NL261914A - - Google Patents

Info

Publication number
NL261914A
NL261914A NL261914DA NL261914A NL 261914 A NL261914 A NL 261914A NL 261914D A NL261914D A NL 261914DA NL 261914 A NL261914 A NL 261914A
Authority
NL
Netherlands
Application number
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.)
Publication of NL261914A publication Critical patent/NL261914A/xx

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
    • 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
    • F02K9/10—Shape or structure of solid propellant charges
    • 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
    • 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)
  • Paints Or Removers (AREA)
  • Epoxy Resins (AREA)
  • Laminated Bodies (AREA)
  • Reinforced Plastic Materials (AREA)
NL261914D 1960-03-04 NL261914A (instruction)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US12870A US3108433A (en) 1960-03-04 1960-03-04 Rocket motor and solid propellent grain with woven polymeric inhibitor coating

Publications (1)

Publication Number Publication Date
NL261914A true NL261914A (instruction)

Family

ID=21757132

Family Applications (2)

Application Number Title Priority Date Filing Date
NL120413D NL120413C (instruction) 1960-03-04
NL261914D NL261914A (instruction) 1960-03-04

Family Applications Before (1)

Application Number Title Priority Date Filing Date
NL120413D NL120413C (instruction) 1960-03-04

Country Status (6)

Country Link
US (1) US3108433A (instruction)
BE (1) BE630804A (instruction)
DE (1) DE1128344B (instruction)
DK (1) DK103003C (instruction)
GB (1) GB963490A (instruction)
NL (2) NL261914A (instruction)

Families Citing this family (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3311013A (en) * 1963-01-09 1967-03-28 Aerojet General Co Propellant liner
GB1100204A (en) * 1964-05-28 1968-01-24 Atlantic Res Corp Improvements in combustible gas-producing charges
US4085173A (en) * 1964-10-05 1978-04-18 Hercules Incorporated Manufacture of solid propellant
US3319424A (en) * 1965-09-30 1967-05-16 Frederick L Haake Method and means for supporting a ram-jet propellant
US3446018A (en) * 1966-12-08 1969-05-27 Thiokol Chemical Corp Liner for solid propellant rocket motor
DE1646309B1 (de) * 1967-03-10 1971-11-11 Messerschmitt Boelkow Blohm Leuchtsatz fuer den sichtbaren und infraroten Spektralbereich und Verfahren zu seiner Herstellung
FR2096975B1 (instruction) * 1970-07-22 1974-05-03 Onera (Off Nat Aerospatiale)
US3737348A (en) * 1970-12-29 1973-06-05 Us Army Headend suspension for a carpet roll solid propellant grain
US3712233A (en) * 1971-01-28 1973-01-23 Dow Chemical Co Caseless pyrotechnic smoldering munition
US4185557A (en) * 1972-04-28 1980-01-29 The United States Of America As Represented By The Secretary Of The Navy Stress reducing liner and method of fabrication
JPS533445B2 (instruction) * 1973-10-17 1978-02-07
US3928965A (en) * 1973-11-07 1975-12-30 Thiokol Corp Rocket motor construction
US3952506A (en) * 1973-11-07 1976-04-27 Thiokol Corporation Rocket motor construction
GB1604865A (en) * 1977-12-29 1981-12-16 Secr Defence Projectile tail fin units
US4362868A (en) * 1979-09-24 1982-12-07 The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britian And Northern Ireland Plasticized cellulose polymers
US4345427A (en) * 1979-10-26 1982-08-24 Thiokol Corporation Rocket motor or gas generator having controlled thrust or mass flow output
US5042385A (en) * 1983-01-24 1991-08-27 The United States Of America As Represented By The Secretary Of The Navy Inhibitor and barrier for use with high energy rocket propellants
US4495764A (en) * 1983-05-26 1985-01-29 The United States Of America As Represented By The Secretary Of The Air Force Integrated insulation wall assembly
US4892764A (en) * 1985-11-26 1990-01-09 Loctite Corporation Fiber/resin composites, and method of making the same
US5024160A (en) * 1986-08-18 1991-06-18 Thiokol Corporation Rapid burning propellant charge for automobile air bag inflators, rocket motors, and igniters therefor
EP0336023A1 (en) * 1988-03-24 1989-10-11 Thiokol Corporation Solid rocket motor propellant with imbedded reticulated structures
US4764319A (en) * 1986-09-18 1988-08-16 Morton Thiokol, Inc. High solids ratio solid rocket motor propellant grains and method of construction thereof
US5127223A (en) * 1986-09-18 1992-07-07 Thiokol Corporation Solid rocket motor propellants with reticulated structures embedded therein and method of manufacture thereof
RU2208695C2 (ru) * 2001-08-29 2003-07-20 Федеральное государственное унитарное предприятие "Пермский завод им. С.М. Кирова" Заряд твёрдого топлива
RU2201520C1 (ru) * 2002-01-29 2003-03-27 Федеральный центр двойных технологий "Союз" Модельный двигатель для определения скорости горения трт в напряженно-деформированном состоянии
US7014041B1 (en) 2003-01-08 2006-03-21 American Grease Stick Company Method of applying flowable material and container therefor
US6994910B2 (en) * 2003-01-09 2006-02-07 Guardian Industries Corp. Heat treatable coated article with niobium nitride IR reflecting layer
RU2298109C2 (ru) * 2005-07-18 2007-04-27 Федеральное государственное унитарное предприятие "Научно-исследовательский институт полимерных материалов" Твердотопливный заряд для ракетного двигателя и способ его изготовления
RU2418186C2 (ru) * 2005-09-28 2011-05-10 Виктор Фридрихович Ланг Корпус ракетного двигателя на твердом топливе
RU2310668C2 (ru) * 2005-12-20 2007-11-20 Федеральное государственное унитарное предприятие "Научно-исследовательский институт полимерных материалов" Связующий состав для пропитки армирующего материала при бронировании зарядов твердого ракетного топлива методом обмотки
RU2295509C1 (ru) * 2005-12-20 2007-03-20 Федеральное государственное унитарное предприятие "Научно-исследовательский институт полимерных материалов" Эпоксидная литьевая композиция для бронирования вкладных зарядов из смесевого твердого ракетного топлива
RU2330832C1 (ru) * 2007-01-25 2008-08-10 Федеральное государственное унитарное предприятие "Научно-исследовательский институт полимерных материалов" Эпоксидная литьевая композиция для бронирования вкладного заряда из смесевого твердого ракетного топлива
RU2355906C1 (ru) * 2007-10-04 2009-05-20 Федеральное государственное унитарное предприятие "Научно-исследовательский институт полимерных материалов" Заряд твердого ракетного топлива для двигателя авиационной ракеты
RU2472826C1 (ru) * 2011-06-27 2013-01-20 Открытое акционерное общество "Научно-исследовательский институт полимерных материалов" Термопластичный бронесостав для покрытия вкладного заряда смесевого медленногорящего твердого ракетного топлива
FR3005724A1 (fr) * 2013-05-17 2014-11-21 Herakles Generateur de gaz pyrotechnique
CN109651931B (zh) * 2019-01-18 2024-02-13 中国工程物理研究院化工材料研究所 一种提升pbx带孔板承载能力的局部涂覆结构及涂覆方法
CN112694372A (zh) * 2020-12-25 2021-04-23 石仲仑 一种环氧基复合推进剂、制备方法及其应用

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2917424A (en) * 1947-10-28 1959-12-15 Aerojet General Co Method of restricting the burning of a solid propellant charge
US2479828A (en) * 1947-11-20 1949-08-23 Aerojet Engineering Corp Propellant charge for rocket motors
DE974892C (de) * 1957-09-19 1961-05-25 Josef Schaberger & Co G M B H Verfahren zum Modifizieren der oberflaechlichen Abbrand-geschwindigkeit von kunstharzhaltigen Feststofftreibsaetzen

Also Published As

Publication number Publication date
DK103003C (da) 1965-11-01
DE1128344B (de) 1962-04-19
NL120413C (instruction)
GB963490A (en) 1964-07-08
BE630804A (instruction)
US3108433A (en) 1963-10-29

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