CH410527A - Feststoffrakete mit innenbrennendem Treibsatz - Google Patents

Feststoffrakete mit innenbrennendem Treibsatz

Info

Publication number
CH410527A
CH410527A CH80363A CH80363A CH410527A CH 410527 A CH410527 A CH 410527A CH 80363 A CH80363 A CH 80363A CH 80363 A CH80363 A CH 80363A CH 410527 A CH410527 A CH 410527A
Authority
CH
Switzerland
Prior art keywords
solid rocket
internal propellant
propellant
internal
rocket
Prior art date
Application number
CH80363A
Other languages
German (de)
English (en)
Inventor
Renner Hermann
Karl-Otto Dipl Ing Wehlow
Original Assignee
Rheinmetall Gmbh
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 Rheinmetall Gmbh filed Critical Rheinmetall Gmbh
Publication of CH410527A publication Critical patent/CH410527A/de

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
    • 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
    • F02K9/18—Shape or structure of solid propellant charges of the internal-burning type having a star or like shaped internal cavity
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Engines (AREA)
  • Gasket Seals (AREA)
CH80363A 1962-01-30 1963-01-21 Feststoffrakete mit innenbrennendem Treibsatz CH410527A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DER31998A DE1161453B (de) 1962-01-30 1962-01-30 Feststoffraketen-Treibsatz

Publications (1)

Publication Number Publication Date
CH410527A true CH410527A (de) 1966-03-31

Family

ID=7403717

Family Applications (1)

Application Number Title Priority Date Filing Date
CH80363A CH410527A (de) 1962-01-30 1963-01-21 Feststoffrakete mit innenbrennendem Treibsatz

Country Status (5)

Country Link
US (1) US3260045A (enEXAMPLES)
BE (1) BE627648A (enEXAMPLES)
CH (1) CH410527A (enEXAMPLES)
DE (1) DE1161453B (enEXAMPLES)
GB (1) GB1019043A (enEXAMPLES)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4781117A (en) * 1987-07-20 1988-11-01 The United States Of America As Represented By The Secretary Of The Navy Fragmentable warhead of modular construction

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2235283A1 (en) * 1973-06-29 1975-01-24 Poudres & Explosifs Ste Nale Propellant blocks for rockers - with central combustion channel having unequal branches
FR2500149B1 (fr) * 1981-02-17 1985-12-06 Poudres & Explosifs Ste Nale Chargement propulsif biregime a canal en trompette comportant une section en etoile
RU2211356C1 (ru) * 2002-01-15 2003-08-27 Федеральное государственное унитарное предприятие "Научно-исследовательский институт полимерных материалов" Ракетный двигатель твердого топлива

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2957307A (en) * 1956-11-06 1960-10-25 Amcel Propulsion Inc Powder propellant rocket motors
US2957309A (en) * 1957-07-22 1960-10-25 Phillips Petroleum Co Rocket motor
GB844245A (en) * 1958-11-25 1960-08-10 Ici Ltd Improvements in or relating to rocket motors

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4781117A (en) * 1987-07-20 1988-11-01 The United States Of America As Represented By The Secretary Of The Navy Fragmentable warhead of modular construction

Also Published As

Publication number Publication date
DE1161453B (de) 1964-01-16
GB1019043A (en) 1966-02-02
BE627648A (enEXAMPLES)
US3260045A (en) 1966-07-12

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