DE3881007T2 - Herstellung eines Raketengehäuses durch Wickeln von Fäden um den Feststofftreibsatz. - Google Patents

Herstellung eines Raketengehäuses durch Wickeln von Fäden um den Feststofftreibsatz.

Info

Publication number
DE3881007T2
DE3881007T2 DE88312382T DE3881007T DE3881007T2 DE 3881007 T2 DE3881007 T2 DE 3881007T2 DE 88312382 T DE88312382 T DE 88312382T DE 3881007 T DE3881007 T DE 3881007T DE 3881007 T2 DE3881007 T2 DE 3881007T2
Authority
DE
Germany
Prior art keywords
manufacture
solid propellant
threads around
winding threads
rocket case
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 - Fee Related
Application number
DE88312382T
Other languages
English (en)
Other versions
DE3881007D1 (de
Inventor
Robert Thomann
John E Latronico
Don C Carson
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.)
Northrop Grumman Innovation Systems LLC
Original Assignee
Thiokol Corp
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 Thiokol Corp filed Critical Thiokol Corp
Application granted granted Critical
Publication of DE3881007D1 publication Critical patent/DE3881007D1/de
Publication of DE3881007T2 publication Critical patent/DE3881007T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F02K9/24—Charging rocket engines with solid propellants; Methods or apparatus specially adapted for working solid propellant charges
    • 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
    • F02K9/34—Casings; Combustion chambers; Liners thereof

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Moulding By Coating Moulds (AREA)
DE88312382T 1987-12-29 1988-12-29 Herstellung eines Raketengehäuses durch Wickeln von Fäden um den Feststofftreibsatz. Expired - Fee Related DE3881007T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US13923787A 1987-12-29 1987-12-29

Publications (2)

Publication Number Publication Date
DE3881007D1 DE3881007D1 (de) 1993-06-17
DE3881007T2 true DE3881007T2 (de) 1993-11-18

Family

ID=22485707

Family Applications (1)

Application Number Title Priority Date Filing Date
DE88312382T Expired - Fee Related DE3881007T2 (de) 1987-12-29 1988-12-29 Herstellung eines Raketengehäuses durch Wickeln von Fäden um den Feststofftreibsatz.

Country Status (6)

Country Link
EP (1) EP0323247B1 (de)
JP (1) JPH01297397A (de)
AU (1) AU621576B2 (de)
CA (1) CA1326127C (de)
DE (1) DE3881007T2 (de)
IL (1) IL88748A0 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102011113539A1 (de) * 2011-09-15 2013-03-21 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Thermalisolation für Raketentriebwerke

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5341638A (en) * 1992-03-09 1994-08-30 Thiokol Corporation Low cost segmented structure for pressure vessels, rocket motors, piping
FR2736421B1 (fr) * 1995-07-07 1997-09-26 Manufactures De Vetements Paul Procede de fabrication d'une unite contenant une matiere active solide utile pour la production de froid, unite obtenue et dispositif frigorigene comportant cette unite
US5976293A (en) * 1997-02-10 1999-11-02 Universal Propulsion Company, Inc. Method for making a case for combustible materials
CA2318005A1 (en) * 2000-09-12 2002-03-12 Heinz Portmann Pre-stressed fibre-reinforce high pressure vessel
RU2539939C1 (ru) * 2013-12-10 2015-01-27 Открытое акционерное общество Центральный научно-исследовательский институт специального машиностроения Способ изготовления корпуса воспламенителя заряда ракетного двигателя из композиционных материалов и его конструкция
CN109653900B (zh) * 2018-11-29 2020-02-11 湖北航天技术研究院总体设计所 一种双脉冲固体发动机装药燃烧室的成型方法
CN115898695B (zh) * 2023-03-09 2023-05-16 陕西普利美材料科技有限公司 一种固体火箭发动机燃烧室绝热层结构及其粘接方法

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2995011A (en) * 1959-09-17 1961-08-08 Phillips Petroleum Co Solid propellant rocket motor
US3811358A (en) * 1961-10-10 1974-05-21 Rockwell International Corp Solid propellants containing reinforcing filament and process of making
US3518916A (en) * 1962-03-19 1970-07-07 North American Rockwell Method for producing reinforced solid propellant grains
FR1356673A (fr) * 1962-05-10 1964-03-27 Thiokol Chemical Corp Moteur de roquette et méthode de construction
GB1072420A (en) * 1964-12-21 1967-06-14 Aerojet General Co Fibre pressure vessel
US3731584A (en) * 1967-06-13 1973-05-08 Rockwell International Corp Automatic propellant feed system
FR2123036B1 (de) * 1969-11-24 1975-07-04 Neyrpic Creusot Loire
FR2552494B1 (fr) * 1983-09-26 1985-12-20 Europ Propulsion Procede de preparation de corps de propulseurs fusees

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102011113539A1 (de) * 2011-09-15 2013-03-21 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Thermalisolation für Raketentriebwerke
DE102011113539B4 (de) * 2011-09-15 2015-10-01 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Thermalisolation für Raketentriebwerke

Also Published As

Publication number Publication date
EP0323247B1 (de) 1993-05-12
IL88748A0 (en) 1989-07-31
EP0323247A1 (de) 1989-07-05
AU2737288A (en) 1989-06-29
AU621576B2 (en) 1992-03-19
DE3881007D1 (de) 1993-06-17
CA1326127C (en) 1994-01-18
JPH01297397A (ja) 1989-11-30

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Legal Events

Date Code Title Description
8327 Change in the person/name/address of the patent owner

Owner name: ALLIANT TECHSYSTEMS INC., EDINA, MINN., US

8339 Ceased/non-payment of the annual fee