IT1128690B - Perfezionamento nelle valvole di iniezione per motori a razzo - Google Patents

Perfezionamento nelle valvole di iniezione per motori a razzo

Info

Publication number
IT1128690B
IT1128690B IT49778/80A IT4977880A IT1128690B IT 1128690 B IT1128690 B IT 1128690B IT 49778/80 A IT49778/80 A IT 49778/80A IT 4977880 A IT4977880 A IT 4977880A IT 1128690 B IT1128690 B IT 1128690B
Authority
IT
Italy
Prior art keywords
improvement
injection valves
rocket engines
rocket
engines
Prior art date
Application number
IT49778/80A
Other languages
English (en)
Other versions
IT8049778A0 (it
Inventor
Wesley Jacqua Vance
Original Assignee
Rockwell International 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 Rockwell International Corp filed Critical Rockwell International Corp
Publication of IT8049778A0 publication Critical patent/IT8049778A0/it
Application granted granted Critical
Publication of IT1128690B publication Critical patent/IT1128690B/it

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
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44Feeding propellants
    • F02K9/56Control
    • F02K9/58Propellant feed valves
    • 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
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44Feeding propellants

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
IT49778/80A 1980-01-18 1980-09-30 Perfezionamento nelle valvole di iniezione per motori a razzo IT1128690B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/113,432 US4326377A (en) 1980-01-18 1980-01-18 Injection shut-off valve for regenerative injection

Publications (2)

Publication Number Publication Date
IT8049778A0 IT8049778A0 (it) 1980-09-30
IT1128690B true IT1128690B (it) 1986-06-04

Family

ID=22349374

Family Applications (1)

Application Number Title Priority Date Filing Date
IT49778/80A IT1128690B (it) 1980-01-18 1980-09-30 Perfezionamento nelle valvole di iniezione per motori a razzo

Country Status (6)

Country Link
US (1) US4326377A (it)
JP (1) JPS56107934A (it)
DE (1) DE3037773A1 (it)
FR (1) FR2474101A1 (it)
GB (1) GB2067740B (it)
IT (1) IT1128690B (it)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4722185A (en) * 1985-09-09 1988-02-02 Rockwell International Corporation Double piston rocket engine assembly
US4726184A (en) * 1985-09-09 1988-02-23 Rockwell International Corporation Rocket engine assembly
US4801092A (en) * 1986-02-24 1989-01-31 Rockwell International Corporation Injector assembly for a fluid fueled engine
US4739613A (en) * 1986-11-17 1988-04-26 Rockwell International Corporation Bi-propellant blade valve assembly
US4707983A (en) * 1986-11-24 1987-11-24 Rockwell International Corporation Flexure disc sealed integral bipropellant valve and injector valve assembly
FR2702008B1 (fr) * 1993-02-26 1995-05-24 Europ Propulsion Système d'injection mobile à obturation réactivable.
FR2734025B1 (fr) * 1995-05-11 1997-08-01 Europ Propulsion Moteur fusee a propergol liquide, a impulsions
US5941062A (en) * 1995-05-11 1999-08-24 Societe Europeenne De Propulsion Pulse rocket engine
US5719351A (en) * 1996-12-03 1998-02-17 Morton International, Inc. Anti-rupture method for liquid propellant gas inflator
US5746445A (en) * 1996-12-03 1998-05-05 Johnson; Darrin L. Injection termination feature
US5768885A (en) * 1996-12-03 1998-06-23 Autoliv Asp, Inc. Regenerative piston liquid propellant rocket motor
US5755091A (en) * 1996-12-17 1998-05-26 Autoliv Asp, Inc. Regenerative piston engine for combustion of liquid monopropellant
US5829784A (en) * 1997-02-13 1998-11-03 General Dynamics Armament Systems, Inc. Airbag inflator for vehicle occupant restraint apparatus
EP1321657A3 (en) * 2001-12-21 2004-03-10 United Technologies Corporation Reduced gain thrust control valve
US7185675B2 (en) * 2001-12-21 2007-03-06 United Technologies Corporation Reduced gain thrust control valve
US8122703B2 (en) * 2006-04-28 2012-02-28 United Technologies Corporation Coaxial ignition assembly
RU2488712C2 (ru) * 2011-07-20 2013-07-27 Государственное образовательное учреждение высшего профессионального образования Томский государственный университет (ТГУ) Способ организации рабочего процесса в космической двигательной установке на газообразном топливе
RU2579295C1 (ru) * 2015-03-23 2016-04-10 Открытое акционерное общество "Конструкторское бюро химавтоматики" Жидкостный ракетный двигатель
LT6464B (lt) 2016-10-31 2017-10-10 UAB "Nanoavionika" Erdvėlaivio variklio kuro purkštuvas-vožtuvas su šilumos valdymo sistema
CN107023401A (zh) * 2017-05-28 2017-08-08 西安成立航空制造有限公司 一种航空发动机燃油喷嘴用预燃级副油路活门及其使用方法
CN110953088B (zh) * 2019-12-09 2022-04-26 陕西天回航天技术有限公司 一种自增压双组元脉冲工作火箭发动机
CN112628015B (zh) * 2019-12-09 2022-07-05 陕西天回航天技术有限公司 一种气动柱塞自增压单组元脉冲工作姿控发动机
CN110925115B (zh) * 2019-12-09 2022-07-05 陕西天回航天技术有限公司 一种环缸型气动柱塞自增压单组元脉冲工作姿控发动机

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2410538A (en) * 1939-11-22 1946-11-05 Walton George William Prime mover
US2954670A (en) * 1953-12-17 1960-10-04 Richard R Helus Method of propellant stowage, arming and initiation of propellant flow for a liquid fuel propulsion system in a liquid fuel rocket motor
US2992528A (en) * 1955-03-28 1961-07-18 Anthony R Ozanich Liquid propellant gas generator for liquid propellant type rockets
US2918791A (en) * 1956-08-20 1959-12-29 Experiment Inc Differential area piston pumping system
US3088406A (en) * 1959-06-22 1963-05-07 Thompson Ramo Wooldridge Inc Quantized impulse rocket
US3011312A (en) * 1959-12-21 1961-12-05 Hydro Space Technology Inc Propulsion system
GB968583A (en) * 1960-01-22 1964-09-02 Automotive Prod Co Ltd Improvements in and relating to valves for liquid pressure control systems
US3170605A (en) * 1963-06-26 1965-02-23 Hugh L Dryden Ejection unit
DE1289363B (de) * 1966-03-25 1969-02-13 Boelkow Gmbh Treibstoffoerdervorrichtung fuer Fluessigkeitsraketen
US3680310A (en) * 1967-05-19 1972-08-01 Us Navy Starting device for monopropellant gas generator
FR2135397B1 (it) * 1971-05-03 1973-05-11 Utilisation Ration Gaz
US4258546A (en) * 1979-01-15 1981-03-31 Rockwell International Corporation Propulsion system

Also Published As

Publication number Publication date
GB2067740A (en) 1981-07-30
GB2067740B (en) 1984-08-22
IT8049778A0 (it) 1980-09-30
DE3037773A1 (de) 1981-07-23
JPH0364702B2 (it) 1991-10-08
DE3037773C2 (it) 1990-07-05
FR2474101B1 (it) 1983-08-26
FR2474101A1 (fr) 1981-07-24
US4326377A (en) 1982-04-27
JPS56107934A (en) 1981-08-27

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Legal Events

Date Code Title Description
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19970925