CH489706A - Rocket engine comprising a propellant charge with two basic components - Google Patents

Rocket engine comprising a propellant charge with two basic components

Info

Publication number
CH489706A
CH489706A CH1284967A CH1284967A CH489706A CH 489706 A CH489706 A CH 489706A CH 1284967 A CH1284967 A CH 1284967A CH 1284967 A CH1284967 A CH 1284967A CH 489706 A CH489706 A CH 489706A
Authority
CH
Switzerland
Prior art keywords
basic components
rocket engine
propellant charge
propellant
charge
Prior art date
Application number
CH1284967A
Other languages
French (fr)
Inventor
Bodinaux Gaston
Original Assignee
Zeebrugge Forges Sa
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 Zeebrugge Forges Sa filed Critical Zeebrugge Forges Sa
Publication of CH489706A publication Critical patent/CH489706A/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/10Shape or structure of solid propellant charges
    • F02K9/12Shape or structure of solid propellant charges made of two or more portions burning at different rates or having different characteristics
    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B23/00Compositions characterised by non-explosive or non-thermic constituents
    • C06B23/007Ballistic modifiers, burning rate catalysts, burning rate depressing agents, e.g. for gas generating
    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B45/00Compositions or products which are defined by structure or arrangement of component of product
    • C06B45/12Compositions or products which are defined by structure or arrangement of component of product having contiguous layers or zones
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/10Shape or structure of solid propellant charges
    • F02K9/18Shape or structure of solid propellant charges of the internal-burning type having a star or like shaped internal cavity
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B1/00Explosive charges characterised by form or shape but not dependent on shape of container

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Organic Chemistry (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Air Bags (AREA)
  • Acyclic And Carbocyclic Compounds In Medicinal Compositions (AREA)
  • Medicinal Preparation (AREA)
  • Inorganic Compounds Of Heavy Metals (AREA)
  • Testing Of Engines (AREA)
CH1284967A 1967-02-22 1967-09-13 Rocket engine comprising a propellant charge with two basic components CH489706A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
BE2046551 1967-02-22
BE2046724 1967-04-10

Publications (1)

Publication Number Publication Date
CH489706A true CH489706A (en) 1970-04-30

Family

ID=25661642

Family Applications (1)

Application Number Title Priority Date Filing Date
CH1284967A CH489706A (en) 1967-02-22 1967-09-13 Rocket engine comprising a propellant charge with two basic components

Country Status (12)

Country Link
AT (1) AT277669B (en)
AU (1) AU5549973A (en)
BE (2) BE694408A (en)
CH (1) CH489706A (en)
DE (1) DE1626083A1 (en)
DK (1) DK141607C (en)
ES (1) ES345609A1 (en)
GB (1) GB1204138A (en)
GR (1) GR33273B (en)
LU (1) LU54389A1 (en)
NL (1) NL6712608A (en)
NO (1) NO122959B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2193491B (en) * 1978-07-21 1988-09-14 Imi Kynoch Limited Kynoch Work Improvements in propellants

Also Published As

Publication number Publication date
NL6712608A (en) 1968-08-23
ES345609A1 (en) 1970-02-01
AT277669B (en) 1970-01-12
DE1626083A1 (en) 1970-04-02
GB1204138A (en) 1970-09-03
DK141607C (en) 1980-10-13
DK141607B (en) 1980-05-05
NO122959B (en) 1971-09-06
BE694408A (en) 1967-08-22
GR33273B (en) 1967-11-18
AU5549973A (en) 1974-11-14
BE696817A (en) 1967-10-10
LU54389A1 (en) 1967-10-30

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Legal Events

Date Code Title Description
PL Patent ceased