GB941529A - Missiles having means for taking up shock on landing - Google Patents

Missiles having means for taking up shock on landing

Info

Publication number
GB941529A
GB941529A GB2351661A GB2351661A GB941529A GB 941529 A GB941529 A GB 941529A GB 2351661 A GB2351661 A GB 2351661A GB 2351661 A GB2351661 A GB 2351661A GB 941529 A GB941529 A GB 941529A
Authority
GB
United Kingdom
Prior art keywords
missile
landing
piston
parachutes
rod
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
GB2351661A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB941529A publication Critical patent/GB941529A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
    • B64D1/02Dropping, ejecting, or releasing articles
    • B64D1/08Dropping, ejecting, or releasing articles the articles being load-carrying devices
    • B64D1/14Absorbing landing shocks
    • 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
    • F42B10/32Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/48Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding
    • F42B10/56Range-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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B8/00Practice or training ammunition
    • F42B8/12Projectiles or missiles
    • F42B8/24Rockets

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

941,529. Missiles with landing means. L. BOLKOW, [trading as BOLKOW-ENTWICKLUNGEN KOMM.-GES.]. June 29, 1961 [July 1, 1960], No. 23516/61. Heading F3A. A missile comprises a nose 2 formed by shellhalves 2a, 2b adapted to open about hinges 4, thereby releasing parachutes 6, 7 and exposing a telescopic landing leg comprising a piston-rod 5a with piston 11 and a fluid containing cylinder 9. An explosive charge 17 which may be ignited for example when the propulsive charge of the missile burns out or by barometric means, removes a cap 18 thereby releasing the shellhalves. The parachute cords 13, 14 are attached to the cylinder 9 via staples 15 (not shown) at the rear of the missile so that on release the parachutes open and automatically hold the missile with its landing leg pointing downwards. A shear pin 20 retains rod 5a in position until contact with the ground, the piston 11 then forcing the damping fluid through bores 12 which are initially sealed by a suitable rupturable skin. A plate 16 prevents undue penetration by rod 5a when landing on soft ground. Alternatives to fluid as a shockabsorbing medium are mentioned and means may be provided to disengage the parachutes from the missile on landing.
GB2351661A 1960-07-01 1961-06-29 Missiles having means for taking up shock on landing Expired GB941529A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEB58429A DE1131559B (en) 1960-07-01 1960-07-01 Flying body for practice purposes

Publications (1)

Publication Number Publication Date
GB941529A true GB941529A (en) 1963-11-13

Family

ID=6972073

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2351661A Expired GB941529A (en) 1960-07-01 1961-06-29 Missiles having means for taking up shock on landing

Country Status (3)

Country Link
CH (1) CH391514A (en)
DE (1) DE1131559B (en)
GB (1) GB941529A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106956777A (en) * 2017-04-06 2017-07-18 北京机械设备研究所 A kind of automatic-opening new relief goods vehicle
CN114132532A (en) * 2022-01-12 2022-03-04 北京中科宇航技术有限公司 Landing leg mechanism for rocket recovery

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE977742C (en) * 1965-04-14 1969-04-30 Kunststofftechnische Studienge Flying body with knife-shaped tail wings that can be folded out against the direction of the air
EP0166278A1 (en) * 1984-06-15 1986-01-02 The State Of Israel Ministry Of Defence Israel Military Industries An aircraft carried smoke bomb
US4687455A (en) * 1985-10-22 1987-08-18 Ron Sculatti Flying model rocket and method of recovery

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE177947C (en) *
FR526120A (en) * 1913-09-27 1921-10-01 Pierre Casimir Louis Claverie Improvements made to devices for launching messages from aerial vessels with a parachute carrying the box containing the message
DE331479C (en) * 1919-11-25 1921-01-08 Rudolf Georg Pellmann Altitude observation and signaling device in connection with a parachute and a projectile
US2887055A (en) * 1956-08-07 1959-05-19 Harvey Machine Co Inc Training and test missile

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106956777A (en) * 2017-04-06 2017-07-18 北京机械设备研究所 A kind of automatic-opening new relief goods vehicle
CN106956777B (en) * 2017-04-06 2019-02-26 北京机械设备研究所 A kind of automatic-opening relief goods vehicle
CN114132532A (en) * 2022-01-12 2022-03-04 北京中科宇航技术有限公司 Landing leg mechanism for rocket recovery
CN114132532B (en) * 2022-01-12 2023-09-29 北京中科宇航技术有限公司 Landing leg mechanism for recovering rocket

Also Published As

Publication number Publication date
DE1131559B (en) 1962-06-14
CH391514A (en) 1965-04-30

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