BE590820A - Régulateur de poussée pour fusée à combustible solide - Google Patents

Régulateur de poussée pour fusée à combustible solide

Info

Publication number
BE590820A
BE590820A BE590820A BE590820A BE590820A BE 590820 A BE590820 A BE 590820A BE 590820 A BE590820 A BE 590820A BE 590820 A BE590820 A BE 590820A BE 590820 A BE590820 A BE 590820A
Authority
BE
Belgium
Prior art keywords
solid fuel
fuel rocket
rocket thrust
thrust regulator
regulator
Prior art date
Application number
BE590820A
Other languages
English (en)
Inventor
Walter A Ledwith
Original Assignee
United Aircraft 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 United Aircraft Corp filed Critical United Aircraft Corp
Publication of BE590820A publication Critical patent/BE590820A/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
    • F02K9/28—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
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/26—Burning control

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Testing Of Engines (AREA)
BE590820A 1959-05-18 1960-05-13 Régulateur de poussée pour fusée à combustible solide BE590820A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US813805A US3031842A (en) 1959-05-18 1959-05-18 Thrust control for solid rocket

Publications (1)

Publication Number Publication Date
BE590820A true BE590820A (fr) 1960-11-14

Family

ID=25213441

Family Applications (1)

Application Number Title Priority Date Filing Date
BE590820A BE590820A (fr) 1959-05-18 1960-05-13 Régulateur de poussée pour fusée à combustible solide

Country Status (3)

Country Link
US (1) US3031842A (fr)
BE (1) BE590820A (fr)
GB (1) GB873670A (fr)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3155019A (en) * 1960-05-06 1964-11-03 Thompson Ramo Wooldridge Inc Hot gas servo system having rotary actuator
US3712058A (en) * 1961-08-14 1973-01-23 Northrop Carolina Inc Solid propellant controlled rocket motors
US3172255A (en) * 1961-09-26 1965-03-09 United Aircraft Corp Ignition device
US3217489A (en) * 1961-11-15 1965-11-16 Thiokol Chemical Corp Rocket motor ignition system
US3182451A (en) * 1962-01-15 1965-05-11 Bendix Corp Thrust control means
NL294375A (fr) * 1962-06-30
US3266238A (en) * 1963-03-28 1966-08-16 Texaco Experiment Inc Rocket with internal restriction
US3345822A (en) * 1966-02-17 1967-10-10 Louis A Povinelli Burning rate control of solid propellants
US3908358A (en) * 1973-01-31 1975-09-30 Thiokol Corp Variable flow gas generating method and system
US4080901A (en) * 1976-04-20 1978-03-28 The United States Of America As Represented By The Aministrator Of The National Aeronautics And Space Administration Molded composite pyrogen igniter for rocket motors
US4591314A (en) * 1984-07-09 1986-05-27 Sundstrand Corporation Hydraulic power supply system utilizing a solid propellant gas generator
US4840024A (en) * 1984-08-20 1989-06-20 Morton Thiokol, Inc. Multiple propellant solid rocket motor
US4817377A (en) * 1987-05-07 1989-04-04 Morton Thiokol, Inc. Head end control and steering system: using a forward end maneuvering gas generator
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
DE3924858A1 (de) * 1989-07-27 1991-02-07 Messerschmitt Boelkow Blohm Gasgenerator fuer staustrahlraketen
US4924775A (en) * 1989-11-02 1990-05-15 The United States Of America As Represented By The Secretary Of The Army Integrated two stage rocket
US6412275B1 (en) * 2000-09-08 2002-07-02 United Technologies Corporation Solid propellant gas generator impulse management scheme for high mass flow turn-down ratio
US8051640B2 (en) * 2008-05-09 2011-11-08 Robert L Geisler Propulsion system, opposing grains rocket engine, and method for controlling the burn rate of solid propellant grains
FR3033882B1 (fr) * 2015-03-16 2017-04-07 Herakles Generateur de gaz
US10563617B2 (en) 2016-09-23 2020-02-18 Raytheon Company Electrically operated propellant for solid rocket motor thrust management
CN113687013B (zh) * 2021-07-30 2022-07-05 西北工业大学 一种用于拍摄过载条件下固体推进剂燃烧试验的装置
CN114941967B (zh) * 2022-06-01 2023-07-25 西北工业大学 一种基于固液混合火箭发动机的可控靶标飞行器

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2408111A (en) * 1943-08-30 1946-09-24 Robert C Truax Two-stage rocket system
US2683963A (en) * 1947-08-05 1954-07-20 Edward F Chandler Reaction engine with automatic pressure regulation
US2555333A (en) * 1948-05-27 1951-06-05 Joseph A Grand Solid fuel
US2791883A (en) * 1951-10-25 1957-05-14 Gen Electric Propellant system
GB719946A (en) * 1952-01-16 1954-12-08 Napier & Son Ltd Improvements in or relating to rocket type jet propulsion units

Also Published As

Publication number Publication date
US3031842A (en) 1962-05-01
GB873670A (en) 1961-07-26

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