I'm just wondering, is there enough data available to be able to be able to display the Hipparcos mission in Celestia? I'm thinking that since Celestia uses the Hipparcos data, it would be good to have the mission displayed (perhaps even to include in the official distribution).
I must confess however that my modelling skills are at present totally pathetic (though I'm still trying to improve them) and I appreciate that those who have such skills probably have other projects that interest them (this is the reason I do not usually make add-on requests). Just want to know if the idea is feasible (and if anyone's interested in it, so much the better!)
Hipparcos probe?
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There seem to be very few detailed pictures of Hipparcos on the Web. e.g.
http://hipparcos.esa.int/science-e/www/ ... ctid=14060
Even the Hipparcos site has very little engineering information.
http://www.rssd.esa.int/Hipparcos/
Two photographs of it, during a thermal test and during assembly, are in
http://esapub.esrin.esa.it/br/br200/Hipparcos.pdf
Info for for ssc generation:
Apparently its orbit changed through the mission, but on http://www.fas.org/spp/guide/europe/sci ... parcos.htm
it says
http://www.rssd.esa.int/Hipparcos/hipp_payload.html
says
.
http://hipparcos.esa.int/science-e/www/ ... ctid=14060
Even the Hipparcos site has very little engineering information.
http://www.rssd.esa.int/Hipparcos/
Two photographs of it, during a thermal test and during assembly, are in
http://esapub.esrin.esa.it/br/br200/Hipparcos.pdf
Info for for ssc generation:
Apparently its orbit changed through the mission, but on http://www.fas.org/spp/guide/europe/sci ... parcos.htm
it says
and...a launch malfunction left the 1.14 metric ton satellite stranded in GTO instead of the intended GEO....
(note that this is a "secondary reference" and not the original description.)The spacecraft maintained a very slow spin rate (~ one revolution every two hours) to facilitate its all-sky mapping mission. At the end of its mission the orbital parameters of HIPPARCOS were about 490 km by 35,880 km at an inclination of 6.8 degrees.
http://www.rssd.esa.int/Hipparcos/hipp_payload.html
says
Satellite Parameters:
Launch mass 1140 kg
Power requirements 295 W
Uplink data rate 2 kbit/s
Downlink data rate 24 kbit/s
Spin axis inclination to Sun 43 degrees
Spin rate 168.75 arcsec/s
Mission Parameters:
Launch date 8 August 1989
End of operations 15 August 1993
Intended satellite orbit Geostationary
Actual satellite orbit Geostationary transfer
Total scientific data >1000 Gbits
.
Selden
A table of satellite sizes and orbital parameters, including Hipparcos, is in
http://satlist.nl/RAE/RAE1989.doc
http://satlist.nl/RAE/RAE1989.doc
Selden