Uosat 12
Also called UO-36 and UoSAT-OSCAR-36
Note: there is a confusion about the object number. At launch 25694 reflected
the actual satellite.
Estimate cost: $9 million ?
http://www.ee.surrey.ac.uk/EE/CSER/UOSAT/missions/uo12/
sat-index articles
Prime
contractor
|
SSTL
|
Platform
|
new
SSTL platform
|
Mass
at launch
|
300-350
kg
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Mass
in orbit
|
|
Dimension
|
|
Solar
array
|
|
Stabilization
|
|
DC
power
|
|
Design
lifetime
|
|
UoSAT-12 carries a number of imaging payloads (Earth Imaging System;up to 10
meter resolution). It carries a propulsion system for orbital housekeeping
experiments. The S-band downlink can run at speeds up to 1Mb/s for downloading
imaging data.
Equipped with 2 cameras (10 m resolution panchromatic, 40 m multispectral).
CCDs are from Eastman Kodak. Also has a colour wide angle camera.
telemetry: 437.400 MHz
UoSAT-12 carries a newly developed Space GPS receiver, the SGR, that is
designed to provide an experimental testbed for orbit and attitude
determination. It has 5 antennas to accurately calculate the spacecraft
attitude through applying interferometry techniques to the phase difference
measurements.
Resistojet is a new propulsion technology on-board. Nitrous oxide is heated by
an electrical element powered by the spacecraft's batteries. The thrust from
the Resistojet can be used to adjust the spacecraft's orbit. A 60-minute
Resistojet firing period will raise the 650km orbit of the spacecraft by 3km.
UoSAT-12 carries 2.5kg of nitrous oxide, sufficient for 14 hours running, in an
expulsion system developed for Surrey in collaboration with Polyflex Aerospace
of Cheltenham, UK.
For use of the Nanyang Technological University (NTU), Singapore. Aim is
to help develop a future LEO equatorial amateur radio system. The payload
consist of an L-band receive and S-band transmit transponder. Uplink: 1265 MHz,
Downlink: 2420 MHz Output power: 7 W