In-Orbit Performance of the MWRI Scanning Mechanisms

Scanning Equipment supporting the Millimeter Wave Radiometer Instrument (MWRI) are flying in a sunsynchronized orbit of 850-km altitude with an inclination of 98.8 deg on the FY-3 meteorological satellite (FY = Feng Yun, Wind and Cloud). MWRI is a linearly polarized, ten-channel passive Radiometer;...

Full description

Bibliographic Details
Main Authors: Schmid, Manfred, Shuang, Yu, Jun, Miao
Format: Other/Unknown Material
Language:unknown
Published: 2014
Subjects:
Online Access:http://hdl.handle.net/2060/20150004048
id ftnasantrs:oai:casi.ntrs.nasa.gov:20150004048
record_format openpolar
spelling ftnasantrs:oai:casi.ntrs.nasa.gov:20150004048 2023-05-15T18:18:28+02:00 In-Orbit Performance of the MWRI Scanning Mechanisms Schmid, Manfred Shuang, Yu Jun, Miao Unclassified, Unlimited, Publicly available May 2014 application/pdf http://hdl.handle.net/2060/20150004048 unknown Document ID: 20150004048 http://hdl.handle.net/2060/20150004048 Copyright, Distribution as joint owner in the copyright CASI Spacecraft Instrumentation and Astrionics The 42nd Aerospace Mechanism Symposium; 59-72; NASA/CP-2014-217519 2014 ftnasantrs 2018-06-09T22:52:04Z Scanning Equipment supporting the Millimeter Wave Radiometer Instrument (MWRI) are flying in a sunsynchronized orbit of 850-km altitude with an inclination of 98.8 deg on the FY-3 meteorological satellite (FY = Feng Yun, Wind and Cloud). MWRI is a linearly polarized, ten-channel passive Radiometer; it measures precipitation and water clouds, sea ice, snow/water equivalent, drought and flood index, land temperature and soil moisture. Following the FY3-A, the FY3-B Satellite was launched in autumn 2010. Since that time, the Scanning Equipment was continuously operated. During the last three and a half years in orbit, the Scanning Mechanism has executed about 65 million revolutions, while the Scan Compensation Mechanism (SCM) - used for momentum compensation - has already successfully executed more than one billion revolutions. During the commissioning phase of the instrument and during the first operation phase, random torque spikes, which manifested themselves as a motor current increase, were observed in the Scan Drive Mechanism, whereas the Scan Compensation drive operated nominally from the beginning. The result of the root cause investigations performed in order to isolate the issue, and the consequences for the follow-on MWRI equipment which was successfully launched by end of September 2013 (now flying on the FY 3-C Spacecraft), are discussed. Other/Unknown Material Sea ice NASA Technical Reports Server (NTRS)
institution Open Polar
collection NASA Technical Reports Server (NTRS)
op_collection_id ftnasantrs
language unknown
topic Spacecraft Instrumentation and Astrionics
spellingShingle Spacecraft Instrumentation and Astrionics
Schmid, Manfred
Shuang, Yu
Jun, Miao
In-Orbit Performance of the MWRI Scanning Mechanisms
topic_facet Spacecraft Instrumentation and Astrionics
description Scanning Equipment supporting the Millimeter Wave Radiometer Instrument (MWRI) are flying in a sunsynchronized orbit of 850-km altitude with an inclination of 98.8 deg on the FY-3 meteorological satellite (FY = Feng Yun, Wind and Cloud). MWRI is a linearly polarized, ten-channel passive Radiometer; it measures precipitation and water clouds, sea ice, snow/water equivalent, drought and flood index, land temperature and soil moisture. Following the FY3-A, the FY3-B Satellite was launched in autumn 2010. Since that time, the Scanning Equipment was continuously operated. During the last three and a half years in orbit, the Scanning Mechanism has executed about 65 million revolutions, while the Scan Compensation Mechanism (SCM) - used for momentum compensation - has already successfully executed more than one billion revolutions. During the commissioning phase of the instrument and during the first operation phase, random torque spikes, which manifested themselves as a motor current increase, were observed in the Scan Drive Mechanism, whereas the Scan Compensation drive operated nominally from the beginning. The result of the root cause investigations performed in order to isolate the issue, and the consequences for the follow-on MWRI equipment which was successfully launched by end of September 2013 (now flying on the FY 3-C Spacecraft), are discussed.
format Other/Unknown Material
author Schmid, Manfred
Shuang, Yu
Jun, Miao
author_facet Schmid, Manfred
Shuang, Yu
Jun, Miao
author_sort Schmid, Manfred
title In-Orbit Performance of the MWRI Scanning Mechanisms
title_short In-Orbit Performance of the MWRI Scanning Mechanisms
title_full In-Orbit Performance of the MWRI Scanning Mechanisms
title_fullStr In-Orbit Performance of the MWRI Scanning Mechanisms
title_full_unstemmed In-Orbit Performance of the MWRI Scanning Mechanisms
title_sort in-orbit performance of the mwri scanning mechanisms
publishDate 2014
url http://hdl.handle.net/2060/20150004048
op_coverage Unclassified, Unlimited, Publicly available
genre Sea ice
genre_facet Sea ice
op_source CASI
op_relation Document ID: 20150004048
http://hdl.handle.net/2060/20150004048
op_rights Copyright, Distribution as joint owner in the copyright
_version_ 1766195060683046912