FR1036205A - Perfectionnements apportés aux projectiles auto-propulsés à charge explosive, notamment aux obus explosifs auto-propulsés - Google Patents

Perfectionnements apportés aux projectiles auto-propulsés à charge explosive, notamment aux obus explosifs auto-propulsés

Info

Publication number
FR1036205A
FR1036205A FR1036205DA FR1036205A FR 1036205 A FR1036205 A FR 1036205A FR 1036205D A FR1036205D A FR 1036205DA FR 1036205 A FR1036205 A FR 1036205A
Authority
FR
France
Prior art keywords
self
propelled
explosive
projectiles
shells
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
Other languages
English (en)
Inventor
Boris Krebs
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 filed Critical
Application granted granted Critical
Publication of FR1036205A publication Critical patent/FR1036205A/fr
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
    • 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
    • F02K7/105—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 using a solid fuel
    • 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
    • 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)
FR1036205D 1951-04-26 1951-04-26 Perfectionnements apportés aux projectiles auto-propulsés à charge explosive, notamment aux obus explosifs auto-propulsés Expired FR1036205A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1036205T 1951-04-26

Publications (1)

Publication Number Publication Date
FR1036205A true FR1036205A (fr) 1953-09-04

Family

ID=9586255

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1036205D Expired FR1036205A (fr) 1951-04-26 1951-04-26 Perfectionnements apportés aux projectiles auto-propulsés à charge explosive, notamment aux obus explosifs auto-propulsés

Country Status (1)

Country Link
FR (1) FR1036205A (fr)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3049876A (en) * 1960-03-30 1962-08-21 James F Connors Annular rocket motor and nozzle configuration
US3112611A (en) * 1958-07-21 1963-12-03 Gen Electric Rocket motor employing a plug type nozzle
US3112612A (en) * 1958-07-21 1963-12-03 Gen Electric Rocket motor
US4063415A (en) * 1972-06-30 1977-12-20 The United States Of America As Represented By The Secretary Of The Army Apparatus for staged combustion in air augmented rockets
US5067406A (en) * 1990-11-05 1991-11-26 The United States Of America As Represented By The Secretary Of The Army Supersonic, low-drag, solid fuel ramjet tubular projectile

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3112611A (en) * 1958-07-21 1963-12-03 Gen Electric Rocket motor employing a plug type nozzle
US3112612A (en) * 1958-07-21 1963-12-03 Gen Electric Rocket motor
US3049876A (en) * 1960-03-30 1962-08-21 James F Connors Annular rocket motor and nozzle configuration
US4063415A (en) * 1972-06-30 1977-12-20 The United States Of America As Represented By The Secretary Of The Army Apparatus for staged combustion in air augmented rockets
US5067406A (en) * 1990-11-05 1991-11-26 The United States Of America As Represented By The Secretary Of The Army Supersonic, low-drag, solid fuel ramjet tubular projectile

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