DE2347895C3 - Außenbrennertreibsatz für Raketentriebwerke - Google Patents

Außenbrennertreibsatz für Raketentriebwerke

Info

Publication number
DE2347895C3
DE2347895C3 DE19732347895 DE2347895A DE2347895C3 DE 2347895 C3 DE2347895 C3 DE 2347895C3 DE 19732347895 DE19732347895 DE 19732347895 DE 2347895 A DE2347895 A DE 2347895A DE 2347895 C3 DE2347895 C3 DE 2347895C3
Authority
DE
Germany
Prior art keywords
propellant
radius
distance
cylinder
center
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
DE19732347895
Other languages
German (de)
English (en)
Other versions
DE2347895A1 (de
DE2347895B2 (de
Inventor
Pierre Louis Sevres Portalier (Frankreich)
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.)
NATIONALE DES POUDRES ET EXPLOSIFS PARIS Ste
Original Assignee
NATIONALE DES POUDRES ET EXPLOSIFS PARIS Ste
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 NATIONALE DES POUDRES ET EXPLOSIFS PARIS Ste filed Critical NATIONALE DES POUDRES ET EXPLOSIFS PARIS Ste
Publication of DE2347895A1 publication Critical patent/DE2347895A1/de
Publication of DE2347895B2 publication Critical patent/DE2347895B2/de
Application granted granted Critical
Publication of DE2347895C3 publication Critical patent/DE2347895C3/de
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
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F02K9/36—Propellant charge supports
    • 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
    • F02K9/10—Shape or structure of solid propellant charges
    • F02K9/20—Shape or structure of solid propellant charges of the external-burning type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/23—Three-dimensional prismatic
    • F05D2250/231—Three-dimensional prismatic cylindrical
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/70—Shape
    • F05D2250/71—Shape curved
    • F05D2250/711—Shape curved convex

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Products (AREA)
  • Cosmetics (AREA)
  • Portable Nailing Machines And Staplers (AREA)
DE19732347895 1972-09-26 1973-09-24 Außenbrennertreibsatz für Raketentriebwerke Expired DE2347895C3 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7233941A FR2201271B1 (cg-RX-API-DMAC10.html) 1972-09-26 1972-09-26

Publications (3)

Publication Number Publication Date
DE2347895A1 DE2347895A1 (de) 1974-04-25
DE2347895B2 DE2347895B2 (de) 1977-09-01
DE2347895C3 true DE2347895C3 (de) 1978-04-27

Family

ID=9104764

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19732347895 Expired DE2347895C3 (de) 1972-09-26 1973-09-24 Außenbrennertreibsatz für Raketentriebwerke

Country Status (4)

Country Link
DE (1) DE2347895C3 (cg-RX-API-DMAC10.html)
FR (1) FR2201271B1 (cg-RX-API-DMAC10.html)
GB (1) GB1402818A (cg-RX-API-DMAC10.html)
IT (1) IT996737B (cg-RX-API-DMAC10.html)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2272167C1 (ru) * 2004-10-04 2006-03-20 Федеральное государственное унитарное предприятие "Научно-исследовательский институт полимерных материалов" Заряд твердого ракетного топлива
RU2319851C1 (ru) * 2006-07-20 2008-03-20 Федеральное государственное унитарное предприятие "Научно-исследовательский институт полимерных материалов" Стартовый ракетный двигатель твердого топлива

Also Published As

Publication number Publication date
FR2201271A1 (cg-RX-API-DMAC10.html) 1974-04-26
FR2201271B1 (cg-RX-API-DMAC10.html) 1975-01-03
DE2347895A1 (de) 1974-04-25
GB1402818A (en) 1975-08-13
DE2347895B2 (de) 1977-09-01
IT996737B (it) 1975-12-10

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Legal Events

Date Code Title Description
C3 Grant after two publication steps (3rd publication)
8339 Ceased/non-payment of the annual fee