GB950722A - Control for a rocket motor - Google Patents

Control for a rocket motor

Info

Publication number
GB950722A
GB950722A GB3234/59A GB323459A GB950722A GB 950722 A GB950722 A GB 950722A GB 3234/59 A GB3234/59 A GB 3234/59A GB 323459 A GB323459 A GB 323459A GB 950722 A GB950722 A GB 950722A
Authority
GB
United Kingdom
Prior art keywords
sleeve
rocket motor
casing
rocket
motor
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
GB3234/59A
Inventor
William Thoby Fisher
Arthur Leighton Brake
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.)
Bristol Aerojet Ltd
Original Assignee
Bristol Aerojet 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 Bristol Aerojet Ltd filed Critical Bristol Aerojet Ltd
Priority to GB3234/59A priority Critical patent/GB950722A/en
Priority to DEB58589A priority patent/DE1154674B/en
Priority to FR832987A priority patent/FR1262426A/en
Publication of GB950722A publication Critical patent/GB950722A/en
Expired 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
    • F02K9/92—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control incorporating means for reversing or terminating thrust
    • 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
    • F02K9/38—Safety devices, e.g. to prevent accidental ignition

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Engines (AREA)

Abstract

950,722. Rocket motors. BRISTOL AEROJET Ltd. May 30, 1960 [Feb. 28, 1959], No. 3234/59. Heading F3A. A control device for a rocket motor incorporates duets 16 in the casing 10 communicating with an annular chamber 14 within a sleeve 13, and a flanged band 21 which initially holds the sleeve until ruptured by a charge 20, ignited by means (not shown) at a predetermined missile speed, whereupon the motor gas pressure moves the sleeve along the casing to open at least two vents 12. In a modification, in the Figure (not shown) accompanying the Complete Specification the rocket motor has a cylindrical combustion chamber on which the slidable sleeve is held by shear pins fracturing when a predetermined pressure is exceeded. Rearward movement of the sleeve is checked by a lead shock-absorbing ring.
GB3234/59A 1959-02-28 1959-02-28 Control for a rocket motor Expired GB950722A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB3234/59A GB950722A (en) 1959-02-28 1959-02-28 Control for a rocket motor
DEB58589A DE1154674B (en) 1959-02-28 1960-07-13 Control or safety device for a solid rocket engine
FR832987A FR1262426A (en) 1959-02-28 1960-07-15 Control or safety device for rocket motors using solid fuel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3234/59A GB950722A (en) 1959-02-28 1959-02-28 Control for a rocket motor

Publications (1)

Publication Number Publication Date
GB950722A true GB950722A (en) 1964-02-26

Family

ID=9754473

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3234/59A Expired GB950722A (en) 1959-02-28 1959-02-28 Control for a rocket motor

Country Status (2)

Country Link
FR (1) FR1262426A (en)
GB (1) GB950722A (en)

Also Published As

Publication number Publication date
FR1262426A (en) 1961-05-26

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