[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Riedler et al., 1997 - Google Patents

Active spacecraft potential control

Riedler et al., 1997

Document ID
10515369211142273603
Author
Riedler W
Torkar K
Rüdenauer F
Fehringer M
Pedersen A
Schmidt R
Grard R
Arends H
Narheim B
Troim J
Torbert R
Olsen R
Whipple E
Goldstein R
Valavanoglou N
Zhao H
Publication year
Publication venue
Space Science Reviews

External Links

Snippet

Charging of the outer surface or of the entire structure of a spacecraft in orbit can have a severe impact on the scientific output of the instruments. Typical floating potentials for magnetospheric satellites (from+ 1 to several tens of volts in sunlight) make it practically …
Continue reading at link.springer.com (other versions)

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/42Arrangements or adaptations of power supply systems
    • B64G1/44Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
    • B64G1/443Photovoltaic cell arrays
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40Arrangements or adaptations of propulsion systems
    • B64G1/402Propellant tanks; Feeding propellants
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/52Protection, safety or emergency devices; Survival aids
    • B64G1/54Protection against radiation
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control

Similar Documents

Publication Publication Date Title
Riedler et al. Active spacecraft potential control
Torkar et al. Active spacecraft potential control for Cluster–implementation and first results
Torkar et al. Active spacecraft potential control investigation
Brophy et al. Ion propulsion system (NSTAR) DS1 technology validation report
Bekkeng et al. Multi-needle Langmuir probe system for electron density measurements and active spacecraft potential control on CubeSats
Lai An overview of electron and ion beam effects in charging and discharging to spacecraft
Olsen Experiments in charge control at geosynchronous orbit-ATS-5 and ATS-6
Torkar et al. Spacecraft potential control aboard Equator-S as a test for Cluster-II
Myers et al. Vehicle charging effects during electron beam emission from the CHARGE-2 experiment
Torkar et al. An experiment to study and control the Langmuir sheath around INTERBALL-2
Banks et al. Results from the vehicle charging and potential experiment on STS-3
Mullen et al. An autonomous charge control system at geosynchronous altitude: Flight results for spacecraft design consideration
Riedler et al. Active Spacecraft Potential Control: an ion emitter experiment for Cluster
Jones et al. Preliminary results of SERT II spacecraft potential measurements using hot wire emissive probes
Torkar et al. Spacecraft potential control for Double Star
Genovese et al. 2000-hour endurance test of indium field emission electric propulsion microthruster cluster
Torkar implementation and first results
Philip et al. Recent hollow cathode investigations at the Royal Aircraft Establishment
Schmidt et al. Novel methods for active spacecraft potential control
Deininger et al. Hollow cathode plasma source for active spacecraft charge control
Fehringer et al. Space-proven indium liquid metal field ion emitters for ion microthruster applications
Lai et al. The effect of photoelectrons on boom‐satellite potential differences during electron beam ejection
Riedler et al. Active spacecraft potential control: An ion emitter experiment.[Cluster mission]
Riedler et al. Active spacecraft potential control: An ion emitter experiment
Banks et al. Charge-2 rocket observations of vehicle charging and charge neutralization