GB1014847A - Improvements in or relating to spin-stabilised rocket projectiles - Google Patents

Improvements in or relating to spin-stabilised rocket projectiles

Info

Publication number
GB1014847A
GB1014847A GB25099/63A GB2509963A GB1014847A GB 1014847 A GB1014847 A GB 1014847A GB 25099/63 A GB25099/63 A GB 25099/63A GB 2509963 A GB2509963 A GB 2509963A GB 1014847 A GB1014847 A GB 1014847A
Authority
GB
United Kingdom
Prior art keywords
spin
chamber
charge
inertia
centres
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
GB25099/63A
Other languages
English (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.)
Rheinmetall Industrie AG
Original Assignee
Rheinmetall GmbH
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 Rheinmetall GmbH filed Critical Rheinmetall GmbH
Publication of GB1014847A publication Critical patent/GB1014847A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/30—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants with the propulsion gases exhausting through a plurality of nozzles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/18—Composite ram-jet/rocket engines
    • 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
    • F42B10/26—Stabilising arrangements using spin
    • F42B10/28—Stabilising arrangements using spin induced by gas action
    • F42B10/30—Stabilising arrangements using spin induced by gas action using rocket motor nozzles
    • 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
    • F42B12/04—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
    • F42B12/10—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge
    • F42B12/12—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge rotatably mounted with respect to missile housing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Toys (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Testing Of Engines (AREA)
GB25099/63A 1962-06-30 1963-06-24 Improvements in or relating to spin-stabilised rocket projectiles Expired GB1014847A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DER33038A DE1213760B (de) 1962-06-30 1962-06-30 Hohlladungsgeschoss mit Eigenantrieb

Publications (1)

Publication Number Publication Date
GB1014847A true GB1014847A (en) 1965-12-31

Family

ID=7403958

Family Applications (1)

Application Number Title Priority Date Filing Date
GB25099/63A Expired GB1014847A (en) 1962-06-30 1963-06-24 Improvements in or relating to spin-stabilised rocket projectiles

Country Status (6)

Country Link
US (1) US3144828A (US07413550-20080819-C00001.png)
BE (1) BE634186A (US07413550-20080819-C00001.png)
CH (1) CH400839A (US07413550-20080819-C00001.png)
DE (1) DE1213760B (US07413550-20080819-C00001.png)
DK (1) DK112497B (US07413550-20080819-C00001.png)
GB (1) GB1014847A (US07413550-20080819-C00001.png)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1569559A (US07413550-20080819-C00001.png) * 1964-11-26 1969-06-06
US8051640B2 (en) * 2008-05-09 2011-11-08 Robert L Geisler Propulsion system, opposing grains rocket engine, and method for controlling the burn rate of solid propellant grains
BG66449B1 (bg) * 2010-01-28 2014-09-30 Любомир ТОМОВ Аеродинамично стабилизирана муниция

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT6796B (US07413550-20080819-C00001.png) * 1899-05-12 1902-02-25 Jacques Luciani
FR816083A (fr) * 1936-03-30 1937-07-29 Perfectionnements aux projectiles
BE428854A (US07413550-20080819-C00001.png) * 1937-06-28
US2519878A (en) * 1946-07-31 1950-08-22 Carold F Bjork Rocket projectile
US2968244A (en) * 1948-05-07 1961-01-17 Jr Leo Maas Jet accelerated missile
US2684629A (en) * 1949-06-16 1954-07-27 Bofors Ab Reaction-motor missile
FR1052450A (fr) * 1952-03-14 1954-01-25 France Etat Projectile auto-propulsé à efficacité améliorée
FR1265295A (fr) * 1960-05-18 1961-06-30 Perfectionnements apportés aux missiles, notamment à ceux destinés à répondre aux besoins de l'infanterie

Also Published As

Publication number Publication date
DE1213760B (de) 1966-03-31
DK112497B (da) 1968-12-16
US3144828A (en) 1964-08-18
BE634186A (US07413550-20080819-C00001.png) 1963-11-04
CH400839A (de) 1965-10-15

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