FR2795135B1 - Systeme de micropropulsion a poudre et procede de realisation d'un tel systeme de micropropulsion - Google Patents

Systeme de micropropulsion a poudre et procede de realisation d'un tel systeme de micropropulsion

Info

Publication number
FR2795135B1
FR2795135B1 FR9907626A FR9907626A FR2795135B1 FR 2795135 B1 FR2795135 B1 FR 2795135B1 FR 9907626 A FR9907626 A FR 9907626A FR 9907626 A FR9907626 A FR 9907626A FR 2795135 B1 FR2795135 B1 FR 2795135B1
Authority
FR
France
Prior art keywords
micropropulsion
powder
producing
micropropulsion system
powder micropropulsion
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 - Lifetime
Application number
FR9907626A
Other languages
English (en)
Other versions
FR2795135A1 (fr
Inventor
Denis Dilhan
Daniel Esteve
Carole Rossi
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.)
Centre National dEtudes Spatiales CNES
Original Assignee
Centre National dEtudes Spatiales CNES
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 Centre National dEtudes Spatiales CNES filed Critical Centre National dEtudes Spatiales CNES
Priority to FR9907626A priority Critical patent/FR2795135B1/fr
Publication of FR2795135A1 publication Critical patent/FR2795135A1/fr
Application granted granted Critical
Publication of FR2795135B1 publication Critical patent/FR2795135B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15C—FLUID-CIRCUIT ELEMENTS PREDOMINANTLY USED FOR COMPUTING OR CONTROL PURPOSES
    • F15C1/00—Circuit elements having no moving parts
    • F15C1/02—Details, e.g. special constructional devices for circuits with fluid elements, such as resistances, capacitive circuit elements; devices preventing reaction coupling in composite elements ; Switch boards; Programme devices
    • F15C1/06—Constructional details; Selection of specified materials ; Constructional realisation of one single element; Canal shapes; Jet nozzles; Assembling an element with other devices, only if the element forms the main part
    • 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
    • F02K9/94—Re-ignitable or restartable rocket- engine plants; Intermittently operated rocket-engine plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15C—FLUID-CIRCUIT ELEMENTS PREDOMINANTLY USED FOR COMPUTING OR CONTROL PURPOSES
    • F15C1/00—Circuit elements having no moving parts
    • F15C1/006—Circuit elements having no moving parts for aeronautics; for rockets (drives, controls); for satellites; for air cushion vehicles; for controlling vessels or torpedoes
    • 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
    • F42B10/661—Steering by varying intensity or direction of thrust using several transversally acting rocket motors, each motor containing an individual propellant charge, e.g. solid charge

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • Theoretical Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Micromachines (AREA)
FR9907626A 1999-06-16 1999-06-16 Systeme de micropropulsion a poudre et procede de realisation d'un tel systeme de micropropulsion Expired - Lifetime FR2795135B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR9907626A FR2795135B1 (fr) 1999-06-16 1999-06-16 Systeme de micropropulsion a poudre et procede de realisation d'un tel systeme de micropropulsion

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9907626A FR2795135B1 (fr) 1999-06-16 1999-06-16 Systeme de micropropulsion a poudre et procede de realisation d'un tel systeme de micropropulsion

Publications (2)

Publication Number Publication Date
FR2795135A1 FR2795135A1 (fr) 2000-12-22
FR2795135B1 true FR2795135B1 (fr) 2001-08-31

Family

ID=9546875

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9907626A Expired - Lifetime FR2795135B1 (fr) 1999-06-16 1999-06-16 Systeme de micropropulsion a poudre et procede de realisation d'un tel systeme de micropropulsion

Country Status (1)

Country Link
FR (1) FR2795135B1 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2842899B1 (fr) * 2002-07-25 2005-05-06 Lacroix Soc E Projectile a mise en oeuvre perfectionnee
FR2899678B1 (fr) * 2006-04-05 2010-09-10 Protac Structure generique d'initiation et de commande pour systemes de controle de trajectoire comportant une couronne de generateurs de gaz.
CN101907040B (zh) * 2010-07-23 2013-04-24 北京航空航天大学 一种采用圆环贮箱的氮气冷气微推进装置
CN114537713B (zh) * 2022-02-24 2024-06-11 中国人民解放军军事科学院国防科技创新研究院 燃气微推进系统

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3328963A (en) * 1962-12-27 1967-07-04 Curtiss Wright Corp Attitude control device for space vehicles
US3263419A (en) * 1963-05-23 1966-08-02 Thiokol Chemical Corp Attitude control system for space vehicles
US3316719A (en) * 1965-03-11 1967-05-02 Curtiss Wright Corp Expansible rocket engines
EP0418636B1 (fr) * 1989-09-19 1993-12-29 DIEHL GMBH & CO. Projectile à trajectoire corrigé
US5836150A (en) * 1995-05-31 1998-11-17 The United States Of America As Represented By The United States Department Of Energy Micro thrust and heat generator
US6068010A (en) * 1995-06-09 2000-05-30 Marotta Scientific Controls, Inc. Microvalve and microthruster for satellites and methods of making and using the same

Also Published As

Publication number Publication date
FR2795135A1 (fr) 2000-12-22

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