critical Hawker Siddeley Dynamics Ltd
Priority to FR989351A priority Critical patent/FR1426963A/fr
Application granted granted Critical
Publication of FR1426963A publication Critical patent/FR1426963A/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
    • F42B10/60Steering arrangements
    • F42B10/66Steering by varying intensity or direction of thrust
    • F42B10/663Steering by varying intensity or direction of thrust using a plurality of transversally acting auxiliary nozzles, which are opened or closed by valves

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
FR989351A 1964-09-25 1964-09-25 Perfectionnements apportés aux missiles Expired FR1426963A (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR989351A FR1426963A (fr) 1964-09-25 1964-09-25 Perfectionnements apportés aux missiles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR989351A FR1426963A (fr) 1964-09-25 1964-09-25 Perfectionnements apportés aux missiles

Publications (1)

Publication Number Publication Date
FR1426963A true FR1426963A (fr) 1966-02-04

Family

ID=8839087

Family Applications (1)

Application Number Title Priority Date Filing Date
FR989351A Expired FR1426963A (fr) 1964-09-25 1964-09-25 Perfectionnements apportés aux missiles

Country Status (1)

Country Link
FR (1) FR1426963A (fr)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1984002974A1 (fr) * 1983-01-19 1984-08-02 Ford Motor Co Systeme de commande a air sous pression dynamique pour missiles teleguides
WO1984002975A1 (fr) * 1983-01-20 1984-08-02 Ford Aerospace & Communication Systeme de guidage par combustion d'air sous pression dynamique
US4685639A (en) * 1985-12-23 1987-08-11 Ford Aerospace & Communications Corp. Pneumatically actuated ram air steering system for a guided missile
EP0725259A1 (fr) * 1995-02-03 1996-08-07 Tda Armements S.A.S. ContrÔle d'un projectile par impulseur multi-chambre et mono-tuyère

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1984002974A1 (fr) * 1983-01-19 1984-08-02 Ford Motor Co Systeme de commande a air sous pression dynamique pour missiles teleguides
US4522357A (en) * 1983-01-19 1985-06-11 Ford Aerospace & Communications Corp. Ram air steering system for a guided missile
WO1984002975A1 (fr) * 1983-01-20 1984-08-02 Ford Aerospace & Communication Systeme de guidage par combustion d'air sous pression dynamique
US4573648A (en) * 1983-01-20 1986-03-04 Ford Aerospace And Communications Corp. Ram air combustion steering system for a guided missile
US4685639A (en) * 1985-12-23 1987-08-11 Ford Aerospace & Communications Corp. Pneumatically actuated ram air steering system for a guided missile
EP0725259A1 (fr) * 1995-02-03 1996-08-07 Tda Armements S.A.S. ContrÔle d'un projectile par impulseur multi-chambre et mono-tuyère
FR2730302A1 (fr) * 1995-02-03 1996-08-09 Tda Armements Sas Controle d'un projectile par impulseur multi-chambre et mono-tuyere
US5657948A (en) * 1995-02-03 1997-08-19 Tda Armements Sas Control of a projectile by multi-chamber and single-nozzle impeller

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