JPH0442537B2 - - Google Patents

Info

Publication number
JPH0442537B2
JPH0442537B2 JP63090435A JP9043588A JPH0442537B2 JP H0442537 B2 JPH0442537 B2 JP H0442537B2 JP 63090435 A JP63090435 A JP 63090435A JP 9043588 A JP9043588 A JP 9043588A JP H0442537 B2 JPH0442537 B2 JP H0442537B2
Authority
JP
Japan
Prior art keywords
stage
combustion
solid propellant
rocket
rocket engine
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
Application number
JP63090435A
Other languages
English (en)
Japanese (ja)
Other versions
JPS63280843A (ja
Inventor
Shingaa Bikutaa
Ii Kerigan Barii
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.)
ATK Launch Systems LLC
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
Publication of JPS63280843A publication Critical patent/JPS63280843A/ja
Publication of JPH0442537B2 publication Critical patent/JPH0442537B2/ja
Granted 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
    • F02K9/10—Shape or structure of solid propellant charges
    • F02K9/12—Shape or structure of solid propellant charges made of two or more portions burning at different rates or having different characteristics
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/002—Launch systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/403—Solid propellant rocket engines
    • 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
    • F02K9/28—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants having two or more propellant charges with the propulsion gases exhausting through a common nozzle
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/641—Interstage or payload connectors

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Testing Of Engines (AREA)
  • Steroid Compounds (AREA)
  • Medicines Containing Plant Substances (AREA)
  • Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
JP63090435A 1987-05-08 1988-04-14 多段ロケット及びその作動を制御する方法 Granted JPS63280843A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US047760 1987-05-08
US07/047,760 US4819426A (en) 1987-05-08 1987-05-08 Rocket propelled vehicle forward end control method and apparatus

Publications (2)

Publication Number Publication Date
JPS63280843A JPS63280843A (ja) 1988-11-17
JPH0442537B2 true JPH0442537B2 (US07935154-20110503-C00006.png) 1992-07-13

Family

ID=21950815

Family Applications (1)

Application Number Title Priority Date Filing Date
JP63090435A Granted JPS63280843A (ja) 1987-05-08 1988-04-14 多段ロケット及びその作動を制御する方法

Country Status (5)

Country Link
US (1) US4819426A (US07935154-20110503-C00006.png)
EP (1) EP0298586B1 (US07935154-20110503-C00006.png)
JP (1) JPS63280843A (US07935154-20110503-C00006.png)
DE (1) DE3866977D1 (US07935154-20110503-C00006.png)
IL (1) IL86141A (US07935154-20110503-C00006.png)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5579635A (en) * 1994-11-18 1996-12-03 Thiokol Corporation Distributed erosion region rocket motor nozzle
US5577630A (en) * 1995-02-02 1996-11-26 Thiokol Corporation Composite conformable pressure vessel
DE19626075C1 (de) * 1996-06-28 1998-01-15 Buck Chem Tech Werke Flugkörper zur Bekämpfung beweglicher Ziele
ES2186459B1 (es) * 1999-11-08 2004-08-16 Enrique Ortega Villasante Submarino portaaeronaves y de desembarco.
US7464535B2 (en) * 2004-06-29 2008-12-16 Honeywell International Inc. Rocket motor nozzle throat area control system and method
US8020722B2 (en) * 2007-08-20 2011-09-20 Richards Kevin W Seamless multi-section pressure vessel
US10023329B1 (en) * 2017-03-04 2018-07-17 Othniel Mbamalu Space vehicle system
FR3110145A1 (fr) * 2020-05-14 2021-11-19 Constellation Technologies Système de lancement pour la mise en orbite d’une charge utile, procédé de mise en orbite associé.
CN112412659B (zh) * 2020-11-05 2021-12-10 北京空天技术研究所 一种飞行器级间连接段与助推器前封头一体化结构
US11988172B2 (en) 2020-11-19 2024-05-21 Raytheon Company Ignition safety device for a multi-pulse or multi-stage rocket motor system
WO2022216362A2 (en) * 2021-02-19 2022-10-13 Cesaroni Aerospace Incorporated Rocket motor
CN114876667B (zh) * 2022-04-27 2023-09-12 西安零壹空间科技有限公司 一种复合固体火箭发动机、装药方法及灌装设备
KR102628965B1 (ko) * 2023-06-13 2024-01-24 국방과학연구소 추진제 그레인의 나선형 배치를 갖는 부스터
KR102650106B1 (ko) * 2023-06-13 2024-03-21 국방과학연구소 추진제 그레인의 방사형 배치를 갖는 부스터

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2724237A (en) * 1946-03-05 1955-11-22 Clarence N Hickman Rocket projectile having discrete flight initiating and sustaining chambers
FR1048002A (fr) * 1951-08-17 1953-12-18 Ruggieri Ets Perfectionnements au chargement des corps moteurs de fusées ou analogues
FR1058495A (fr) * 1952-06-18 1954-03-16 Soc Tech De Rech Ind Propulseur à réaction
FR1143581A (fr) * 1954-05-14 1957-10-02 Soc Tech De Rech Ind Propulseur à poudre
US2945442A (en) * 1958-01-02 1960-07-19 Barnet R Adelman Explosive separation device
US3107487A (en) * 1960-08-12 1963-10-22 Aerojet General Co Rocket motor
US3385063A (en) * 1962-03-19 1968-05-28 Air Force Usa Multi-stage solid propellant motor
US3380251A (en) * 1963-03-03 1968-04-30 Thiokol Chemical Corp Ignition control of solid propellant rocket engines
US3349564A (en) * 1965-09-29 1967-10-31 Thiokol Chemical Corp Solid propellant rocket motor
FR2074761B1 (US07935154-20110503-C00006.png) * 1970-01-26 1974-08-09 Onera (Off Nat Aerospatiale)
US3724217A (en) * 1971-10-06 1973-04-03 Thiokol Chemical Corp Rocket system
US3826087A (en) * 1971-11-11 1974-07-30 Thiokol Chemical Corp Gas rocket system
US4550888A (en) * 1977-10-11 1985-11-05 Randle Douglass Dual pressure solid propellant control system
GB8324899D0 (en) * 1983-09-16 1983-10-19 Secr Defence Rocket motors
US4594945A (en) * 1984-11-28 1986-06-17 General Dynamics, Pomona Division Thermal protection for propellant grains

Also Published As

Publication number Publication date
JPS63280843A (ja) 1988-11-17
EP0298586B1 (en) 1991-12-18
IL86141A0 (en) 1988-11-15
US4819426A (en) 1989-04-11
IL86141A (en) 1992-12-01
DE3866977D1 (de) 1992-01-30
EP0298586A1 (en) 1989-01-11

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