GB884128A - Improvements in or relating to flying bodies for supersonic speeds - Google Patents

Improvements in or relating to flying bodies for supersonic speeds

Info

Publication number
GB884128A
GB884128A GB5097/58A GB509758A GB884128A GB 884128 A GB884128 A GB 884128A GB 5097/58 A GB5097/58 A GB 5097/58A GB 509758 A GB509758 A GB 509758A GB 884128 A GB884128 A GB 884128A
Authority
GB
United Kingdom
Prior art keywords
nose
supersonic speeds
relating
neck
flying bodies
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
GB5097/58A
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 GB884128A publication Critical patent/GB884128A/en
Expired 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
    • F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C30/00—Supersonic type aircraft
    • 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
    • F42B10/38—Range-increasing arrangements
    • 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
    • F42B10/38—Range-increasing arrangements
    • F42B10/42—Streamlined projectiles
    • F42B10/46—Streamlined nose cones; Windshields; Radomes

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Toys (AREA)

Abstract

884,128. Self-propelled missiles. TAKACS, F. Feb. 17, 1958 [July 9, 1957], No. 5097/58. Class 9(2). A rocket or missile for use at supersonic speeds has a generally conical nose 11 connected by a neck 13 of reduced section to the body. The peripheral surface of the nose may be provided with ribs 17 which are tapered towards the tip of the nose. The nose 11 may be a surface of revolution tapering to a point, Fig. 5, from a base 12 joined to the neck 13 by a frusto-conical portion 15. Guide surfaces 16 such as rudders may be mounted on the nose 11 and stabilizing fins may be attached to the body around the nozzle.
GB5097/58A 1957-07-09 1958-02-17 Improvements in or relating to flying bodies for supersonic speeds Expired GB884128A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH884128X 1957-07-09

Publications (1)

Publication Number Publication Date
GB884128A true GB884128A (en) 1961-12-06

Family

ID=4545114

Family Applications (1)

Application Number Title Priority Date Filing Date
GB5097/58A Expired GB884128A (en) 1957-07-09 1958-02-17 Improvements in or relating to flying bodies for supersonic speeds

Country Status (2)

Country Link
US (1) US2980370A (en)
GB (1) GB884128A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3762666A (en) * 1971-06-08 1973-10-02 Us Army Hypervelocity missile design to accomodate seekers

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3231219A (en) * 1963-09-03 1966-01-25 Everett C Young Buffer for high-speed craft
US3425650A (en) * 1967-10-02 1969-02-04 Joseph Silva Air deflector for supersonic aircraft
US3416758A (en) * 1967-10-04 1968-12-17 Navy Usa Self-balancing spike control
US4225102A (en) * 1979-03-12 1980-09-30 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Aerodynamic side-force alleviator means
US4790499A (en) * 1984-07-31 1988-12-13 Taylor Thomas C Aerospike for attachment to space vehicle system
US4650139A (en) * 1984-07-31 1987-03-17 Taylor Thomas C Aerospike for attachment to space vehicle system
US5505409A (en) * 1994-05-20 1996-04-09 Wells; Anthony R. Supercavitating airframe
US5740984A (en) * 1994-09-22 1998-04-21 Mcdonnell Douglas Corporation Low sonic boom shock control/alleviation surface
DE19953701C2 (en) * 1999-11-08 2002-01-24 Lfk Gmbh Methods and devices for reducing pressure and temperature on the front of a missile at supersonic speeds
US8157216B2 (en) * 2008-06-30 2012-04-17 Ata Engineering, Inc. Methods and apparatus for an asymmetrical fairing
US8502126B2 (en) * 2010-05-27 2013-08-06 Raytheon Company System and method for navigating an object
WO2012060230A1 (en) * 2010-11-02 2012-05-10 独立行政法人宇宙航空研究開発機構 Nose for supersonic flying object
CN106275368B (en) * 2016-10-28 2018-05-29 清华大学 A kind of bionic Aircraft based on marmem driving deforms nose cone device
US20200108916A1 (en) * 2018-10-03 2020-04-09 Taylor DiAnte' Brown Skin grooves used for directing fluid on aircraft, landcraft, spacecraft, and watercraft related vehicles or propelled/projectile objects
US11614106B2 (en) * 2019-08-21 2023-03-28 Lockheed Martin Corporation Partially submerged periodic riblets
CN114572387B (en) * 2022-05-06 2022-08-12 北京航空航天大学 Forward-jet flow resistance-reducing heat-proof method for hypersonic-velocity pointed cone aircraft

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1065506A (en) * 1912-03-18 1913-06-24 Louis Constantin Means for reducing the resistance to the passage of vehicles in fluids.
FR982929A (en) * 1943-07-30 1951-06-18 Improvements to aircraft wings and other forms of fluid penetration
GB718498A (en) * 1950-10-24 1954-11-17 Arthur Veryan Stephens Improvements in and relating to solid/fluid boundary surfaces
US2752850A (en) * 1952-01-30 1956-07-03 Arthur H Warner Self-propelled missile
US2816721A (en) * 1953-09-15 1957-12-17 Taylor Richard John Rocket powered aerial vehicle

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3762666A (en) * 1971-06-08 1973-10-02 Us Army Hypervelocity missile design to accomodate seekers

Also Published As

Publication number Publication date
US2980370A (en) 1961-04-18

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