CH324499A - Self-propelled projectile - Google Patents

Self-propelled projectile

Info

Publication number
CH324499A
CH324499A CH324499DA CH324499A CH 324499 A CH324499 A CH 324499A CH 324499D A CH324499D A CH 324499DA CH 324499 A CH324499 A CH 324499A
Authority
CH
Switzerland
Prior art keywords
self
propelled projectile
projectile
propelled
Prior art date
Application number
Other languages
French (fr)
Original Assignee
Energa
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 Energa filed Critical Energa
Publication of CH324499A publication Critical patent/CH324499A/en

Links

Classifications

    • 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
    • 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
    • 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
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • 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
    • F02K9/95—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by starting or ignition means or arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Devices Affording Protection Of Roads Or Walls For Sound Insulation (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)
CH324499D 1953-03-14 1953-03-14 Self-propelled projectile CH324499A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH739417X 1953-03-14

Publications (1)

Publication Number Publication Date
CH324499A true CH324499A (en) 1957-09-30

Family

ID=4533013

Family Applications (1)

Application Number Title Priority Date Filing Date
CH324499D CH324499A (en) 1953-03-14 1953-03-14 Self-propelled projectile

Country Status (5)

Country Link
BE (1) BE525998A (en)
CH (1) CH324499A (en)
DE (1) DE934996C (en)
FR (1) FR1154410A (en)
GB (1) GB739417A (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1104867B (en) * 1958-02-11 1961-04-13 J G W Berckholtz Fa Rocket with stabilizer
DE1154978B (en) * 1961-06-12 1963-09-26 Rheinmetall Gmbh Propellant for solid rockets, especially for short-flame missiles
US4311005A (en) * 1979-05-11 1982-01-19 Raytheon Company Rocket motor
CN113202563B (en) * 2021-04-22 2022-08-16 沈阳航空航天大学 Coaxial reverse rotation two-stage turbine device for weakening missile launching tail flame energy

Also Published As

Publication number Publication date
FR1154410A (en) 1958-04-10
BE525998A (en)
GB739417A (en) 1955-10-26
DE934996C (en) 1955-11-10

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