FR3138169B1 - POWER SUPPLY ASSEMBLY FOR SPACESHIP PLASMA THRUSTER - Google Patents
POWER SUPPLY ASSEMBLY FOR SPACESHIP PLASMA THRUSTER Download PDFInfo
- Publication number
- FR3138169B1 FR3138169B1 FR2207618A FR2207618A FR3138169B1 FR 3138169 B1 FR3138169 B1 FR 3138169B1 FR 2207618 A FR2207618 A FR 2207618A FR 2207618 A FR2207618 A FR 2207618A FR 3138169 B1 FR3138169 B1 FR 3138169B1
- Authority
- FR
- France
- Prior art keywords
- plasma thruster
- power supply
- supply assembly
- spaceship
- thruster
- 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.)
- Active
Links
- 206010063493 Premature ageing Diseases 0.000 abstract 1
- 208000032038 Premature aging Diseases 0.000 abstract 1
- 230000015556 catabolic process Effects 0.000 abstract 1
- 238000006731 degradation reaction Methods 0.000 abstract 1
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
- F03H1/0006—Details applicable to different types of plasma thrusters
- F03H1/0018—Arrangements or adaptations of power supply systems
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Plasma Technology (AREA)
Abstract
Un ensemble d’alimentation électrique (1) pour propulseur à plasma (2) de vaisseau spatial (100) permet de contrôler un courant de maintien (Ikeeper) qui est fourni à une électrode de maintien (22) du propulseur à plasma. L’ensemble d’alimentation électrique prend en compte une contribution à un courant de retour (Ibody) en provenance du propulseur à plasma, qui est constituée par un courant de fuite (Ileak) s’écoulant vers une masse électrique (102) du vaisseau spatial. De cette façon, un vieillissement prématuré ou une dégradation du propulseur à plasma peut être évité.Figure d’abrégé : Figure 1A power supply assembly (1) for a plasma thruster (2) of a spacecraft (100) controls a holding current (Ikeeper) which is supplied to a holding electrode (22) of the plasma thruster. The power supply assembly takes into account a contribution to a return current (Ibody) from the plasma thruster, which is constituted by a leakage current (Ileak) flowing to an electrical ground (102) of the vessel spatial. In this way, premature aging or degradation of the plasma thruster can be avoided. Abstract figure: Figure 1
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2207618A FR3138169B1 (en) | 2022-07-25 | 2022-07-25 | POWER SUPPLY ASSEMBLY FOR SPACESHIP PLASMA THRUSTER |
EP23738832.7A EP4384707A1 (en) | 2022-07-25 | 2023-06-19 | Power supply assembly for a plasma thruster of a spacecraft |
PCT/FR2023/050895 WO2024023409A1 (en) | 2022-07-25 | 2023-06-19 | Power supply assembly for a plasma thruster of a spacecraft |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2207618 | 2022-07-25 | ||
FR2207618A FR3138169B1 (en) | 2022-07-25 | 2022-07-25 | POWER SUPPLY ASSEMBLY FOR SPACESHIP PLASMA THRUSTER |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3138169A1 FR3138169A1 (en) | 2024-01-26 |
FR3138169B1 true FR3138169B1 (en) | 2024-07-12 |
Family
ID=84569345
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR2207618A Active FR3138169B1 (en) | 2022-07-25 | 2022-07-25 | POWER SUPPLY ASSEMBLY FOR SPACESHIP PLASMA THRUSTER |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP4384707A1 (en) |
FR (1) | FR3138169B1 (en) |
WO (1) | WO2024023409A1 (en) |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6518693B1 (en) * | 1998-11-13 | 2003-02-11 | Aerojet-General Corporation | Method and apparatus for magnetic voltage isolation |
FR2788084B1 (en) * | 1998-12-30 | 2001-04-06 | Snecma | PLASMA PROPELLER WITH CLOSED ELECTRON DRIFT WITH ORIENTABLE PUSH VECTOR |
FR3094046B1 (en) * | 2019-03-18 | 2021-04-23 | Centre Nat Rech Scient | Ion thruster control method, and ion propulsion system |
-
2022
- 2022-07-25 FR FR2207618A patent/FR3138169B1/en active Active
-
2023
- 2023-06-19 EP EP23738832.7A patent/EP4384707A1/en active Pending
- 2023-06-19 WO PCT/FR2023/050895 patent/WO2024023409A1/en unknown
Also Published As
Publication number | Publication date |
---|---|
EP4384707A1 (en) | 2024-06-19 |
FR3138169A1 (en) | 2024-01-26 |
WO2024023409A1 (en) | 2024-02-01 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
RU2684968C2 (en) | Spacecraft propulsion system and method | |
FR3138169B1 (en) | POWER SUPPLY ASSEMBLY FOR SPACESHIP PLASMA THRUSTER | |
US20140326703A1 (en) | Extended cascade plasma gun | |
FR2640387A1 (en) | METHOD FOR SELECTING THE OPTIMAL SERIAL PROTECTION RESISTANCE IN A COCKCROFT-WALTON HIGH VOLTAGE CIRCUIT | |
FR2767356A1 (en) | Mixing head for combustion chamber of rocket motor | |
US9410539B2 (en) | Micro-nozzle thruster | |
RU2738136C1 (en) | Ionic rocket engine and method of operation thereof | |
US3414702A (en) | Nonthermionic electron beam apparatus | |
RU2672054C1 (en) | Electric arc plasma torch for coatings from refractory dispersed materials application | |
CN115681058B (en) | Multi-working-mode Hall propulsion system and spacecraft with same | |
Potrivitu et al. | Systematic testing of improved designs of miniaturized LaB6 hollow cathodes for electric propulsion systems for cubesats and small satellites | |
Myers | Geometric scaling of applied-field magnetoplasmadynamic thrusters | |
Zhuang et al. | Micro-vacuum arc thruster with extended lifetime | |
JPH0771361A (en) | Production device for space navigation craft | |
Rudolph et al. | Onset phenomena in self-field MPD arcjets | |
GB582731A (en) | Improvements in or relating to electric arc cutting devices | |
RU2771562C2 (en) | Device for regulating flow of working medium for electric rocket engine | |
US20170305579A1 (en) | Power architecture for solar electric propulsion applications | |
US12025110B2 (en) | Charging mitigation device and electric discharge avoidance method | |
RU2762684C1 (en) | Current supply output design and electromagnetic device | |
RU2823975C1 (en) | Coaxial ablation pulse plasma engine with thrust vectoring | |
RU2738522C1 (en) | Ionic rocket engine and method of operation thereof | |
RU2702773C1 (en) | Pinch erosion-bearing rocket engine | |
RU2745180C1 (en) | Combined ion rocket engine and coroning electrode | |
RU2735043C1 (en) | Plasma-ion rocket engine |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 2 |
|
PLSC | Publication of the preliminary search report |
Effective date: 20240126 |
|
PLFP | Fee payment |
Year of fee payment: 3 |