DE69841644D1 - Raketenantrieb mit einer Stufenstruktur des Innenraums - Google Patents

Raketenantrieb mit einer Stufenstruktur des Innenraums

Info

Publication number
DE69841644D1
DE69841644D1 DE69841644T DE69841644T DE69841644D1 DE 69841644 D1 DE69841644 D1 DE 69841644D1 DE 69841644 T DE69841644 T DE 69841644T DE 69841644 T DE69841644 T DE 69841644T DE 69841644 D1 DE69841644 D1 DE 69841644D1
Authority
DE
Germany
Prior art keywords
interior
stepped structure
rocket drive
rocket
drive
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 - Lifetime
Application number
DE69841644T
Other languages
English (en)
Inventor
Kurt B Kreiner
Carl R Stechmann
Joel Neiderman
David Bronson
Peter Woll
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.)
DirecTV Group Inc
Original Assignee
Hughes Electronics 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 Hughes Electronics Corp filed Critical Hughes Electronics Corp
Application granted granted Critical
Publication of DE69841644D1 publication Critical patent/DE69841644D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—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
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/90—Coating; Surface treatment
    • 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
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/10—Metals, alloys or intermetallic compounds
    • F05D2300/13—Refractory metals, i.e. Ti, V, Cr, Zr, Nb, Mo, Hf, Ta, W
    • F05D2300/133—Titanium
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/10—Metals, alloys or intermetallic compounds
    • F05D2300/14—Noble metals, i.e. Ag, Au, platinum group metals
    • F05D2300/143—Platinum group metals, i.e. Os, Ir, Pt, Ru, Rh, Pd
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/50—Intrinsic material properties or characteristics
    • F05D2300/502—Thermal properties
DE69841644T 1997-08-29 1998-08-27 Raketenantrieb mit einer Stufenstruktur des Innenraums Expired - Lifetime DE69841644D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US5759397P 1997-08-29 1997-08-29

Publications (1)

Publication Number Publication Date
DE69841644D1 true DE69841644D1 (de) 2010-06-10

Family

ID=22011567

Family Applications (2)

Application Number Title Priority Date Filing Date
DE69841644T Expired - Lifetime DE69841644D1 (de) 1997-08-29 1998-08-27 Raketenantrieb mit einer Stufenstruktur des Innenraums
DE69820173T Expired - Lifetime DE69820173T2 (de) 1997-08-29 1998-08-27 Verbindungsring für eine Raketenbrennkammer

Family Applications After (1)

Application Number Title Priority Date Filing Date
DE69820173T Expired - Lifetime DE69820173T2 (de) 1997-08-29 1998-08-27 Verbindungsring für eine Raketenbrennkammer

Country Status (4)

Country Link
US (1) US6269630B1 (de)
EP (1) EP0899447B1 (de)
JP (1) JP3068060B2 (de)
DE (2) DE69841644D1 (de)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0899449B1 (de) * 1997-08-29 2003-03-12 Hughes Electronics Corporation Raketenmotor mit einem Verbindungsstück zwischen Verbrennungskammer und Injektor
DE19927734C2 (de) * 1999-06-17 2002-04-11 Astrium Gmbh Schubkammer eines Antriebstriebwerks für Satelliten und Transportgeräte für Raumfahrtanwendungen
US6918243B2 (en) * 2003-05-19 2005-07-19 The Boeing Company Bi-propellant injector with flame-holding zone igniter
US7565795B1 (en) * 2006-01-17 2009-07-28 Pratt & Whitney Rocketdyne, Inc. Piezo-resonance igniter and ignition method for propellant liquid rocket engine
US8122703B2 (en) 2006-04-28 2012-02-28 United Technologies Corporation Coaxial ignition assembly
US20080299504A1 (en) * 2007-06-01 2008-12-04 Mark David Horn Resonance driven glow plug torch igniter and ignition method
US8814562B2 (en) * 2008-06-02 2014-08-26 Aerojet Rocketdyne Of De, Inc. Igniter/thruster with catalytic decomposition chamber
US9404441B2 (en) * 2008-08-18 2016-08-02 Aerojet Rocketdyne Of De, Inc. Low velocity injector manifold for hypergolic rocket engine
US8161725B2 (en) 2008-09-22 2012-04-24 Pratt & Whitney Rocketdyne, Inc. Compact cyclone combustion torch igniter
CN101539072B (zh) * 2009-04-17 2010-09-22 北京航空航天大学 一种液体管路填充状态可视装置
RU2532640C2 (ru) * 2010-11-17 2014-11-10 Федеральное государственное унитарное предприятие "Научно-исследовательский институт машиностроения" (ФГУП "НИИМаш") Камера жидкостного ракетного двигателя малой тяги
JP5992722B2 (ja) 2012-05-17 2016-09-14 株式会社Ｉｈｉエアロスペース スラスタ装置及び宇宙機
JP6679273B2 (ja) * 2015-11-02 2020-04-15 三菱重工業株式会社 燃焼器及びロケットエンジン
CN109595099B (zh) * 2018-11-19 2021-01-05 西北工业大学 一种地面试车实验用固液混合发动机
CN110566367B (zh) * 2019-08-20 2021-09-03 西安航天动力技术研究所 一种降低双脉冲固体发动机隔层应变的燃烧室
CN114412667B (zh) * 2021-12-20 2023-06-23 上海空间推进研究所 发动机燃烧室与喷管延伸段的连接系统及其加工方法

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4785748A (en) 1987-08-24 1988-11-22 The Marquardt Company Method sudden expansion (SUE) incinerator for destroying hazardous materials & wastes
US4915938A (en) 1987-11-13 1990-04-10 Zawadzki Mary E Hair treating composition
US4936091A (en) * 1988-03-24 1990-06-26 Aerojet General Corporation Two stage rocket combustor
US4882904A (en) * 1988-03-24 1989-11-28 Aerojet-General Corporation Two stage rocket combustor
US6138451A (en) * 1998-05-11 2000-10-31 Hughes Electronics Corporation Rocket engine with combustion chamber step structure insert, and its fabrication
US6138450A (en) * 1998-05-11 2000-10-31 Hughes Electronics Corporation Rocket engine with integral combustion chamber step structure and its fabrication

Also Published As

Publication number Publication date
JPH11132107A (ja) 1999-05-18
EP0899447B1 (de) 2003-12-03
JP3068060B2 (ja) 2000-07-24
DE69820173T2 (de) 2004-10-14
DE69820173D1 (de) 2004-01-15
EP0899447A3 (de) 2000-06-14
US6269630B1 (en) 2001-08-07
EP0899447A2 (de) 1999-03-03

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