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(Q111497132)
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THEMIS-A
satellite in the THEMIS constellation
Explorer 85
THEMIS-P5
MIDEX-5A
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No description defined
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Statements
instance of
geomagnetic satellite
0 references
part of
THEMIS
0 references
image
THEMIS spacecraft model.png
3,000 × 2,879; 2.22 MB
0 references
mass
77
kilogram
criterion used
dry weight
1 reference
reference URL
http://www.swales.com/spacecraft/themis.html
archive URL
https://web.archive.org/web/20070218122341/http://www.swales.com/spacecraft/themis.html
126
kilogram
criterion used
launch weight
1 reference
reference URL
http://www.swales.com/spacecraft/themis.html
archive URL
https://web.archive.org/web/20070218122341/http://www.swales.com/spacecraft/themis.html
country of origin
United States of America
0 references
start point
Cape Canaveral Space Launch Complex 17B
1 reference
stated in
Jonathan's Space Report
space launch vehicle
Delta II
serial number
D-323
1 reference
stated in
Jonathan's Space Report
operator
National Aeronautics and Space Administration
0 references
launch contractor
United Launch Alliance
1 reference
reference URL
https://www.nasaspaceflight.com/2007/02/ulas-delta-ii-launches-with-themis/
UTC date of spacecraft launch
17 February 2007
refine date
23:01:00
1 reference
stated in
Jonathan's Space Report
manufacturer
Swales Aerospace
criterion used
general contractor
2 references
reference URL
http://www.swales.com/spacecraft/themis.html
archive URL
https://web.archive.org/web/20070218122341/http://www.swales.com/spacecraft/themis.html
reference URL
https://www.nasaspaceflight.com/2007/02/ulas-delta-ii-launches-with-themis/
University of California, Berkeley
criterion used
subcontractor
applies to part
space instrument
system integration
1 reference
reference URL
http://www.swales.com/spacecraft/themis.html
archive URL
https://web.archive.org/web/20070218122341/http://www.swales.com/spacecraft/themis.html
powered by
spacecraft solar array
nominal power output
37
watt
1 reference
reference URL
http://www.swales.com/spacecraft/themis.html
archive URL
https://web.archive.org/web/20070218122341/http://www.swales.com/spacecraft/themis.html
reaction control system
source of energy
hydrazine
quantity
4
1 reference
reference URL
http://www.swales.com/spacecraft/themis.html
archive URL
https://web.archive.org/web/20070218122341/http://www.swales.com/spacecraft/themis.html
height
51
centimetre
1 reference
reference URL
https://directory.eoportal.org/web/eoportal/satellite-missions/t/themis#spacecraft
diameter
84
centimetre
1 reference
reference URL
https://directory.eoportal.org/web/eoportal/satellite-missions/t/themis
Identifiers
COSPAR ID
2007-004A
0 references
NSSDCA ID
2007-004A
0 references
SCN
30580
1 reference
stated in
Jonathan's Space Report
Wolfram Language entity code
Entity["Satellite", "30580"]
0 references
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