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

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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Bibliographic Details
Main Authors: Srivastava, Sarthak, Anant Kumar Telikicherla Kandala, Gacal, Glenn Franco
Other Authors: School of Mechanical and Aerospace Engineering
Format: Conference Paper
Language:English
Published: 2021
Subjects:
Engineering::Mechanical engineering
Satellite
Very Low Earth Orbit
Online Access:https://digitalcommons.usu.edu/smallsat/2019/all2019/140/
https://hdl.handle.net/10356/148434

Internet

https://digitalcommons.usu.edu/smallsat/2019/all2019/140/
https://hdl.handle.net/10356/148434

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