JPS5623542A - Rocket attitude controller - Google Patents

Rocket attitude controller

Info

Publication number
JPS5623542A
JPS5623542A JP9934479A JP9934479A JPS5623542A JP S5623542 A JPS5623542 A JP S5623542A JP 9934479 A JP9934479 A JP 9934479A JP 9934479 A JP9934479 A JP 9934479A JP S5623542 A JPS5623542 A JP S5623542A
Authority
JP
Japan
Prior art keywords
nozzle
passage
rocket
cylinder chamber
ejection
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.)
Pending
Application number
JP9934479A
Other languages
English (en)
Inventor
Yasushi Watabe
Teruo Fujiwara
Kunio Shimano
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.)
Nissan Motor Co Ltd
Original Assignee
Nissan Motor Co Ltd
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 Nissan Motor Co Ltd filed Critical Nissan Motor Co Ltd
Priority to JP9934479A priority Critical patent/JPS5623542A/ja
Priority to GB8024112A priority patent/GB2055332B/en
Priority to US06/171,466 priority patent/US4384694A/en
Priority to DE3028557A priority patent/DE3028557C2/de
Priority to FR8016989A priority patent/FR2463443B1/fr
Publication of JPS5623542A publication Critical patent/JPS5623542A/ja
Pending 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
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/82—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control by injection of a secondary fluid into the rocket exhaust gases
    • 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
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/805—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control servo-mechanisms or control devices therefor
    • 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
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/90—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using deflectors

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Control Of Position Or Direction (AREA)
JP9934479A 1979-08-03 1979-08-03 Rocket attitude controller Pending JPS5623542A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
JP9934479A JPS5623542A (en) 1979-08-03 1979-08-03 Rocket attitude controller
GB8024112A GB2055332B (en) 1979-08-03 1980-07-23 Rocket attitude control apparatus
US06/171,466 US4384694A (en) 1979-08-03 1980-07-23 Rocket attitude control apparatus
DE3028557A DE3028557C2 (de) 1979-08-03 1980-07-28 Vorrichtung zur Steuerung der Fluglage einer Rakete
FR8016989A FR2463443B1 (fr) 1979-08-03 1980-07-31 Appareil de controle de l'assiette d'une fusee

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP9934479A JPS5623542A (en) 1979-08-03 1979-08-03 Rocket attitude controller

Publications (1)

Publication Number Publication Date
JPS5623542A true JPS5623542A (en) 1981-03-05

Family

ID=14244989

Family Applications (1)

Application Number Title Priority Date Filing Date
JP9934479A Pending JPS5623542A (en) 1979-08-03 1979-08-03 Rocket attitude controller

Country Status (5)

Country Link
US (1) US4384694A (ja)
JP (1) JPS5623542A (ja)
DE (1) DE3028557C2 (ja)
FR (1) FR2463443B1 (ja)
GB (1) GB2055332B (ja)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4615110A (en) * 1985-02-15 1986-10-07 E. I. Du Pont De Nemours And Company Hand tool for inserting and withdrawing a pin grid into and from a socket
US4707981A (en) * 1986-01-27 1987-11-24 Rockwell International Corporation Variable expansion ratio reaction engine
GB8822282D0 (en) * 1988-09-22 1989-04-19 British Aerospace Course correction unit
US5125596A (en) * 1989-05-23 1992-06-30 Cavalleri Robert J Fluid shielded movable strut for missile and rocket thrust vector control
US5072891A (en) * 1989-11-22 1991-12-17 Applied Technology Associates Combination actuator and coolant supply for missile and rocket vector control
US6681560B2 (en) 2002-01-08 2004-01-27 Atlantic Research Corporation Nozzle throat area control apparatus and method
RU2600259C1 (ru) * 2015-08-11 2016-10-20 Александр Абрамович Часовской Летательный аппарат
RU2636443C1 (ru) * 2016-09-30 2017-11-23 Александр Абрамович Часовской Летательный аппарат
RU2650319C1 (ru) * 2017-01-10 2018-04-11 Александр Абромович Часовской Летательный аппарат
CN107628274B (zh) * 2017-09-20 2019-10-11 北京航空航天大学 利用火箭发动机燃气的姿态控制装置和姿态控制系统
CN109163624B (zh) * 2018-09-27 2024-02-13 宁波天擎航天科技有限公司 一种可分离的火箭推进系统
CN110356589B (zh) * 2019-06-04 2021-01-05 宁波天擎航天科技有限公司 复用的侧喷流系统防水击控制方法、装置、计算机设备
CN114030654B (zh) * 2021-10-08 2023-06-06 北京控制工程研究所 一种基于脉宽调制的大气进入姿态控制方法
CN114856857B (zh) * 2022-05-12 2023-06-13 中国航发四川燃气涡轮研究院 多通道的集成式圆转方机匣

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB770025A (en) * 1952-10-10 1957-03-13 Snecma Device for steering aircraft, rockets and the like, having a jet propelling nozzle
US3020714A (en) * 1956-07-03 1962-02-13 Snecma Device for controlling the jet of a reaction propulsion motor
FR1197700A (fr) * 1957-12-11 1959-12-02 Bertin & Cie Dispositif permettant de diriger des mobiles propulsés par des fusées
FR1208542A (fr) * 1958-06-19 1960-02-24 & De Construction De Moteurs D Perfectionnements aux dispositifs de réglage des jets
GB916692A (en) * 1958-06-19 1963-01-23 Snecma Improvements in jet control apparatus
US3128602A (en) * 1960-12-30 1964-04-14 Bendix Corp Thrust vector control
US3182450A (en) * 1962-03-21 1965-05-11 Bendix Corp Means to insulate thrust vector interceptor surface
US3300978A (en) * 1962-06-18 1967-01-31 Lockheed Aircraft Corp Directional control means for rocket motor
FR1378040A (fr) * 1963-05-17 1964-11-13 Bertin & Cie Dispositif perfectionné de guidage par déviation du jet s'échappant d'une tuyère
US3318532A (en) * 1964-04-29 1967-05-09 Gen Motors Corp Gas injection thrust vector control system for rocket engines
US3465966A (en) * 1966-02-16 1969-09-09 Thiokol Chemical Corp Rocket control
US3568954A (en) * 1966-04-04 1971-03-09 William C Mccorkle Jr Directional control-automatic meteorological compensation (d.c.-automet) inertial guidance system for artillery missiles
US3926390A (en) * 1972-11-21 1975-12-16 Us Army Control valve logic
US4017040A (en) * 1976-01-12 1977-04-12 The United States Of America As Represented By The Secretary Of The Navy Steerable extraction rocket

Also Published As

Publication number Publication date
FR2463443A1 (fr) 1981-02-20
FR2463443B1 (fr) 1985-08-16
GB2055332A (en) 1981-03-04
DE3028557A1 (de) 1981-02-12
GB2055332B (en) 1983-06-02
DE3028557C2 (de) 1982-12-02
US4384694A (en) 1983-05-24

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