FR1414824A - Deformable connection device and its application to rockets - Google Patents

Deformable connection device and its application to rockets

Info

Publication number
FR1414824A
FR1414824A FR982999A FR982999A FR1414824A FR 1414824 A FR1414824 A FR 1414824A FR 982999 A FR982999 A FR 982999A FR 982999 A FR982999 A FR 982999A FR 1414824 A FR1414824 A FR 1414824A
Authority
FR
France
Prior art keywords
rockets
application
connection device
deformable connection
deformable
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
FR982999A
Other languages
French (fr)
Inventor
Andre Emile Dorangeon
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 FR982999A priority Critical patent/FR1414824A/en
Priority to DE1965S0098390 priority patent/DE1298371B/en
Priority to GB3139965A priority patent/GB1107635A/en
Application granted granted Critical
Publication of FR1414824A publication Critical patent/FR1414824A/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
    • F02K9/84—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using movable nozzles
    • 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
    • F02K9/97—Rocket nozzles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/666—Steering by varying intensity or direction of thrust characterised by using a nozzle rotatable about an axis transverse to the axis of the projectile

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Excavating Of Shafts Or Tunnels (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
FR982999A 1964-07-24 1964-07-24 Deformable connection device and its application to rockets Expired FR1414824A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR982999A FR1414824A (en) 1964-07-24 1964-07-24 Deformable connection device and its application to rockets
DE1965S0098390 DE1298371B (en) 1964-07-24 1965-07-23 Swivel nozzle for recoil engines
GB3139965A GB1107635A (en) 1964-07-24 1965-07-23 Deformable jet pipe

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR982999A FR1414824A (en) 1964-07-24 1964-07-24 Deformable connection device and its application to rockets

Publications (1)

Publication Number Publication Date
FR1414824A true FR1414824A (en) 1965-10-22

Family

ID=8835353

Family Applications (1)

Application Number Title Priority Date Filing Date
FR982999A Expired FR1414824A (en) 1964-07-24 1964-07-24 Deformable connection device and its application to rockets

Country Status (3)

Country Link
DE (1) DE1298371B (en)
FR (1) FR1414824A (en)
GB (1) GB1107635A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2199578A1 (en) * 1972-07-26 1974-04-12 Aerojet General Co
FR2316057A1 (en) * 1975-06-09 1977-01-28 Imp Metal Ind Kynoch Ltd Gas pipe for rocket motor - produced from parts and simultaneously given plastic protective lining
FR2523650A1 (en) * 1982-03-17 1983-09-23 Centre Nat Etd Spatiales DEPLOYABLE DEVICE FOR EXTENDING THE NOZZLE OF A ROCKET ENGINE

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5033693A (en) * 1988-12-14 1991-07-23 The Boeing Company Single-piece, flexible inlet ramp

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH248073A (en) * 1944-10-11 1947-04-15 Sulzer Ag Pipeline with a folded tube.
US2578140A (en) * 1946-09-12 1951-12-11 Goodrich Co B F Stretchable diaphragm
DE801603C (en) * 1948-10-02 1951-01-15 Steinmueller Gmbh L & C Lens compensator
CH278361A (en) * 1949-12-13 1951-10-15 Wellig Sebastian Elastic pipe connection.
DE1042971B (en) * 1954-01-02 1958-11-06 Carborundum Co Device for the conduction and directional release of gases, especially for rocket engines
US3049877A (en) * 1956-02-13 1962-08-21 Thiokol Chemical Corp Nozzle for reaction motor
DE1766808U (en) * 1958-03-12 1958-05-14 Hubert Salmen COMPENSATOR.
US3090198A (en) * 1960-11-17 1963-05-21 Gen Motors Corp Swivel nozzle control
DE1150879B (en) * 1961-04-25 1963-06-27 Ernst Heinkel Flugzeugbau G M Device for deflecting a flow center jet

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2199578A1 (en) * 1972-07-26 1974-04-12 Aerojet General Co
FR2316057A1 (en) * 1975-06-09 1977-01-28 Imp Metal Ind Kynoch Ltd Gas pipe for rocket motor - produced from parts and simultaneously given plastic protective lining
FR2523650A1 (en) * 1982-03-17 1983-09-23 Centre Nat Etd Spatiales DEPLOYABLE DEVICE FOR EXTENDING THE NOZZLE OF A ROCKET ENGINE
EP0091841A1 (en) * 1982-03-17 1983-10-19 Centre National D'etudes Spatiales Device to be deployed for the extension of the exhaust nozzle of a rocket engine
US4480437A (en) * 1982-03-17 1984-11-06 Centre National D'etudes Spatiales Unfoldable device for extending the nozzle of a rocket engine

Also Published As

Publication number Publication date
DE1298371B (en) 1969-06-26
GB1107635A (en) 1968-03-27

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