CH270050A - Charge propulsive pour fusées. - Google Patents

Charge propulsive pour fusées.

Info

Publication number
CH270050A
CH270050A CH270050DA CH270050A CH 270050 A CH270050 A CH 270050A CH 270050D A CH270050D A CH 270050DA CH 270050 A CH270050 A CH 270050A
Authority
CH
Switzerland
Prior art keywords
rockets
propellant charge
propellant
charge
Prior art date
Application number
Other languages
English (en)
French (fr)
Inventor
Corporation Aeroje Engineering
Original Assignee
Aerojet Engineering Corp
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 Aerojet Engineering Corp filed Critical Aerojet Engineering Corp
Publication of CH270050A publication Critical patent/CH270050A/fr

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32Constructional parts; Details not otherwise provided for
    • F02K9/36Propellant charge supports
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C35/00Flying-boats; Seaplanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32Constructional parts; Details not otherwise provided for
    • F02K9/34Casings; Combustion chambers; Liners thereof

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
CH270050D 1945-05-28 1947-12-31 Charge propulsive pour fusées. CH270050A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US270050XA 1945-05-28 1945-05-28

Publications (1)

Publication Number Publication Date
CH270050A true CH270050A (fr) 1950-08-15

Family

ID=21835107

Family Applications (1)

Application Number Title Priority Date Filing Date
CH270050D CH270050A (fr) 1945-05-28 1947-12-31 Charge propulsive pour fusées.

Country Status (6)

Country Link
BE (1) BE481853A (en)van)
CH (1) CH270050A (en)van)
FR (1) FR959832A (en)van)
GB (1) GB660789A (en)van)
LU (1) LU29004A1 (en)van)
NL (1) NL71198C (en)van)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108590886A (zh) * 2018-05-23 2018-09-28 精功(绍兴)复合材料有限公司 鸟笼式火箭发动机壳体缠绕成型模具及其制备方法

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3005692A (en) * 1956-09-21 1961-10-24 Phillips Petroleum Co Coated ammonium nitrate propellants
US5062365A (en) * 1986-08-18 1991-11-05 Thiokol Corporation Rapid burning propellent charge for automobile air bag inflators, rocket motors, and igniters therefor
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
CN112391002B (zh) * 2019-08-16 2022-05-27 南京理工大学 一种用于固体推进剂的热收缩包覆层及制备方法
CN113147009B (zh) * 2021-03-12 2022-12-30 哈尔滨玻璃钢研究院有限公司 一种大尺寸纤维带药缠绕成型发动机壳体工艺方法

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108590886A (zh) * 2018-05-23 2018-09-28 精功(绍兴)复合材料有限公司 鸟笼式火箭发动机壳体缠绕成型模具及其制备方法

Also Published As

Publication number Publication date
FR959832A (en)van) 1950-04-06
GB660789A (en) 1951-11-14
BE481853A (en)van)
NL71198C (en)van)
LU29004A1 (en)van)

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