GB8619036D0 - Rocket motor extendible nozzle exit cone - Google Patents

Rocket motor extendible nozzle exit cone

Info

Publication number
GB8619036D0
GB8619036D0 GB868619036A GB8619036A GB8619036D0 GB 8619036 D0 GB8619036 D0 GB 8619036D0 GB 868619036 A GB868619036 A GB 868619036A GB 8619036 A GB8619036 A GB 8619036A GB 8619036 D0 GB8619036 D0 GB 8619036D0
Authority
GB
United Kingdom
Prior art keywords
rocket motor
nozzle exit
exit cone
extendible nozzle
motor extendible
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.)
Granted
Application number
GB868619036A
Other versions
GB2179877A (en
GB2179877B (en
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.)
ATK Launch Systems LLC
Original Assignee
Morton Thiokol Inc
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 Morton Thiokol Inc filed Critical Morton Thiokol Inc
Publication of GB8619036D0 publication Critical patent/GB8619036D0/en
Publication of GB2179877A publication Critical patent/GB2179877A/en
Application granted granted Critical
Publication of GB2179877B publication Critical patent/GB2179877B/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
    • F02K9/97—Rocket nozzles
    • F02K9/976—Deployable nozzles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/401—Liquid propellant rocket engines
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/403—Solid propellant rocket engines

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Nozzles (AREA)
  • Shaping Metal By Deep-Drawing, Or The Like (AREA)
GB8619036A 1985-08-05 1986-08-05 Rocket motor extendible nozzle exit cone Expired GB2179877B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US76247285A 1985-08-05 1985-08-05

Publications (3)

Publication Number Publication Date
GB8619036D0 true GB8619036D0 (en) 1986-09-17
GB2179877A GB2179877A (en) 1987-03-18
GB2179877B GB2179877B (en) 1989-08-23

Family

ID=25065149

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8619036A Expired GB2179877B (en) 1985-08-05 1986-08-05 Rocket motor extendible nozzle exit cone

Country Status (3)

Country Link
JP (1) JPS6291647A (en)
FR (1) FR2585771B1 (en)
GB (1) GB2179877B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113153581A (en) * 2021-04-28 2021-07-23 哈尔滨工程大学 Flexible double-bell-shaped spray pipe with structure of flow charging pipeline coated by extensible material

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6183837B2 (en) * 2013-08-19 2017-08-23 国立研究開発法人宇宙航空研究開発機構 Exhaust nozzle

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113153581A (en) * 2021-04-28 2021-07-23 哈尔滨工程大学 Flexible double-bell-shaped spray pipe with structure of flow charging pipeline coated by extensible material
CN113153581B (en) * 2021-04-28 2022-11-15 哈尔滨工程大学 Flexible double-bell-shaped spray pipe with structure of flow charging pipeline coated by extensible material

Also Published As

Publication number Publication date
JPH0353463B2 (en) 1991-08-15
GB2179877A (en) 1987-03-18
GB2179877B (en) 1989-08-23
FR2585771A1 (en) 1987-02-06
JPS6291647A (en) 1987-04-27
FR2585771B1 (en) 1991-01-25

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19950805