NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Vehicle Charging And Potential (VCAP)The vehicle charging and potential (VCAP) payload includes a small electron accelerator capable of operating in a pulsed mode with firing pulses ranging from 600 nanoseconds to 107 seconds (100 milliamps at 1000 volts), a spherical retarding potential analyzer - Langmuir probe, and charge current probes. This instrumentation will support studies of beam plasma interactions and the electrical charging of the spacecraft. Active experiments may also be performed to investigate the fundamental processes of artificial aurora and ionospheric perturbations. In addition, by firing the beam up the geomagnetic field lines of force (away from the Earth) investigations of parallel electric field may be performed.
Document ID
19860009893
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Roberts, B.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1986
Publication Information
Publication: Solar Terrestrial Observatory Space Station Workshop Report
Subject Category
Spacecraft Instrumentation
Accession Number
86N19364
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available