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AU3635299A - Three axis thruster - Google Patents

Three axis thruster

Info

Publication number
AU3635299A
AU3635299A AU36352/99A AU3635299A AU3635299A AU 3635299 A AU3635299 A AU 3635299A AU 36352/99 A AU36352/99 A AU 36352/99A AU 3635299 A AU3635299 A AU 3635299A AU 3635299 A AU3635299 A AU 3635299A
Authority
AU
Australia
Prior art keywords
axis thruster
thruster
axis
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.)
Abandoned
Application number
AU36352/99A
Inventor
R. Joseph Cassady
Roger M. Myers
Robert D. Osborne
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.)
General Dynamics Ordnance and Tactical Systems Inc
Original Assignee
Primex Technologies Inc
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
Priority claimed from US09/058,314 external-priority patent/US6173565B1/en
Application filed by Primex Technologies Inc filed Critical Primex Technologies Inc
Publication of AU3635299A publication Critical patent/AU3635299A/en
Abandoned legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H1/00—Using plasma to produce a reactive propulsive thrust
    • F03H1/0087—Electro-dynamic thrusters, e.g. pulsed plasma thrusters
    • 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
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
    • 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
    • B64G1/411—Electric propulsion
    • B64G1/413—Ion or plasma engines

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Plasma Technology (AREA)
AU36352/99A 1998-03-02 1999-03-01 Three axis thruster Abandoned AU3635299A (en)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US7643598P 1998-03-02 1998-03-02
US60076435 1998-03-02
US09/058,314 US6173565B1 (en) 1998-04-09 1998-04-09 Three axis pulsed plasma thruster with angled cathode and anode strip lines
US09058314 1998-04-09
PCT/US1999/004602 WO1999045270A1 (en) 1998-03-02 1999-03-01 Three axis thruster

Publications (1)

Publication Number Publication Date
AU3635299A true AU3635299A (en) 1999-09-20

Family

ID=26737488

Family Applications (1)

Application Number Title Priority Date Filing Date
AU36352/99A Abandoned AU3635299A (en) 1998-03-02 1999-03-01 Three axis thruster

Country Status (2)

Country Link
AU (1) AU3635299A (en)
WO (1) WO1999045270A1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007044071A1 (en) * 2007-09-14 2009-04-02 Thales Electron Devices Gmbh Drive arrangement in a spacecraft
CN108518391B (en) * 2018-04-08 2020-01-31 西安交通大学 high-efficiency plasma pneumatic exciter driven by low voltage

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4589398A (en) * 1984-02-27 1986-05-20 Pate Ronald C Combustion initiation system employing hard discharge ignition
US4821509A (en) * 1985-06-10 1989-04-18 Gt-Devices Pulsed electrothermal thruster
US5335179A (en) * 1992-12-24 1994-08-02 General Electric Co. Unified spacecraft attitude control system with pseudo-complementary paired thrusters
US5395076A (en) * 1993-03-19 1995-03-07 Martin Marietta Corporation Spacecraft velocity change maneuvers by variable arcjets

Also Published As

Publication number Publication date
WO1999045270A1 (en) 1999-09-10

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Legal Events

Date Code Title Description
MK6 Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase