Manzella et al., 2001 - Google Patents
High voltage SPT performanceManzella et al., 2001
View PDF- Document ID
- 7934584745833549827
- Author
- Manzella D
- Jacobson D
- Jankovsky R
- Publication year
- Publication venue
- 37th Joint Propulsion Conference and Exhibit
External Links
Snippet
A 2.3 kilowatt stationary plasma thruster designed to operate at high voltage was tested at discharge voltages between 300 and 1250 Volts. Discharge specific impulses between 1600 and 3700 seconds were demonstrated with thrust between 40 and 145 mN. Test data …
- 230000000694 effects 0 abstract description 11
Classifications
-
- 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
- B64G1/402—Propellant tanks; Feeding propellants
-
- 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
- B64G1/42—Arrangements or adaptations of power supply systems
- B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
- B64G1/443—Photovoltaic cell arrays
-
- 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
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/002—Launch systems
- B64G1/007—Orbit transfer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
- B64G1/1014—Navigation satellites
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Manzella et al. | High voltage SPT performance | |
Dannenmayer et al. | Elementary scaling relations for Hall effect thrusters | |
Liang | The Combination of Two Concentric Discharge Channels into a Nested Hall-Effect Thruster. | |
Wollenhaupt et al. | Overview of thermal arcjet thruster development | |
Conversano et al. | Performance enhancement of a long-life, low-power hall thruster for deep-space smallsats | |
Brown et al. | Air Force Research Laboratory high power electric propulsion technology development | |
Kim | Stationary plasma thrusters in Russia: problems and perspectives | |
Gilland et al. | Multimegawatt electric propulsion system design considerations | |
Welander et al. | Life and operating range extension of the BPT-4000 qualification model hall thruster | |
Manzella et al. | Hall thruster technology for NASA science missions | |
Semenkin et al. | Feasibility of high power multi-mode EPS development based on the thruster with anode layer | |
Cadiou et al. | An overview of the CNES electric propulsion program | |
Xu | Ion collimation and in-channel potential shaping using in-channel electrodes for Hall effect thrusters | |
Pigeon et al. | A Low Power Cylindrical Hall Thruster for Next Generation Microsatellites | |
Leiter et al. | Evaluation of the performance of the advanced 200mn radio-frequency ion thruster rit-xt | |
FRISBEE et al. | SP-100 nuclear electric propulsion for Mars cargo missions | |
Kaminska et al. | Performances of an argon arc-jet thruster for satellites | |
Butler et al. | Multimode, high specific impulse Hall thruster technology | |
Dudeck et al. | Plasma propulsion for geostationary satellites and interplanetary spacecraft | |
Lyons et al. | Electric propulsion concepts enabled by high power systems for space exploration | |
Ferreira et al. | Hall plasma thruster development for micro and nano satellites | |
Racca | Capability of solar electric propulsion for planetary missions | |
Killinger et al. | Development of a high performance RF-ion thruster | |
STONE et al. | The NASA low thrust propulsion program | |
Wallace et al. | The design and performance of the T6 ion thruster |