FR1423944A - Rocket propulsion shutdown device - Google Patents

Rocket propulsion shutdown device

Info

Publication number
FR1423944A
FR1423944A FR996413A FR996413A FR1423944A FR 1423944 A FR1423944 A FR 1423944A FR 996413 A FR996413 A FR 996413A FR 996413 A FR996413 A FR 996413A FR 1423944 A FR1423944 A FR 1423944A
Authority
FR
France
Prior art keywords
shutdown device
rocket propulsion
rocket
propulsion
shutdown
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
FR996413A
Other languages
French (fr)
Inventor
Don Pierre Louis Jea Colombani
Adolphe Otton Gontier Ernst
Janos Rona
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Priority to FR996413A priority Critical patent/FR1423944A/en
Application granted granted Critical
Publication of FR1423944A publication Critical patent/FR1423944A/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
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/90—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using deflectors
    • 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
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/92—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control incorporating means for reversing or terminating thrust

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR996413A 1964-11-26 1964-11-26 Rocket propulsion shutdown device Expired FR1423944A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR996413A FR1423944A (en) 1964-11-26 1964-11-26 Rocket propulsion shutdown device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR996413A FR1423944A (en) 1964-11-26 1964-11-26 Rocket propulsion shutdown device

Publications (1)

Publication Number Publication Date
FR1423944A true FR1423944A (en) 1966-01-07

Family

ID=8843428

Family Applications (1)

Application Number Title Priority Date Filing Date
FR996413A Expired FR1423944A (en) 1964-11-26 1964-11-26 Rocket propulsion shutdown device

Country Status (1)

Country Link
FR (1) FR1423944A (en)

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