suitabilities of the onboard sensors. The name of the Marine
Observation Satellite MOS-1 is related to this reason.
Design features
At present, the MOS-1 is in a conception design phase and
its onboard sensors are now under preliminary development.
Table 1 shows a general conception of this MOS-1, indicating the
orbit parameters, the characteristics of the sensors and the com-
munication equipment.
The planned orbit is a non-sun- synchronous one which is
about 540 km high and about 70 degrees in orbit inclination.
This orbit was selected taking into account many factors such as
the mission objectives, the launching rocket capability, the launch-
ing range safety, etc.. However, an higher altitude orbit may
have the preference if the resolution of the onboard sensors could
be improved.
Three sensors are selected : a Visible and near-infrared
scanning radiometer ( VNIR ), a Visible and thermal-infrared
scanning radiometer ( VTIR ) and a Microwave scanning radiometer
(MSR ). The VNIR observes sea surface colors which relate to
the content of vegetal plankton. The VTIR measures sea surface
temperature. The MSR measures sea-surface temperature and
water vapour distribution.
For the communication equipment which transmits the above-
mentioned sensor data to the earth station, 21 GHz band is selected
taking into consideration the present international frequency allo-
cation as wellas the frequency bandwidth required. However, a
15 GHz band is an alternate candidate, considering a new interna-
tional allocation in future.
The estimated weight of the satellite is about 500 kg. The
electric power required is about 300 W. The satellite attitude
control system is of 3-axis type, whose accuracies are * 0.5? for
pitch and roll and Y0.7° for yaw. This satellite is scheduled to
be launched arround 1983, and its design life will be about 2 years.
Ground System for Receiving Landsat Data
General
The objectives of the establishment of the ground system for
receiving Landsat data are to develop advanced use of Landsat data
as well as to promote the development of Japanese Earth observation
satellites.
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