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GB989880A - Improvements in or relating to rocket projectiles - Google Patents

Improvements in or relating to rocket projectiles

Info

Publication number
GB989880A
GB989880A GB2402257A GB2402257A GB989880A GB 989880 A GB989880 A GB 989880A GB 2402257 A GB2402257 A GB 2402257A GB 2402257 A GB2402257 A GB 2402257A GB 989880 A GB989880 A GB 989880A
Authority
GB
United Kingdom
Prior art keywords
orifices
gases
chamber
july
relating
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
GB2402257A
Inventor
Reginald John Rosser
Arthur Gwynfryn Walters
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.)
SECR AVIATION
Minister of Aviation
Original Assignee
SECR AVIATION
Minister of Aviation
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 SECR AVIATION, Minister of Aviation filed Critical SECR AVIATION
Priority to GB2402257A priority Critical patent/GB989880A/en
Publication of GB989880A publication Critical patent/GB989880A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/02—Stabilising arrangements
    • F42B10/26—Stabilising arrangements using spin
    • F42B10/28—Stabilising arrangements using spin induced by gas action
    • F42B10/30—Stabilising arrangements using spin induced by gas action using rocket motor nozzles
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Toys (AREA)

Abstract

989,880. Rocket motor. MINISTER OF AVIATION. July 1, 1958 [July 29, 1957], No. 24022/57. Heading F3A. In a rocket projectile, inaccuracy of flight due to asymmetry of combustion-gas flow, is reduced by baffles which deflect the gases through several small, internal, orifices to a chamber in which the gases are remixed and then ejected from the propulsion nozzles. As shown, the gases from the propellant charge 4 pass to the propulsion nozzle 11 through the annular space 7, the orifices 12 in the baffle plate 1 and the mixing chamber 2. The orifices may be set at angle to the radii to produce swirling in chamber 2.
GB2402257A 1957-07-29 1957-07-29 Improvements in or relating to rocket projectiles Expired GB989880A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2402257A GB989880A (en) 1957-07-29 1957-07-29 Improvements in or relating to rocket projectiles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2402257A GB989880A (en) 1957-07-29 1957-07-29 Improvements in or relating to rocket projectiles

Publications (1)

Publication Number Publication Date
GB989880A true GB989880A (en) 1965-04-22

Family

ID=10205136

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2402257A Expired GB989880A (en) 1957-07-29 1957-07-29 Improvements in or relating to rocket projectiles

Country Status (1)

Country Link
GB (1) GB989880A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1751740B1 (en) * 1968-07-20 1971-06-16 Kayser Lutz Tilo Rocket engine for liquid and / or gaseous fuels

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1751740B1 (en) * 1968-07-20 1971-06-16 Kayser Lutz Tilo Rocket engine for liquid and / or gaseous fuels

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