DE2605768C2 - Radialbrenner mit Festtreibstoffsatz für ein Raketengeschoß - Google Patents

Radialbrenner mit Festtreibstoffsatz für ein Raketengeschoß

Info

Publication number
DE2605768C2
DE2605768C2 DE2605768A DE2605768A DE2605768C2 DE 2605768 C2 DE2605768 C2 DE 2605768C2 DE 2605768 A DE2605768 A DE 2605768A DE 2605768 A DE2605768 A DE 2605768A DE 2605768 C2 DE2605768 C2 DE 2605768C2
Authority
DE
Germany
Prior art keywords
radial
solid propellant
projectile
combustion chamber
nozzle
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
DE2605768A
Other languages
German (de)
English (en)
Other versions
DE2605768A1 (de
Inventor
Manfred Dipl.-Ing. 4000 Düsseldorf Moll
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.)
Rheinmetall Industrie AG
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
Priority to DE2605768A priority Critical patent/DE2605768C2/de
Priority to SE7701241A priority patent/SE7701241L/xx
Priority to GB5448/77A priority patent/GB1563364A/en
Priority to US05/767,379 priority patent/US4104969A/en
Priority to FR7703875A priority patent/FR2341047A1/fr
Publication of DE2605768A1 publication Critical patent/DE2605768A1/de
Application granted granted Critical
Publication of DE2605768C2 publication Critical patent/DE2605768C2/de
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
    • F02K9/95—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by starting or ignition means or arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Finger-Pressure Massage (AREA)
DE2605768A 1976-02-13 1976-02-13 Radialbrenner mit Festtreibstoffsatz für ein Raketengeschoß Expired DE2605768C2 (de)

Priority Applications (5)

Application Number Priority Date Filing Date Title
DE2605768A DE2605768C2 (de) 1976-02-13 1976-02-13 Radialbrenner mit Festtreibstoffsatz für ein Raketengeschoß
SE7701241A SE7701241L (sv) 1976-02-13 1977-02-04 Sett att forbettra driftforhallandet hos en radialbrennare for en raketprojektil och radialbrennare med en anordning for settets utforande
GB5448/77A GB1563364A (en) 1976-02-13 1977-02-09 Rocket propulsion units having radially consumable propulsive charges
US05/767,379 US4104969A (en) 1976-02-13 1977-02-10 Arrangement for improving the burning efficiency of a rocket-borne solid propellant charge cartridge
FR7703875A FR2341047A1 (fr) 1976-02-13 1977-02-11 Procede d'amelioration des caracteristiques de fonctionnement d'un projectile auto-propulse ayant une charge a combution radiale, et bruleur a charge a combustion radiale

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2605768A DE2605768C2 (de) 1976-02-13 1976-02-13 Radialbrenner mit Festtreibstoffsatz für ein Raketengeschoß

Publications (2)

Publication Number Publication Date
DE2605768A1 DE2605768A1 (de) 1977-08-18
DE2605768C2 true DE2605768C2 (de) 1982-09-23

Family

ID=5969815

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2605768A Expired DE2605768C2 (de) 1976-02-13 1976-02-13 Radialbrenner mit Festtreibstoffsatz für ein Raketengeschoß

Country Status (5)

Country Link
US (1) US4104969A (enExample)
DE (1) DE2605768C2 (enExample)
FR (1) FR2341047A1 (enExample)
GB (1) GB1563364A (enExample)
SE (1) SE7701241L (enExample)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3246380A1 (de) * 1982-12-15 1984-06-20 Diehl GmbH & Co, 8500 Nürnberg Vorrichtung zur reduzierung des bodenwiderstandes bei geschossen
FR2574480B1 (fr) * 1984-12-10 1987-02-13 Matra Dispositif comportant une charge utile et un propulseur a tuyere deplacable longitudinalement
DE8908723U1 (de) * 1989-07-18 1989-11-16 Josef Lubig GmbH, 5300 Bonn Düsenbefestigung
US5440993A (en) * 1990-12-07 1995-08-15 Osofsky; Irving B. High velocity impulse rocket
US5309712A (en) * 1991-05-03 1994-05-10 Mund Jr Charles J Solid fuel rocket motor seals
RU2260143C2 (ru) * 2003-12-04 2005-09-10 Федеральное государственное унитарное предприятие "Научно-исследовательский институт полимерных материалов" Твердотопливный газогенератор

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1347125A (en) * 1919-02-28 1920-07-20 Schneider & Cie Projectile for bomb-throwers
US2426239A (en) * 1942-12-28 1947-08-26 Henry M Renner Rocket shell
NL246977A (enExample) * 1958-12-31
US3306204A (en) * 1962-10-05 1967-02-28 Aerojet General Co Rocket projectile with supported propellant grain
US3490373A (en) * 1968-05-09 1970-01-20 Thiokol Chemical Corp Self-destructing rocket propelled grenade
US3583162A (en) * 1969-03-07 1971-06-08 Thiokol Chemical Corp Closure and solid propellant grain support for a solid propellant rocket motor
DE1915878C3 (de) * 1969-03-28 1974-07-18 Arnold Ingemar Groedinge Magnusson Raketenbrennkammer für ein Raketengeschoß
US3698321A (en) * 1969-10-29 1972-10-17 Thiokol Chemical Corp Rocket assisted projectile
FR2240427B1 (enExample) * 1973-08-09 1976-11-19 Thomson Brandt
FR2277982A1 (fr) * 1974-07-11 1976-02-06 Europ Propulsion Propulseur monochambre a tuyere libre

Also Published As

Publication number Publication date
US4104969A (en) 1978-08-08
FR2341047B1 (enExample) 1983-02-18
GB1563364A (en) 1980-03-26
SE7701241L (sv) 1977-08-14
FR2341047A1 (fr) 1977-09-09
DE2605768A1 (de) 1977-08-18

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Legal Events

Date Code Title Description
OD Request for examination
D2 Grant after examination
8339 Ceased/non-payment of the annual fee