FR1522555A - Dispositif de gouverne par déviation de jet - Google Patents

Dispositif de gouverne par déviation de jet

Info

Publication number
FR1522555A
FR1522555A FR99373A FR99373A FR1522555A FR 1522555 A FR1522555 A FR 1522555A FR 99373 A FR99373 A FR 99373A FR 99373 A FR99373 A FR 99373A FR 1522555 A FR1522555 A FR 1522555A
Authority
FR
France
Prior art keywords
steering device
jet deflection
deflection
jet
steering
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
FR99373A
Other languages
English (en)
Inventor
Don Pierre Louis Jea Colombani
Adolphe Otton Gontier Ernst
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 FR99373A priority Critical patent/FR1522555A/fr
Priority to GB1248968A priority patent/GB1215231A/en
Priority to DE19686607645 priority patent/DE6607645U/de
Application granted granted Critical
Publication of FR1522555A publication Critical patent/FR1522555A/fr
Expired legal-status Critical Current

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
    • F02K9/80Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/82Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control by injection of a secondary fluid into the rocket exhaust gases

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Testing Of Engines (AREA)
FR99373A 1967-03-17 1967-03-17 Dispositif de gouverne par déviation de jet Expired FR1522555A (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR99373A FR1522555A (fr) 1967-03-17 1967-03-17 Dispositif de gouverne par déviation de jet
GB1248968A GB1215231A (en) 1967-03-17 1968-03-14 Direction-controlling and nozzle-cooling means for rocket-engine propelled vehicles
DE19686607645 DE6607645U (de) 1967-03-17 1968-03-15 Durch einen raketenmotor angetriebenes luftfahrzeug.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR99373A FR1522555A (fr) 1967-03-17 1967-03-17 Dispositif de gouverne par déviation de jet

Publications (1)

Publication Number Publication Date
FR1522555A true FR1522555A (fr) 1968-04-26

Family

ID=8627156

Family Applications (1)

Application Number Title Priority Date Filing Date
FR99373A Expired FR1522555A (fr) 1967-03-17 1967-03-17 Dispositif de gouverne par déviation de jet

Country Status (3)

Country Link
DE (1) DE6607645U (fr)
FR (1) FR1522555A (fr)
GB (1) GB1215231A (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0015216A1 (fr) * 1979-02-27 1980-09-03 AEROSPATIALE Société Nationale Industrielle Agencement de pilotage d'un propulseur d'engin à propergol solide
US5816539A (en) * 1994-02-18 1998-10-06 Lockheed Martin Corporation Orbital assist module and interstage

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0015216A1 (fr) * 1979-02-27 1980-09-03 AEROSPATIALE Société Nationale Industrielle Agencement de pilotage d'un propulseur d'engin à propergol solide
FR2450356A1 (fr) * 1979-02-27 1980-09-26 Aerospatiale Agencement de pilotage d'un propulseur d'engin a propergol solide
US5816539A (en) * 1994-02-18 1998-10-06 Lockheed Martin Corporation Orbital assist module and interstage

Also Published As

Publication number Publication date
GB1215231A (en) 1970-12-09
DE6607645U (de) 1971-04-01

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