IT1016432B - THRUST VECTOR CONTROL SYSTEM FOR A ROCKET ENGINE - Google Patents

THRUST VECTOR CONTROL SYSTEM FOR A ROCKET ENGINE

Info

Publication number
IT1016432B
IT1016432B IT52123/74A IT5212374A IT1016432B IT 1016432 B IT1016432 B IT 1016432B IT 52123/74 A IT52123/74 A IT 52123/74A IT 5212374 A IT5212374 A IT 5212374A IT 1016432 B IT1016432 B IT 1016432B
Authority
IT
Italy
Prior art keywords
control system
vector control
rocket engine
thrust vector
thrust
Prior art date
Application number
IT52123/74A
Other languages
Italian (it)
Original Assignee
Aerojet General Co
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 Aerojet General Co filed Critical Aerojet General Co
Application granted granted Critical
Publication of IT1016432B publication Critical patent/IT1016432B/en

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
    • F02K9/84Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using movable nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Transmission Devices (AREA)
  • Joints Allowing Movement (AREA)
IT52123/74A 1973-07-19 1974-07-15 THRUST VECTOR CONTROL SYSTEM FOR A ROCKET ENGINE IT1016432B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US38062273A 1973-07-19 1973-07-19

Publications (1)

Publication Number Publication Date
IT1016432B true IT1016432B (en) 1977-05-30

Family

ID=23501874

Family Applications (1)

Application Number Title Priority Date Filing Date
IT52123/74A IT1016432B (en) 1973-07-19 1974-07-15 THRUST VECTOR CONTROL SYSTEM FOR A ROCKET ENGINE

Country Status (8)

Country Link
JP (1) JPS5038300A (en)
BE (1) BE817601A (en)
DE (1) DE2434425A1 (en)
FR (1) FR2238053A1 (en)
IL (1) IL45180A0 (en)
IT (1) IT1016432B (en)
NO (1) NO742436L (en)
SE (1) SE7409412L (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS51150237A (en) * 1975-06-19 1976-12-23 Oki Electric Ind Co Ltd Pachage
JPS58114215A (en) * 1981-12-28 1983-07-07 Fujitsu Ltd Cooling method of electronic apparatus
FR3072732B1 (en) * 2017-10-24 2020-10-09 Centre Nat Etd Spatiales ROTARY NOZZLE, PROPULSION SYSTEM INCLUDING SUCH A NOZZLE AND SPACE LAUNCHER INCLUDING SUCH A PROPULSION SYSTEM

Also Published As

Publication number Publication date
JPS5038300A (en) 1975-04-09
SE7409412L (en) 1975-01-20
DE2434425A1 (en) 1975-05-28
FR2238053A1 (en) 1975-02-14
NO742436L (en) 1975-02-17
IL45180A0 (en) 1975-04-25
BE817601A (en) 1974-11-04

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