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BE835727A - Propulseur de fusee a plusieurs chambres - Google Patents

Propulseur de fusee a plusieurs chambres

Info

Publication number
BE835727A
BE835727A BE0/162002A BE162002A BE835727A BE 835727 A BE835727 A BE 835727A BE 0/162002 A BE0/162002 A BE 0/162002A BE 162002 A BE162002 A BE 162002A BE 835727 A BE835727 A BE 835727A
Authority
BE
Belgium
Prior art keywords
rocket propeller
chamber rocket
chamber
propeller
rocket
Prior art date
Application number
BE0/162002A
Other languages
English (en)
Original Assignee
Dynamit Nobel Ag
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 Dynamit Nobel Ag filed Critical Dynamit Nobel Ag
Publication of BE835727A publication Critical patent/BE835727A/fr

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
    • 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
    • F02K9/26—Burning control
    • 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
    • F02K9/74—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant
    • F02K9/76—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with another rocket-engine plant; Multistage rocket-engine plants
    • F02K9/763—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with another rocket-engine plant; Multistage rocket-engine plants with solid propellant
    • 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
    • F02K9/94—Re-ignitable or restartable rocket- engine plants; Intermittently operated rocket-engine plants

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Feeding, Discharge, Calcimining, Fusing, And Gas-Generation Devices (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
BE0/162002A 1974-11-30 1975-11-19 Propulseur de fusee a plusieurs chambres BE835727A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19742456721 DE2456721C2 (de) 1974-11-30 1974-11-30 Mehrkammer-Raketentriebwerk

Publications (1)

Publication Number Publication Date
BE835727A true BE835727A (fr) 1983-07-15

Family

ID=5932175

Family Applications (1)

Application Number Title Priority Date Filing Date
BE0/162002A BE835727A (fr) 1974-11-30 1975-11-19 Propulseur de fusee a plusieurs chambres

Country Status (4)

Country Link
BE (1) BE835727A (fr)
DE (1) DE2456721C2 (fr)
FR (1) FR2569234A1 (fr)
GB (1) GB1605168A (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5386776A (en) * 1993-02-24 1995-02-07 Thiokol Corporation Bore mitigants for solid propellant rocket motors
FR2844557B1 (fr) 2002-09-12 2006-03-03 Snecma Propulsion Solide Systeme et procede de controle des oscillations de pression d'origine hydrodynamique pour propulseur a propergol solide
US8127534B2 (en) 2008-02-19 2012-03-06 Raytheon Company Pellet loaded attitude control rocket motor
US7685940B1 (en) 2008-03-21 2010-03-30 Raytheon Company Rocket motor with pellet and bulk solid propellants
US20110024165A1 (en) 2009-07-31 2011-02-03 Raytheon Company Systems and methods for composite structures with embedded interconnects
US8826640B2 (en) 2010-11-12 2014-09-09 Raytheon Company Flight vehicles including electrically-interconnective support structures and methods for the manufacture thereof
CN106870204A (zh) * 2017-01-19 2017-06-20 北京航空航天大学 固液火箭发动机燃烧室中间扰流装置
CN114263548B (zh) * 2021-12-22 2022-07-12 宁波天擎航天科技有限公司 一种固液混合发动机及飞行器

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2956401A (en) * 1959-06-12 1960-10-18 Ernest M Kane Variable thrust rocket motor
DE2214802A1 (de) * 1972-03-25 1973-09-27 Dynamit Nobel Ag Feststoffraketenmotor

Also Published As

Publication number Publication date
GB1605168A (en) 1982-09-08
DE2456721C2 (de) 1983-07-07
DE2456721A1 (de) 1982-11-04
FR2569234A1 (fr) 1986-02-21

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