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GB8502392D0 - Flight body - Google Patents

Flight body

Info

Publication number
GB8502392D0
GB8502392D0 GB858502392A GB8502392A GB8502392D0 GB 8502392 D0 GB8502392 D0 GB 8502392D0 GB 858502392 A GB858502392 A GB 858502392A GB 8502392 A GB8502392 A GB 8502392A GB 8502392 D0 GB8502392 D0 GB 8502392D0
Authority
GB
United Kingdom
Prior art keywords
flight body
flight
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Withdrawn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
GB858502392A
Other versions
GB2153982A (en
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.)
Dynamit Nobel AG
Original Assignee
Dynamit Nobel 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 Dynamit Nobel AG filed Critical Dynamit Nobel AG
Publication of GB8502392D0 publication Critical patent/GB8502392D0/en
Publication of GB2153982A publication Critical patent/GB2153982A/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Withdrawn legal-status Critical Current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
    • F42B10/02—Stabilising arrangements
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/16—Wrap-around fins

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)
  • Toys (AREA)
GB08502392A 1984-02-02 1985-01-31 Flight body Withdrawn GB2153982A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19843403508 DE3403508A1 (en) 1984-02-02 1984-02-02 MISSILE

Publications (2)

Publication Number Publication Date
GB8502392D0 true GB8502392D0 (en) 1985-03-06
GB2153982A GB2153982A (en) 1985-08-29

Family

ID=6226496

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08502392A Withdrawn GB2153982A (en) 1984-02-02 1985-01-31 Flight body

Country Status (4)

Country Link
DE (1) DE3403508A1 (en)
FR (1) FR2559256A1 (en)
GB (1) GB2153982A (en)
IT (1) IT1182164B (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4717093A (en) * 1985-08-12 1988-01-05 Grumman Aerospace Corporation Penguin missile folding wing configuration
US4691880A (en) * 1985-11-14 1987-09-08 Grumman Aerospace Corporation Torsion spring powered missile wing deployment system
US4796835A (en) * 1986-12-17 1989-01-10 The Marquardt Company Projectile
FR2655720A1 (en) * 1989-12-08 1991-06-14 Thomson Brandt Armements WING GALBEE DEPLOYABLE FOR FLYING ENGINE.
SE465440B (en) * 1990-04-04 1991-09-09 Bofors Ab submunition
US6186442B1 (en) * 1998-09-04 2001-02-13 The United States Of America As Represented By The Secretary Of The Army Wing deployer and locker
GB0109277D0 (en) * 2001-04-12 2001-05-30 Olympic Technologies Ltd Small arms projectile
US8640589B2 (en) 2010-07-20 2014-02-04 Raytheon Company Projectile modification method

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE551492A (en) * 1955-10-20 Brandt Soc Nouv Ets
GB967841A (en) * 1961-01-03 1964-08-26 William Fisher Darling Improvements in fluid moving rotors
FR2130968A5 (en) * 1971-03-29 1972-11-10 Cnim
GB1597098A (en) * 1971-06-23 1981-09-03 British Aerospace Missiles
US3964696A (en) * 1974-10-30 1976-06-22 The United States Of America As Represented By The Secretary Of The Navy Method of controlling the spin rate of tube launched rockets
DE2518645C2 (en) * 1975-04-26 1986-07-17 Rheinmetall GmbH, 4000 Düsseldorf Twist brake for a payload that can be ejected from a twist projectile
FR2321723A1 (en) * 1975-07-29 1977-03-18 Thomson Brandt ATTITUDE CONTROL SYSTEM AND MACHINE EQUIPPED WITH SUCH A SYSTEM
US4029270A (en) * 1975-08-11 1977-06-14 General Dynamics Corporation Mechanical roll rate stabilizer for a rolling missile
US4044684A (en) * 1976-07-13 1977-08-30 Federal Laboratories, Inc. Aerosol projectile for lachrymating material
DE2747570A1 (en) * 1976-11-10 1978-05-18 Minnesota Mining & Mfg BULLET
GB2038457A (en) * 1978-12-30 1980-07-23 Dynamit Nobel Ag Practice ammunition braking device

Also Published As

Publication number Publication date
DE3403508A1 (en) 1985-08-08
IT8547626A0 (en) 1985-01-31
FR2559256A1 (en) 1985-08-09
IT8547626A1 (en) 1986-07-31
IT1182164B (en) 1987-09-30
GB2153982A (en) 1985-08-29

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

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