FR1426963A - Improvements to missiles - Google Patents

Improvements to missiles

Info

Publication number: FR1426963A
Authority: FR; France
Prior art keywords: missiles
Prior art date: 1964-09-25
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

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.)

1964-09-25

Filing date

1964-09-25

Publication date

1966-02-04

1964-09-25 Application filed by Hawker Siddeley Dynamics Ltd filed Critical Hawker Siddeley Dynamics Ltd

1964-09-25 Priority to FR989351A priority Critical patent/FR1426963A/en

1966-02-04 Application granted granted Critical

1966-02-04 Publication of FR1426963A publication Critical patent/FR1426963A/en

Status 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
- F42B10/60—Steering arrangements
- F42B10/66—Steering by varying intensity or direction of thrust
- F42B10/663—Steering 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 Improvements to missiles Expired FR1426963A (en)

Priority Applications (1)

Application Number	Priority Date	Filing Date	Title
FR989351A FR1426963A (en)	1964-09-25	1964-09-25	Improvements to missiles

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
FR989351A FR1426963A (en)	1964-09-25	1964-09-25	Improvements to missiles

Publications (1)

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

Family

ID=8839087

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
FR989351A Expired FR1426963A (en)	1964-09-25	1964-09-25	Improvements to missiles

Country Status (1)

Country	Link
FR (1)	FR1426963A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
WO1984002975A1 (en) *	1983-01-20	1984-08-02	Ford Aerospace & Communication	Ram air combustion steering system for a guided missile
WO1984002974A1 (en) *	1983-01-19	1984-08-02	Ford Motor Co	Ram air 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 (en) *	1995-02-03	1996-08-07	Tda Armements S.A.S.	Projectile control by a multi-chamber, single nozzle thruster

1964
- 1964-09-25 FR FR989351A patent/FR1426963A/en not_active Expired

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
WO1984002974A1 (en) *	1983-01-19	1984-08-02	Ford Motor Co	Ram air steering system for a guided missile
US4522357A (en) *	1983-01-19	1985-06-11	Ford Aerospace & Communications Corp.	Ram air steering system for a guided missile
WO1984002975A1 (en) *	1983-01-20	1984-08-02	Ford Aerospace & Communication	Ram air combustion steering system for a guided missile
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 (en) *	1995-02-03	1996-08-07	Tda Armements S.A.S.	Projectile control by a multi-chamber, single nozzle thruster
FR2730302A1 (en) *	1995-02-03	1996-08-09	Tda Armements Sas	CONTROL OF A PROJECTILE BY MULTI-CHAMBER AND SINGLE-TUBE IMPELLER
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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