GB2293644A - A missile or rocket comprising two parts which are separable along trajectory - Google Patents

A missile or rocket comprising two parts which are separable along trajectory Download PDF

Info

Publication number
GB2293644A
GB2293644A GB9517710A GB9517710A GB2293644A GB 2293644 A GB2293644 A GB 2293644A GB 9517710 A GB9517710 A GB 9517710A GB 9517710 A GB9517710 A GB 9517710A GB 2293644 A GB2293644 A GB 2293644A
Authority
GB
United Kingdom
Prior art keywords
canopy
rear part
cord
machine according
front part
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.)
Withdrawn
Application number
GB9517710A
Other languages
English (en)
Other versions
GB9517710D0 (en
Inventor
Marc Pinol
Philippe Mourry
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.)
Etienne LaCroix Tous Artifices SA
Original Assignee
Etienne LaCroix Tous Artifices 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 Etienne LaCroix Tous Artifices SA filed Critical Etienne LaCroix Tous Artifices SA
Publication of GB9517710D0 publication Critical patent/GB9517710D0/en
Publication of GB2293644A publication Critical patent/GB2293644A/en
Withdrawn legal-status Critical Current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
    • F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/48—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding
    • F42B10/56—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding of parachute or paraglider type

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
GB9517710A 1994-09-02 1995-08-31 A missile or rocket comprising two parts which are separable along trajectory Withdrawn GB2293644A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9410559A FR2724222A1 (fr) 1994-09-02 1994-09-02 Engin volant, notamment missile ou roquette, comprenant deux parties separables sur trajectoire

Publications (2)

Publication Number Publication Date
GB9517710D0 GB9517710D0 (en) 1995-11-01
GB2293644A true GB2293644A (en) 1996-04-03

Family

ID=9466656

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9517710A Withdrawn GB2293644A (en) 1994-09-02 1995-08-31 A missile or rocket comprising two parts which are separable along trajectory

Country Status (2)

Country Link
FR (1) FR2724222A1 (uk)
GB (1) GB2293644A (uk)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018234071A1 (de) * 2017-06-22 2018-12-27 Rheinmetall Waffe Munition Gmbh Schneideinrichtung

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2771805B1 (fr) 1997-12-02 2000-02-18 Lacroix Soc E Generateur pyroacoustique pour la protection de sous-marins et de batiments de surface
EP3036497B1 (en) 2013-08-20 2018-04-25 BAE Systems PLC Illumination munition

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1258044A (uk) * 1967-11-02 1971-12-22
US5239927A (en) * 1991-07-25 1993-08-31 Rheinmetall Gmbh Deceleration device for submunition

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3730099A (en) * 1970-12-17 1973-05-01 Us Navy Controlled descent system
US3834312A (en) * 1973-03-14 1974-09-10 Bofors Ab Parachute-borne flare assemblage
FR2656082A1 (fr) * 1989-12-15 1991-06-21 Thomson Brandt Armements Systeme deployable pour l'emport et la sustentation d'une munition.

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1258044A (uk) * 1967-11-02 1971-12-22
US5239927A (en) * 1991-07-25 1993-08-31 Rheinmetall Gmbh Deceleration device for submunition

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018234071A1 (de) * 2017-06-22 2018-12-27 Rheinmetall Waffe Munition Gmbh Schneideinrichtung

Also Published As

Publication number Publication date
FR2724222A1 (fr) 1996-03-08
GB9517710D0 (en) 1995-11-01
FR2724222B1 (uk) 1997-02-28

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)