The Design Progress of LAPAN-Chiba University SAR Micro-Satellite

R. H. Triharjanto, P. Budiantoro, Dwi Yanto, J. Sumantyo
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引用次数: 5

Abstract

The paper describes the progress in system and subsystem design of LAPAN-A5/ChibaSat, the 1st micro-satellite jointly developed by Satellite Technology Center, Indonesian National Institute for Aeronautics and Space (LAPAN), and Center for Environmental Remote Sensing, Chiba University. The satellite will carry synthetic aperture radar (SAR) payload for land cover and ice observation. Augmented with and automatic identification system (AIS) payload, the satellite will also carry maritime surveillance mission. As the Engineering Model of the SAR payload is completed in 2016, the design enters system/configuration phase. The focus of the design phase is to comply with launch constraint such as dimensional envelope and weight, as well as power budget and link budget, while ensuring that the fulfilment of mission objectives. The design method is trade-off study on simplified SAR micro-satellite design model. The design assumes to use bus subsystem heritage from previous LAPAN’s satellites. The design result shows the SAR missions required could be served within micro-satellite dimensional and weight constraints.
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lapan -千叶大学SAR微卫星设计进展
本文介绍了由卫星技术中心、印尼国家航空航天研究所(LAPAN)和千叶大学环境遥感研究中心联合研制的第一颗微型卫星LAPAN- a5 /ChibaSat的系统和子系统设计进展。该卫星将携带合成孔径雷达(SAR)有效载荷,用于陆地覆盖和冰观测。增强和自动识别系统(AIS)有效载荷,卫星也将执行海上监视任务。随着SAR有效载荷的工程模型于2016年完成,设计进入系统/配置阶段。设计阶段的重点是在保证完成任务目标的同时,满足尺寸包络线和重量等发射约束,以及功率预算和链路预算。设计方法是简化SAR微卫星设计模型的权衡研究。该设计假定使用从以前的LAPAN卫星继承的总线子系统。设计结果表明,在小卫星尺寸和重量限制的条件下,可以完成所需的SAR任务。
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