ATE11443T1 - Raketenmotoren oder gasgeneratoren. - Google Patents

Raketenmotoren oder gasgeneratoren.

Info

Publication number
ATE11443T1
ATE11443T1 AT80303794T AT80303794T ATE11443T1 AT E11443 T1 ATE11443 T1 AT E11443T1 AT 80303794 T AT80303794 T AT 80303794T AT 80303794 T AT80303794 T AT 80303794T AT E11443 T1 ATE11443 T1 AT E11443T1
Authority
AT
Austria
Prior art keywords
propellant
filament
holes
combustion chamber
grain
Prior art date
Application number
AT80303794T
Other languages
English (en)
Inventor
Roger H.Jr. Whitesides
Original Assignee
Morton Thiokol, Inc.
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 Morton Thiokol, Inc. filed Critical Morton Thiokol, Inc.
Application granted granted Critical
Publication of ATE11443T1 publication Critical patent/ATE11443T1/de

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
    • F02K9/34—Casings; Combustion chambers; Liners thereof
    • F02K9/346—Liners, e.g. inhibitors
    • 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
    • F02K9/08—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

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)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Control Of Electric Motors In General (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)
  • Reinforced Plastic Materials (AREA)
AT80303794T 1979-10-26 1980-10-24 Raketenmotoren oder gasgeneratoren. ATE11443T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US06/088,706 US4345427A (en) 1979-10-26 1979-10-26 Rocket motor or gas generator having controlled thrust or mass flow output
EP80303794A EP0028150B1 (de) 1979-10-26 1980-10-24 Raketenmotoren oder Gasgeneratoren

Publications (1)

Publication Number Publication Date
ATE11443T1 true ATE11443T1 (de) 1985-02-15

Family

ID=22212948

Family Applications (1)

Application Number Title Priority Date Filing Date
AT80303794T ATE11443T1 (de) 1979-10-26 1980-10-24 Raketenmotoren oder gasgeneratoren.

Country Status (6)

Country Link
US (1) US4345427A (de)
EP (1) EP0028150B1 (de)
JP (1) JPS5666431A (de)
AT (1) ATE11443T1 (de)
CA (1) CA1166854A (de)
DE (1) DE3070031D1 (de)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4587805A (en) * 1985-01-29 1986-05-13 The United States Of America As Represented By The Secretary Of The Air Force Electro-optical control of solid fuel rocket burn rate
US4630437A (en) * 1985-01-29 1986-12-23 The United States Of America As Represented By The Secretary Of The Air Force Optical control method for solid fuel rocket burn rate
FR2591281B1 (fr) * 1985-12-05 1988-04-01 Europ Propulsion Amenagement interne anti-clappement pour propulseur a poudre et son procede de fabrication.
EP0269642A4 (de) * 1986-02-28 1988-06-23 Commw Of Australia Raketenantriebladung mit negativdruckexponent.
US5817968A (en) * 1987-08-03 1998-10-06 The United States Of America As Represented By The Secretary Of The Air Force Gas generation with high pressure sensitivity exponent propellant
RU2164617C1 (ru) * 1999-08-09 2001-03-27 Научно-исследовательский институт полимерных материалов Газогенератор
RU2211356C1 (ru) * 2002-01-15 2003-08-27 Федеральное государственное унитарное предприятие "Научно-исследовательский институт полимерных материалов" Ракетный двигатель твердого топлива
US20050115439A1 (en) * 2003-12-02 2005-06-02 Abel Stephen G. Multiple pulse segmented gas generator
RU2274761C2 (ru) * 2004-02-24 2006-04-20 Государственное образовательное учреждение высшего профессионального образования "Южно-Российский государственный технический университет" (Новочеркасский политехнический институт") Способ регулирования соотношения компонентов топлива в гибридном ракетном двигателе
RU2319852C1 (ru) * 2006-06-15 2008-03-20 Федеральное государственное образовательное учреждение высшего профессионального образования Пермская Государственная сельскохозяйственная академия имени академика Д.Н.Прянишникова Ракетный двигатель твердого топлива с изменяемым электромагнитным регулированием интенсивности горения топлива
US8667776B2 (en) 2009-02-23 2014-03-11 Raytheon Company Pellet-loaded multiple impulse rocket motor
US8242422B2 (en) * 2009-02-23 2012-08-14 Raytheon Company Modular divert and attitude control system
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
RU2493401C1 (ru) * 2012-04-10 2013-09-20 Открытое акционерное общество "Научно-исследовательский институт полимерных материалов" Ракетный двигатель твердого топлива
RU2498100C1 (ru) * 2012-06-14 2013-11-10 Открытое акционерное общество "Научно-исследовательский институт полимерных материалов" Ракетный двигатель твердого топлива
RU2756361C1 (ru) * 2021-02-15 2021-09-29 Акционерное общество "Корпорация "Московский институт теплотехники" (АО "Корпорация "МИТ") Стендовое устройство для определения суммарного импульса тяги твердотопливной газореактивной системы ориентации, снабженной газонакопительной емкостью, и способ определения суммарного импульса тяги твердотопливной газореактивной системы ориентации с газонакопительной емкостью
CN112983676B (zh) * 2021-03-31 2023-06-13 西北工业大学 一种固体火箭发动机燃烧室药柱
CN114941584B (zh) * 2022-04-28 2025-09-30 湖北航天技术研究院总体设计所 适用于固体姿控发动机压强波动的绝热结构及燃发器
US20240167435A1 (en) * 2022-11-22 2024-05-23 Raytheon Company Multipulse rocket motor with pressure-equalizing channels

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2733568A (en) * 1956-02-07 Solid propellant jet reaction motor
US2986001A (en) * 1956-08-16 1961-05-30 Aerojet General Co Shock absorbing means for rocket propellant grains
US2957309A (en) * 1957-07-22 1960-10-25 Phillips Petroleum Co Rocket motor
US3009385A (en) * 1957-12-26 1961-11-21 Phillips Petroleum Co Method of loading a rocket motor with solid propellant
NL261914A (de) * 1960-03-04
US3392524A (en) * 1966-06-23 1968-07-16 Thiokol Chemical Corp Tube burning rate sensor for solid propellant back bleed tube rocket motors
US3381476A (en) * 1966-08-10 1968-05-07 Thiokol Chemical Corp Filament control system for the burning rate of a solid propellant rocket motor
US3407595A (en) * 1966-09-28 1968-10-29 Thiokol Chemical Corp Means for stress relieving case bonded solid propellant grains
US3630028A (en) * 1969-12-01 1971-12-28 Leonard H Caveny Pressure level control system for a solid propellant rocket motor
US3672170A (en) * 1970-06-12 1972-06-27 Lockheed Aircraft Corp Propellant grain suspension system
US3713395A (en) * 1971-04-28 1973-01-30 Us Navy Solid propellant
US3919841A (en) * 1974-07-05 1975-11-18 Us Navy Rocket motor apparatus

Also Published As

Publication number Publication date
EP0028150B1 (de) 1985-01-23
JPS5666431A (en) 1981-06-04
DE3070031D1 (en) 1985-03-07
US4345427A (en) 1982-08-24
EP0028150A1 (de) 1981-05-06
CA1166854A (en) 1984-05-08

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Legal Events

Date Code Title Description
UEP Publication of translation of european patent specification
REN Ceased due to non-payment of the annual fee