INSPIRESAT-4/ARCADE : a VLEO mission for atmospheric temperature measurements and ionospheric plasma characterization

Most nano-satellite and small satellite missions are designed for 400 km or higher altitudes. This is because small satellites, with mass, volume and power constraints, have limited propulsion capabilities to counteract the high aerodynamic drag in lower altitudes. Thus little or no science data...

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Main Authors: Srivastava, Sarthak, Anant Kumar Telikicherla Kandala, Gacal, Glenn Franco
其他作者: School of Mechanical and Aerospace Engineering
格式: Conference or Workshop Item
語言:English
出版: 2021
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在線閱讀:https://digitalcommons.usu.edu/smallsat/2019/all2019/140/
https://hdl.handle.net/10356/148434
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機構: Nanyang Technological University
語言: English