GB923320A - Injector head for rockets - Google Patents

Injector head for rockets

Info

Publication number
GB923320A
GB923320A GB334061A GB334061A GB923320A GB 923320 A GB923320 A GB 923320A GB 334061 A GB334061 A GB 334061A GB 334061 A GB334061 A GB 334061A GB 923320 A GB923320 A GB 923320A
Authority
GB
United Kingdom
Prior art keywords
propellant
chamber
injector head
issues
plates
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
GB334061A
Inventor
Walter A Ledwith
Augustus Hasbrouck
Frank Lattanzio
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.)
Raytheon Technologies Corp
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
Priority to US821067A priority Critical patent/US3115009A/en
Application filed by United Aircraft Corp filed Critical United Aircraft Corp
Priority to GB334061A priority patent/GB923320A/en
Priority to DEU7787A priority patent/DE1151987B/en
Priority to FR856525A priority patent/FR1324919A/en
Publication of GB923320A publication Critical patent/GB923320A/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
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F02K9/52—Injectors

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

923,320. Generating combustion products under pressure. UNITED AIRCRAFT CORPORATION. Jan. 27, 1961, No. 3340/61. Class 51 (1). [Also in Group XXVI] The injector head 4 of the rocket chamber 8 is formed of plates 14, 32 so as to permit the injection of liquid fuel and oxidizer into 8 through the nozzles 24 and annular passages 36. The cap 28 and duct 29 form a chamber 26 from which one propellant issues through the nozzle. The second propellant is supplied from inlet 42, through the annular manifold 50 to the chamber 38 between plates 14, 32 from which the propellant issues through passages 36. The controlling located opening 6 carries an igniter (not shown).
GB334061A 1959-06-17 1961-01-27 Injector head for rockets Expired GB923320A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
US821067A US3115009A (en) 1959-06-17 1959-06-17 Injector head for rockets
GB334061A GB923320A (en) 1961-01-27 1961-01-27 Injector head for rockets
DEU7787A DE1151987B (en) 1961-01-27 1961-02-13 Missile injection head
FR856525A FR1324919A (en) 1961-01-27 1961-03-23 Rocket injection head

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB334061A GB923320A (en) 1961-01-27 1961-01-27 Injector head for rockets

Publications (1)

Publication Number Publication Date
GB923320A true GB923320A (en) 1963-04-10

Family

ID=9756474

Family Applications (1)

Application Number Title Priority Date Filing Date
GB334061A Expired GB923320A (en) 1959-06-17 1961-01-27 Injector head for rockets

Country Status (1)

Country Link
GB (1) GB923320A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109695515A (en) * 2019-02-01 2019-04-30 北京星际荣耀空间科技有限公司 Total assembling structure, rocket engine, liquid rocket
CN111412086A (en) * 2020-05-21 2020-07-14 安徽九州云箭航天技术有限公司 Weldless injector for liquid rocket engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109695515A (en) * 2019-02-01 2019-04-30 北京星际荣耀空间科技有限公司 Total assembling structure, rocket engine, liquid rocket
CN111412086A (en) * 2020-05-21 2020-07-14 安徽九州云箭航天技术有限公司 Weldless injector for liquid rocket engine

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