[go: up one dir, main page]

Wong et al., 1987 - Google Patents

The UoSAT-2 spacecraft power system

Wong et al., 1987

Document ID
6215447438646887697
Author
Wong H
Blewett M
Publication year
Publication venue
Journal of the Institution of Electronic and Radio Engineers

External Links

Snippet

Four panels of Si solar cells provide power to charge packs of NiCd battery cells via a battery charge regulator. Regulated+ 10 V,− 10 V and+ 5 V supplies from a centralized power regulating system, as well as+ 14 V unregulated battery voltage, are supplied to a …
Continue reading at digital-library.theiet.org (other versions)

Classifications

    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/34Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
    • H02J7/35Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J9/00Circuit arrangement for emergency or standby power supply, e.g. for emergency lighting
    • H02J9/04Circuit arrangement for emergency or standby power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source
    • H02J9/06Circuit arrangement for emergency or standby power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source with automatic change-over
    • H02J9/061Circuit arrangement for emergency or standby power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source with automatic change-over characterised by the use of electronic means
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J1/00Circuit arrangements for dc mains or dc distribution networks
    • H02J1/10Parallel operation of dc sources
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/0013Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries for charging several batteries simultaneously or sequentially
    • 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
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control

Similar Documents

Publication Publication Date Title
EP1389582B1 (en) Battery cell balancing system
Lashab et al. Space microgrids: New concepts on electric power systems for satellites
Wong et al. The UoSAT-2 spacecraft power system
US6157161A (en) Low cost battery charging systems
Edpuganti et al. Comparison study of electric power system architectures for CubeSat
Bekhti et al. Effect of the bus voltage level on the power system design for microsatellites
Bekhti et al. Design and implementation of a power distribution system adopting overcurrent protection
Van der Zel et al. Three generations of DC power systems for experimental small satellites
Vobornik et al. Experimental electric power system for small satellites with independent supply channels
Castiaux et al. Power conditioning units for high power geostationary satellites
Karahan et al. Electrical Power Subsystem of IMECE Satellite
US11799420B1 (en) Solar array reverse current protection
Cunningham et al. MSFC electrical power systems for cubesats
Cheremetiev Design of reliable electrical power system for foresail-1 small satellite
Bonin Power system design, analysis, and power electronics implementation on generic nanosatellite bus (GNB) spacecraft
Barrera Spacecraft Electrical Power Systems
Sullivan HETE Satellite Power Subsystem
Krummann The power subsystem for the next generation GOES satellite
Cherdak et al. Nimbus power systems/1960-1969
Özkaya et al. Power Subsystem of rasat flight model
Denney Keys et al. Design and Development of the Solar Dynamics Observatory (SDO) Electrical Power System
MacKenzie et al. Nimbus Power Systems (1960-1969)
Croci et al. The RADARSAT-2 power control unit
Denney et al. Design and Development of the Solar Dynamics Observatory (SDO) Electrical Power System
Cussen Solar cells in satellite power supplies