Main Charactoristics of JERS-1 Satellite
Dimensions Bus body: approx 1m x 1.8m x 3.1m Box_shape
SAR Antenna: approx 12m x 2.5m
Solar Cell Paddle: approx 8m x 3.4mWeight approx 1.4 tons Attitude and Orbit
Control Subsystem3-Axis Attitude/Zero-momentum System Design Life 2 years Launch Vehicle H-1 Launch Vehicle Launch Site
Tanegashima Space Center
Launched Date Feburary 11, 1992 Orbit Sort of orbit Sun Synchronous
Subrecurrent OrbitAltitude approx 570km Orbit inclination approx 98 degree Period approx 96 minutes Recurrent period 44 days Local time at descending node a.m.10:30`a.m.11:00
JERS-1 is equipped with following instruments exclusively for
transmitting and recording observed data.Parameters of transmission and recording equipements
Mission Data Transmitter
[MDT]Carrier Frequency 8GHz Bands, 2 channels Moduration QPSK Power amplifier TWT(Helix type) Antenna type Shaped reflector beam antenna Mission Data Recorder
[MDR]Recording data rate 30Mbps x 2ch Recording Time 20 minutes
OPS major characteristics
OPtical Sensor
[OPS]Swath 75km Resolution 18m x 24m Number of
Observation
Bands3 visible and near infrared bands
1 stereo-viewing band
4 shortwave infrared bands
2. Reflectance characteristics of Minerals
The relation between the reflectance of minerals and the wavelength range of each short wave infrared(SWIR) bands are shown in the following figure.
The JERS-1 OPS band configuration and their effectiveness in mineral
classification with SWIR relative reflectance pattern.
An OPS Image shown below, is from typical altered zone, which is processed and analyzed by ERSDAC.
(Click the JPEGimage, then expand to GIF:903x900pixels, 1168kB)
JERS-1, OPS ratio compressed image(BGR=6/8, 2/1, 3/5).
Observation Date: October 9, 1992 Path 534-Row 239
Beatty, Nevada, USA.
The area high-lighted in yellow with ratio compressed, indicate
possibly containing gold-silver deposits in the Tertiary clastic rocks.
(central part of the image)
The areas covered by OPS obserations, are shown in green area of following chart.