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  • ACRS 1995


    Poster Session 4

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    Thai Remote Sensing Satellite System

    Dr. Suvit Vibulsresth, Waraporn Suchaichit
    The National Research Council of Thailand (NRCT)
    196 Phaholyothin Road, Chatuchak
    Bangkok 10900, Thailand
    Tel. 662-5790116 Fax. 662-5613035


    Abstract
    In October 1994, the Ministry of Science, Technology and Environment (MOSTE) concluded a Memorandum of Understanding (MOU) with the Canadian Space Agency for cooperation in space technology and applications. An earth observation small sat mission, as the first cooperative mission under the MOU recently received the Thai Government approval. MOSTE, through its technical authority in the National Research Council of Thailand (NRCT) will own and operate the satellite system. This will be the first satellite to operate in an orbit dedicated to the equatorial regions. The first operational mission will extend the information available to both scientific and operational users and will augment data currently available from the Landsat series of spacecraft. This paper will present an overall system concept for the Smallsat Program, which will operate over its 5 years lift span.

    1. System Overview
    The purpose of the system is the provision of regularly updated multispectral image I data on an operational basis. Output from the system will take the form of image data products which can be distributed to users who will apply the data, either directly or after further processing, to the management of resources.

    2. System Architecture
    The essentilal elements of the Thai Remote Sensing Satellite System are : I. the Ground Segment .2. the Space Segment
    1. the Launch Segment
    2. the Space Segment
    3. the Launch Segment
    2.1 System Description and Performance

    2.1.1 Overall System Description

    The performance parameters of the Thai Remote Sensing Satellite System are summarized in the following tables.

    Table 2.1.1-1 Mission Performance
    Mission Life 5 years
    Orbit Type 73 orbits/5 days Multi -sun-syschronous
    Orbital Period 97 minutes
    Orbit Inclination 28 degrees
    Orbital Altitude 600 km
    Coverage Repeat Every 5 days
    Illumination Repeat 49 days
    Command Up link S-Band: 2 kbps
    Telemetry Downlink S-Band: Direct 2/4 kbps Playback 32/128 kbps
    Data Downlink X-Band: < 85 Mbps

    TABLE 2.1.1-2 Temporal Performance
    Parameter Value
    Revisit Time Twice every 5 days
    Accessibility Region 29.60N to 29.60S
    Maximum Imaging Capability 10 minutes/orbits
    Useable opportunities per year 63

    Table 2.1.1-3 Spatial Performance
    Parameter Value
    Swath Width 185 km imaged swath which is selectable within a 275 km accessibility region.
    Across Track Resolution 30 m (nadir)
    Along Track Resolution 30 m (madir)
    Geometric Distortion < 1/2 pixel Band to
    Band Registration < 1 pixel
    Image Locations < 5 km

    TABLE 2.1.1-4 Spectral Performance
    Parameter Value
    Spectral Bandwidths:  
    Blue 0.45 to 0.52 mm+01
    Green 0.52 to 0.60 mm+01
    Red 0.63 to 0.69 mm+01
    NIR 0.76 to 0.90 mm+01

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