GB746214A - Improvements relating to rocket motors - Google Patents

Improvements relating to rocket motors

Info

Publication number
GB746214A
GB746214A GB14391/54A GB1439154A GB746214A GB 746214 A GB746214 A GB 746214A GB 14391/54 A GB14391/54 A GB 14391/54A GB 1439154 A GB1439154 A GB 1439154A GB 746214 A GB746214 A GB 746214A
Authority
GB
United Kingdom
Prior art keywords
lining
insulating
heat
casing
propellant
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
GB14391/54A
Other languages
English (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.)
Saab Bofors AB
Original Assignee
Bofors AB
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 Bofors AB filed Critical Bofors AB
Publication of GB746214A publication Critical patent/GB746214A/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
    • F02K9/08—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
    • F02K9/34—Casings; Combustion chambers; Liners thereof
    • F02K9/346—Liners, e.g. inhibitors

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Thermal Insulation (AREA)
  • Laminated Bodies (AREA)
GB14391/54A 1953-05-19 1954-05-17 Improvements relating to rocket motors Expired GB746214A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE746214X 1953-05-19

Publications (1)

Publication Number Publication Date
GB746214A true GB746214A (en) 1956-03-14

Family

ID=20323228

Family Applications (1)

Application Number Title Priority Date Filing Date
GB14391/54A Expired GB746214A (en) 1953-05-19 1954-05-17 Improvements relating to rocket motors

Country Status (3)

Country Link
BE (1) BE528963A (enrdf_load_stackoverflow)
FR (1) FR1100712A (enrdf_load_stackoverflow)
GB (1) GB746214A (enrdf_load_stackoverflow)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3010355A (en) * 1957-06-10 1961-11-28 Phillips Petroleum Co Method for making a rocket motor
US3017744A (en) * 1957-07-11 1962-01-23 James A Jett Propellant grain and rocket motor
US3077734A (en) * 1956-12-10 1963-02-19 Phillips Petroleum Co Solid-propellant rocket motor
US3235183A (en) * 1963-05-29 1966-02-15 United Aircraft Corp Ablation cooled rocket nozzle
DE1214476B (de) * 1956-12-21 1966-04-14 Haveg Industries Inc Hochtemperaturfestes Bau- bzw. Schutzschicht-material fuer Raketenbrennkammern oder Flugkoerperaussenhuellen
US3301785A (en) * 1960-05-02 1967-01-31 North American Aviation Inc Insulated solid propellant rocket motor
US5280706A (en) * 1992-06-25 1994-01-25 Thiokol Corporation Composite/metal hybrid rocket motor case and methods for manufacturing
US5564272A (en) * 1994-07-29 1996-10-15 Thiokol Corporation Slotted hybrid pressure vessel
RU2304726C2 (ru) * 2005-09-28 2007-08-20 Открытое акционерное общество "Институт прикладной физики" Корпус ракетного двигателя на твердом топливе
RU2831320C2 (ru) * 2005-09-28 2024-12-04 Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации Корпус ракетного двигателя на твердом топливе

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3077734A (en) * 1956-12-10 1963-02-19 Phillips Petroleum Co Solid-propellant rocket motor
DE1214476B (de) * 1956-12-21 1966-04-14 Haveg Industries Inc Hochtemperaturfestes Bau- bzw. Schutzschicht-material fuer Raketenbrennkammern oder Flugkoerperaussenhuellen
US3010355A (en) * 1957-06-10 1961-11-28 Phillips Petroleum Co Method for making a rocket motor
US3017744A (en) * 1957-07-11 1962-01-23 James A Jett Propellant grain and rocket motor
US3301785A (en) * 1960-05-02 1967-01-31 North American Aviation Inc Insulated solid propellant rocket motor
US3235183A (en) * 1963-05-29 1966-02-15 United Aircraft Corp Ablation cooled rocket nozzle
US5280706A (en) * 1992-06-25 1994-01-25 Thiokol Corporation Composite/metal hybrid rocket motor case and methods for manufacturing
US5348603A (en) * 1992-06-25 1994-09-20 Thiokol Corporation Composite/metal hybrid rocket motor case and methods for manufacturing
US5564272A (en) * 1994-07-29 1996-10-15 Thiokol Corporation Slotted hybrid pressure vessel
RU2304726C2 (ru) * 2005-09-28 2007-08-20 Открытое акционерное общество "Институт прикладной физики" Корпус ракетного двигателя на твердом топливе
RU2418186C2 (ru) * 2005-09-28 2011-05-10 Виктор Фридрихович Ланг Корпус ракетного двигателя на твердом топливе
RU2831320C2 (ru) * 2005-09-28 2024-12-04 Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации Корпус ракетного двигателя на твердом топливе

Also Published As

Publication number Publication date
BE528963A (enrdf_load_stackoverflow)
FR1100712A (fr) 1955-09-23

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