GB8800422D0 - Solid rocket motor propellants with reticulated structures embedded therein to provide variable burn rate characteristics - Google Patents

Solid rocket motor propellants with reticulated structures embedded therein to provide variable burn rate characteristics

Info

Publication number
GB8800422D0
GB8800422D0 GB888800422A GB8800422A GB8800422D0 GB 8800422 D0 GB8800422 D0 GB 8800422D0 GB 888800422 A GB888800422 A GB 888800422A GB 8800422 A GB8800422 A GB 8800422A GB 8800422 D0 GB8800422 D0 GB 8800422D0
Authority
GB
United Kingdom
Prior art keywords
rate characteristics
rocket motor
burn rate
provide variable
solid rocket
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.)
Withdrawn
Application number
GB888800422A
Other versions
GB2214275A (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
Priority claimed from US06/908,762 external-priority patent/US4756251A/en
Application filed by Morton Thiokol Inc filed Critical Morton Thiokol Inc
Publication of GB8800422D0 publication Critical patent/GB8800422D0/en
Publication of GB2214275A publication Critical patent/GB2214275A/en
Withdrawn legal-status Critical Current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
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/26—Burning control
    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B45/00—Compositions or products which are defined by structure or arrangement of component of product
GB8800422A 1986-09-18 1988-01-08 Propellant grain Withdrawn GB2214275A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/908,762 US4756251A (en) 1986-09-18 1986-09-18 Solid rocket motor propellants with reticulated structures embedded therein to provide variable burn rate characteristics

Publications (2)

Publication Number Publication Date
GB8800422D0 true GB8800422D0 (en) 1988-06-02
GB2214275A GB2214275A (en) 1989-08-31

Family

ID=25426215

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8800422A Withdrawn GB2214275A (en) 1986-09-18 1988-01-08 Propellant grain

Country Status (1)

Country Link
GB (1) GB2214275A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10035174B2 (en) 2015-02-09 2018-07-31 United Technologies Corporation Open-cell reticulated foam

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB885409A (en) * 1958-04-14 1961-12-28 Hexcel Products Inc Fuel grains for rocket engines
US3509822A (en) * 1960-06-09 1970-05-05 Susquehanna Corp Propellent grains
GB972724A (en) * 1961-05-19 1964-10-14 Atlantic Res Corp Rocket motor
US3499283A (en) * 1965-12-23 1970-03-10 Thiokol Chemical Corp Rocket charge design
US3616841A (en) * 1967-10-30 1971-11-02 Energy Research And Generation Method of making an inorganic reticulated foam structure
US3946039A (en) * 1967-10-30 1976-03-23 Energy Research & Generation, Inc. Reticulated foam structure
US4574700A (en) * 1984-11-15 1986-03-11 The United States Of America As Represented By The Secretary Of The Air Force Solid rocket motor with nozzle containing aromatic amide fibers

Also Published As

Publication number Publication date
GB2214275A (en) 1989-08-31

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)