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FR1340562A - Improvements to rocket launcher installations with launch tubes, in particular those for aerodynes - Google Patents

Improvements to rocket launcher installations with launch tubes, in particular those for aerodynes

Info

Publication number
FR1340562A
FR1340562A FR917535A FR917535A FR1340562A FR 1340562 A FR1340562 A FR 1340562A FR 917535 A FR917535 A FR 917535A FR 917535 A FR917535 A FR 917535A FR 1340562 A FR1340562 A FR 1340562A
Authority
FR
France
Prior art keywords
aerodynes
installations
particular those
rocket launcher
launch tubes
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
FR917535A
Other languages
French (fr)
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.)
Brevets Aero Mecaniques SA
Original Assignee
Brevets Aero Mecaniques 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
Priority claimed from LU40914A external-priority patent/LU40914A1/xx
Application filed by Brevets Aero Mecaniques SA filed Critical Brevets Aero Mecaniques SA
Priority to FR917535A priority Critical patent/FR1340562A/en
Application granted granted Critical
Publication of FR1340562A publication Critical patent/FR1340562A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00—Rocket or torpedo launchers
    • F41F3/04—Rocket or torpedo launchers for rockets
    • F41F3/052—Means for securing the rocket in the launching apparatus

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
FR917535A 1961-12-06 1962-12-04 Improvements to rocket launcher installations with launch tubes, in particular those for aerodynes Expired FR1340562A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR917535A FR1340562A (en) 1961-12-06 1962-12-04 Improvements to rocket launcher installations with launch tubes, in particular those for aerodynes

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
LU40914A LU40914A1 (en) 1961-12-06 1961-12-06
FR917535A FR1340562A (en) 1961-12-06 1962-12-04 Improvements to rocket launcher installations with launch tubes, in particular those for aerodynes

Publications (1)

Publication Number Publication Date
FR1340562A true FR1340562A (en) 1963-10-18

Family

ID=26198734

Family Applications (1)

Application Number Title Priority Date Filing Date
FR917535A Expired FR1340562A (en) 1961-12-06 1962-12-04 Improvements to rocket launcher installations with launch tubes, in particular those for aerodynes

Country Status (1)

Country Link
FR (1) FR1340562A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3398639A (en) * 1965-10-06 1968-08-27 Oerlikon Buehrle Holding Ag Holding device for a rocket in a launcher tube
US4132150A (en) * 1977-08-08 1979-01-02 The Unites States Of America As Represented By The Secretary Of The Army Blast actuated detent
US4191087A (en) * 1978-08-14 1980-03-04 The United States Of America As Represented By The Secretary Of The Army Rocket detent and release mechanism
WO1980001411A1 (en) * 1978-12-29 1980-07-10 Hughes Aircraft Co Automatic blast actuated positive release missile detent
US4304170A (en) * 1979-04-16 1981-12-08 The Boeing Company Locking assembly for a rocket and launch tube
US4550640A (en) * 1983-09-16 1985-11-05 Werkzeugmaschinenfabrik Oerlikon-Buehrle Ag Missile canister restraint device
FR2786860A1 (en) * 1998-12-08 2000-06-09 Agency Defense Dev Retaining catch for rocket munition has piston driven by exhaust gases to retract catch ball engaging missile

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3398639A (en) * 1965-10-06 1968-08-27 Oerlikon Buehrle Holding Ag Holding device for a rocket in a launcher tube
US4132150A (en) * 1977-08-08 1979-01-02 The Unites States Of America As Represented By The Secretary Of The Army Blast actuated detent
US4191087A (en) * 1978-08-14 1980-03-04 The United States Of America As Represented By The Secretary Of The Army Rocket detent and release mechanism
WO1980001411A1 (en) * 1978-12-29 1980-07-10 Hughes Aircraft Co Automatic blast actuated positive release missile detent
US4336740A (en) * 1978-12-29 1982-06-29 Hughes Aircraft Company Automatic blast actuated positive release missile detent
US4304170A (en) * 1979-04-16 1981-12-08 The Boeing Company Locking assembly for a rocket and launch tube
US4550640A (en) * 1983-09-16 1985-11-05 Werkzeugmaschinenfabrik Oerlikon-Buehrle Ag Missile canister restraint device
FR2786860A1 (en) * 1998-12-08 2000-06-09 Agency Defense Dev Retaining catch for rocket munition has piston driven by exhaust gases to retract catch ball engaging missile
US6286409B1 (en) * 1998-12-08 2001-09-11 Agency For Defense Development Apparatus for restraining and releasing missile using rigid sphere

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