GB2335711B - Process for generating lateral thrust - Google Patents

Process for generating lateral thrust

Info

Publication number
GB2335711B
GB2335711B GB9906729A GB9906729A GB2335711B GB 2335711 B GB2335711 B GB 2335711B GB 9906729 A GB9906729 A GB 9906729A GB 9906729 A GB9906729 A GB 9906729A GB 2335711 B GB2335711 B GB 2335711B
Authority
GB
United Kingdom
Prior art keywords
lateral thrust
generating lateral
generating
thrust
lateral
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 - Fee Related
Application number
GB9906729A
Other versions
GB2335711A (en
GB9906729D0 (en
Inventor
German Mundig
Wolfgang Muller
Joachim Reinecke
Peter Gleich
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.)
Daimler AG
Original Assignee
DaimlerChrysler AG
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 DaimlerChrysler AG filed Critical DaimlerChrysler AG
Publication of GB9906729D0 publication Critical patent/GB9906729D0/en
Publication of GB2335711A publication Critical patent/GB2335711A/en
Application granted granted Critical
Publication of GB2335711B publication Critical patent/GB2335711B/en
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • 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
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F02K9/56—Control
    • 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
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • 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
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/68—Decomposition chambers
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Air Bags (AREA)
  • Testing Of Engines (AREA)
  • Plasma Technology (AREA)
GB9906729A 1998-03-26 1999-03-23 Process for generating lateral thrust Expired - Fee Related GB2335711B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19813330A DE19813330C2 (en) 1998-03-26 1998-03-26 Process for generating a transverse thrust

Publications (3)

Publication Number Publication Date
GB9906729D0 GB9906729D0 (en) 1999-05-19
GB2335711A GB2335711A (en) 1999-09-29
GB2335711B true GB2335711B (en) 2000-05-17

Family

ID=7862402

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9906729A Expired - Fee Related GB2335711B (en) 1998-03-26 1999-03-23 Process for generating lateral thrust

Country Status (3)

Country Link
DE (1) DE19813330C2 (en)
FR (1) FR2776716B1 (en)
GB (1) GB2335711B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112901374B (en) * 2020-12-21 2022-02-22 中国人民解放军国防科技大学 Manual flow regulating device

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4203775A1 (en) * 1992-02-10 1993-08-12 Erno Raumfahrttechnik Gmbh Hydrazine fuelled propulsion unit with decomposition chamber - has injection bores inclined to lines perpendicular to one or more injector head outer surfaces

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3142541A (en) * 1961-08-18 1964-07-28 Chandler Evans Corp Gas generator for rocket propellants
DE1776010A1 (en) * 1968-09-03 1971-09-16 Messerschmitt Boelkow Blohm Process for conveying liquid fuels for gas generators or rocket combustion chambers, and conveying system for carrying out the process
FR2283390A1 (en) * 1974-08-26 1976-03-26 Centre Nat Etd Spatiales DEVICE FOR PRESSURIZING A LIQUID MONERGOL IN A TANK FOR THIS PURPOSE
US3956885A (en) * 1974-09-03 1976-05-18 Avco Corporation Electrothermal reactor
GB1534601A (en) * 1976-07-23 1978-12-06 Secr Defence Electrothermal gas thrusters
DE3616184A1 (en) * 1985-08-21 1987-02-26 Rheinmetall Gmbh PRESSURE VALVE FOR A PYROTECHNICAL GAS GENERATOR
GB2190729A (en) * 1986-05-21 1987-11-25 Plessey Co Plc Solid propellant burn rate control device
DE4122756A1 (en) * 1991-07-10 1993-02-11 Erno Raumfahrttechnik Gmbh ENGINE FOR SPACING BODIES

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4203775A1 (en) * 1992-02-10 1993-08-12 Erno Raumfahrttechnik Gmbh Hydrazine fuelled propulsion unit with decomposition chamber - has injection bores inclined to lines perpendicular to one or more injector head outer surfaces

Also Published As

Publication number Publication date
FR2776716A1 (en) 1999-10-01
GB2335711A (en) 1999-09-29
DE19813330C2 (en) 2000-04-13
FR2776716B1 (en) 2002-01-04
GB9906729D0 (en) 1999-05-19
DE19813330A1 (en) 1999-09-30

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20070323