IT7828403A0 - Aeromobile guidabile. - Google Patents

Aeromobile guidabile.

Info

Publication number
IT7828403A0
IT7828403A0 IT7828403A IT2840378A IT7828403A0 IT 7828403 A0 IT7828403 A0 IT 7828403A0 IT 7828403 A IT7828403 A IT 7828403A IT 2840378 A IT2840378 A IT 2840378A IT 7828403 A0 IT7828403 A0 IT 7828403A0
Authority
IT
Italy
Prior art keywords
drivable
aircraft
drivable aircraft
Prior art date
Application number
IT7828403A
Other languages
English (en)
Other versions
IT1099232B (it
Original Assignee
Bayern Chemie Gmbh Flugchemie
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 Bayern Chemie Gmbh Flugchemie filed Critical Bayern Chemie Gmbh Flugchemie
Publication of IT7828403A0 publication Critical patent/IT7828403A0/it
Application granted granted Critical
Publication of IT1099232B publication Critical patent/IT1099232B/it

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
    • F02K9/82—Rocket-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
    • 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

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)
  • Nozzles (AREA)
  • Storing, Repeated Paying-Out, And Re-Storing Of Elongated Articles (AREA)
IT28403/78A 1977-10-06 1978-10-04 Aeromobile guidabile IT1099232B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19772744897 DE2744897A1 (de) 1977-10-06 1977-10-06 Lenkflugkoerper

Publications (2)

Publication Number Publication Date
IT7828403A0 true IT7828403A0 (it) 1978-10-04
IT1099232B IT1099232B (it) 1985-09-18

Family

ID=6020761

Family Applications (1)

Application Number Title Priority Date Filing Date
IT28403/78A IT1099232B (it) 1977-10-06 1978-10-04 Aeromobile guidabile

Country Status (4)

Country Link
DE (1) DE2744897A1 (it)
FR (1) FR2405456A1 (it)
GB (1) GB2005606B (it)
IT (1) IT1099232B (it)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3042301B2 (ja) 1994-04-28 2000-05-15 日産自動車株式会社 サイドスラスタ
DE112010005752B4 (de) * 2010-07-22 2014-11-13 Saab Ab Kühlvorrichtung zum Kühlen von Verbrennungsgasen aus rückstoßfreien Antipanzerwaffen
CN112572840A (zh) * 2020-12-14 2021-03-30 兰州空间技术物理研究所 一种电推进系统贮供单元及其制造方法
CN116696607A (zh) * 2023-05-17 2023-09-05 西北工业大学 基于多孔射流矢量合成技术的流体喉部喷管推力调节装置及调节方法

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3147590A (en) * 1961-03-16 1964-09-08 Thompson Ramo Wooldridge Inc Reaction motor with nozzle vector control having ablative port means and cooled valve means
FR1316191A (fr) * 1962-02-26 1963-01-25 United Aircraft Corp Dispositif de commande pour appareil propulseur
US3266732A (en) * 1963-09-03 1966-08-16 United Aircraft Corp Roll control system
US3270505A (en) * 1964-10-21 1966-09-06 Norman L Crabill Control system for rocket vehicles
GB1134835A (en) * 1965-12-06 1968-11-27 Us Navy Liquid injection thrust vectoring
US4063685A (en) * 1976-07-30 1977-12-20 The United States Of America As Represented By The Secretary Of The Army Thrust vector control by circulation control over aerodynamic surfaces in a supersonic nozzle

Also Published As

Publication number Publication date
GB2005606A (en) 1979-04-25
FR2405456A1 (fr) 1979-05-04
IT1099232B (it) 1985-09-18
DE2744897A1 (de) 1979-04-19
GB2005606B (en) 1982-06-30

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