ES374022A1 - Rocket launcher - Google Patents

Rocket launcher

Info

Publication number
ES374022A1
ES374022A1 ES374022A ES374022A ES374022A1 ES 374022 A1 ES374022 A1 ES 374022A1 ES 374022 A ES374022 A ES 374022A ES 374022 A ES374022 A ES 374022A ES 374022 A1 ES374022 A1 ES 374022A1
Authority
ES
Spain
Prior art keywords
loading tray
rocket
members
gases
apron
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
ES374022A
Other languages
Spanish (es)
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.)
Rheinmetall Air Defence AG
Original Assignee
Werkzeugmaschinenfabrik Oerlikon Buhrle AG
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 Werkzeugmaschinenfabrik Oerlikon Buhrle AG filed Critical Werkzeugmaschinenfabrik Oerlikon Buhrle AG
Publication of ES374022A1 publication Critical patent/ES374022A1/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A27/00Gun mountings permitting traversing or elevating movement, e.g. gun carriages
    • F41A27/30Stabilisation or compensation systems, e.g. compensating for barrel weight or wind force on the barrel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A9/00Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
    • F41A9/01Feeding of unbelted ammunition
    • F41A9/06Feeding of unbelted ammunition using cyclically moving conveyors, i.e. conveyors having ammunition pusher or carrier elements which are emptied or disengaged from the ammunition during the return stroke
    • F41A9/09Movable ammunition carriers or loading trays, e.g. for feeding from magazines
    • F41A9/10Movable ammunition carriers or loading trays, e.g. for feeding from magazines pivoting or swinging
    • F41A9/13Movable ammunition carriers or loading trays, e.g. for feeding from magazines pivoting or swinging in a vertical plane
    • F41A9/14Movable ammunition carriers or loading trays, e.g. for feeding from magazines pivoting or swinging in a vertical plane which is transverse to the barrel axis

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Toys (AREA)
  • Rollers For Roller Conveyors For Transfer (AREA)
  • Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)

Abstract

A rocket launcher comprises a magazine chamber 1 housing a loading tray 2 which terminates in a launcher tube, a conveyer roller 4 for feeding rockets 42 laterally into the loading tray 2, a preferably pivoted closure member 7 and a preferably pivoted apron member 23, the two members being spaced above and one at each side of the axis of the loading tray 2. The closure and apron members 7, 23 form backscattering surfaces for the propellent gases from a launched rocket, the gases acting in the surface of the closure member 7 through apertures 43 formed therein, the gases exerting equal and opposite torques on the members. In the construction shown the closure member 7 is spring urged into its rest position in which strips 12, 14 thereof abut the upper surface of a rocket 42 in the loading tray 2 and is urged in an anticlockwise direction by a rocket being fed into the loading tray 2. During feeding the apron member 23 is also swung away from its rest position in which it is held by a spring- loaded pawl (Fig. 3, not shown). A cover strip 45 is provided on the wall of the magazine chamber.
ES374022A 1968-11-29 1969-11-28 Rocket launcher Expired ES374022A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH1788768A CH499768A (en) 1968-11-29 1968-11-29 Rocket launcher

Publications (1)

Publication Number Publication Date
ES374022A1 true ES374022A1 (en) 1971-12-01

Family

ID=4428844

Family Applications (1)

Application Number Title Priority Date Filing Date
ES374022A Expired ES374022A1 (en) 1968-11-29 1969-11-28 Rocket launcher

Country Status (10)

Country Link
US (1) US3601000A (en)
JP (1) JPS493680B1 (en)
BE (1) BE742178A (en)
CH (1) CH499768A (en)
ES (1) ES374022A1 (en)
FR (1) FR2024505A1 (en)
GB (1) GB1234849A (en)
NL (1) NL6917702A (en)
NO (1) NO124179B (en)
SE (1) SE370118B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3999460A (en) * 1975-12-03 1976-12-28 Skliris Lewis E Rocket launching mechanism
US5294078A (en) * 1992-07-07 1994-03-15 Gurr John W Integrated system and method for assembling, and then transporting and supporting a launch vehicle
CN109200597B (en) * 2018-11-26 2024-01-26 桂林航天工业学院 Small solid rocket system

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL293330A (en) * 1962-06-04
CH492189A (en) * 1968-06-07 1970-06-15 Oerlikon Buehrle Ag Rocket launcher for rockets with folding tail

Also Published As

Publication number Publication date
FR2024505A1 (en) 1970-08-28
BE742178A (en) 1970-05-04
NO124179B (en) 1972-03-13
DE1959378A1 (en) 1970-06-25
US3601000A (en) 1971-08-24
CH499768A (en) 1970-11-30
NL6917702A (en) 1970-06-02
GB1234849A (en) 1971-06-09
JPS493680B1 (en) 1974-01-28
SE370118B (en) 1974-09-30

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