[go: up one dir, main page]

GB2505629B - Segmented carbon-carbon exit cone assembly - Google Patents

Segmented carbon-carbon exit cone assembly

Info

Publication number
GB2505629B
GB2505629B GB8525645A GB8525645A GB2505629B GB 2505629 B GB2505629 B GB 2505629B GB 8525645 A GB8525645 A GB 8525645A GB 8525645 A GB8525645 A GB 8525645A GB 2505629 B GB2505629 B GB 2505629B
Authority
GB
United Kingdom
Prior art keywords
carbon
segmented
cone assembly
exit cone
assembly
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 - Lifetime
Application number
GB8525645A
Other versions
GB2505629A (en
GB8525645D0 (en
Inventor
Donald C Giedt
Frank S Inman
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
Priority to GB8525645A priority Critical patent/GB2505629B/en
Anticipated expiration legal-status Critical
Publication of GB8525645D0 publication Critical patent/GB8525645D0/en
Publication of GB2505629A publication Critical patent/GB2505629A/en
Application granted granted Critical
Publication of GB2505629B publication Critical patent/GB2505629B/en
Expired - Lifetime 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
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/50—Building or constructing in particular ways
    • F05D2230/51—Building or constructing in particular ways in a modular way, e.g. using several identical or complementary parts or features
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/29—Three-dimensional machined; miscellaneous
    • F05D2250/292—Three-dimensional machined; miscellaneous tapered
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/20—Oxide or non-oxide ceramics
    • F05D2300/22—Non-oxide ceramics
    • F05D2300/224—Carbon, e.g. graphite

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Moulding By Coating Moulds (AREA)
GB8525645A 1985-10-17 1985-10-17 Segmented carbon-carbon exit cone assembly Expired - Lifetime GB2505629B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8525645A GB2505629B (en) 1985-10-17 1985-10-17 Segmented carbon-carbon exit cone assembly

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8525645A GB2505629B (en) 1985-10-17 1985-10-17 Segmented carbon-carbon exit cone assembly

Publications (3)

Publication Number Publication Date
GB8525645D0 GB8525645D0 (en) 2013-10-16
GB2505629A GB2505629A (en) 2014-03-12
GB2505629B true GB2505629B (en) 2014-11-26

Family

ID=49396985

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8525645A Expired - Lifetime GB2505629B (en) 1985-10-17 1985-10-17 Segmented carbon-carbon exit cone assembly

Country Status (1)

Country Link
GB (1) GB2505629B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11028802B2 (en) 2016-11-14 2021-06-08 Northrop Grumman Systems Corporation Liquid rocket engine assemblies and related methods

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114922747B (en) * 2022-06-21 2023-11-14 北京星河动力航天科技股份有限公司 Liquid rocket engine, nozzle thereof and extension part of nozzle

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2127771A (en) * 1982-09-29 1984-04-18 Avco Corp Fiber composite

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2127771A (en) * 1982-09-29 1984-04-18 Avco Corp Fiber composite

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11028802B2 (en) 2016-11-14 2021-06-08 Northrop Grumman Systems Corporation Liquid rocket engine assemblies and related methods
US11846256B2 (en) 2016-11-14 2023-12-19 Northrop Grumman Systems Corporation Liquid rocket engine assemblies and related methods

Also Published As

Publication number Publication date
GB2505629A (en) 2014-03-12
GB8525645D0 (en) 2013-10-16

Similar Documents

Publication Publication Date Title
GB8617381D0 (en) Installation
DE3663598D1 (en) Nuclear-fuel assembly
GB8606907D0 (en) Assembly
GB8515557D0 (en) Support assembly
EP0205664A3 (en) Brake support assembly
GB2505629B (en) Segmented carbon-carbon exit cone assembly
GB2172556B (en) An improved sideguard assembly
GB2170388B (en) Material-separating assemblies
GB8607723D0 (en) Lining hollow member
EP0194013A3 (en) Parachute
GB8608662D0 (en) Brakepad assembly
GB8602825D0 (en) Transformer-impedance assembly
GB8618685D0 (en) Cutter-bit assemblies
GB8613428D0 (en) Headwork assemblies
GB8524728D0 (en) Support assembly
GB2171439B (en) Traffic cone
ZA869274B (en) Screening assembly
IE851150L (en) Parachute
GB8503399D0 (en) Traffic cone
GB8507246D0 (en) Channel section members
CS951685A1 (en) List pruziny
AU94887S (en) An extruded section
AU94886S (en) An extruded section
GB8510141D0 (en) Support assembly
IE850438L (en) Laidlomycin phenylcarbamate

Legal Events

Date Code Title Description
PE20 Patent expired after termination of 20 years

Expiry date: 20051016