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Interpretation of STS-3/plasma diagnostics package results in terms of large space structure plasma interactionsThe Plasma Diagnostics Package, which was flown aboard STS-3 recorded various chemical releases from the Orbiter. Changes in the plasma environment were observed to occur during Flash Evaporator System (FES) releases, water dumps and maneuvering thruster operations. During flash evaporator operations, broadband Orbiter-generated electro-static noise is enhanced and plasma density irregularity (delta n/N) is observed to increase by as much as 4 times and is strongly peaked below 6 Hz. In the case of water dumps, background electrostatic noise is enhanced or suppressed depending on frequency and Delta N/N is also seen to increase by as much as 4 times. Various changes in the plasma environment are effected by primary and vernier thruster operations. In addition, thruster activity stimulates electrostatic noise with a spectrum which is most intense at frequencies below 10 kHz.
Document ID
19840008923
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kurth, W. S.
(Iowa Univ. Iowa City, IA, United States)
Date Acquired
September 4, 2013
Publication Date
January 27, 1984
Subject Category
Plasma Physics
Report/Patent Number
NAS 1.26:173266
NASA-CR-173266
Report Number: NAS 1.26:173266
Report Number: NASA-CR-173266
Accession Number
84N16991
Funding Number(s)
CONTRACT_GRANT: NAG3-449
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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