Micro- and mini-satellites of ISRO-technology and applications

被引:2
|
作者
Thyagarajan, K. [1 ]
Murthy, D. V. A. Raghava [1 ]
机构
[1] ISRO, Satellite Ctr, Bangalore, Karnataka, India
关键词
D O I
10.1016/j.actaastro.2009.03.050
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
With rich experience of the successful Indian remote sensing satellite series, Indian Space Research Organization (ISRO) has started theme-based satellites like Resourcesat and Oceansat. Further taking the advantage of the improved technologies in areas of miniaturization, the micro- and mini-satellite series have been started, which will provide opportunity for the payloads of stand-alone missions, for applications, study or research. These include payloads for Earth imaging. atmospheric monitoring, ocean monitoring, scientific applications, and stellar observation. The micro-satellites are of 100 kg class, planned with a payload of about 30 kg and 20 W power and mini-satellites of 450 kg class for payloads of 200 kg and power of 200 W. The first satellite in the micro-satellite series is an Earth imaging payload followed by the second satellite with scientific payloads with the participation of students. Further the scientific proposals for micro-satellites are under evaluation. Similarly the first two missions of mini-satellites are defined with first one carrying ocean and environment monitoring payloads followed by the Earth imaging satellite with multi-spectral camera with 700 km swath. The Current paper touches upon the technology involved in realization of the micro- and mini-satellites and the scope of applications of the series. (C) 2009 Published by Elsevier Ltd.
引用
收藏
页码:1375 / 1382
页数:8
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