Aerodynamic force and moment computations for very low Earth orbit satellites using a TPMC model

Aerodynamic force and moment computations for very low Earth orbit satellites using a TPMC model

The recent upswing in satellite operations of very low Earth orbit has triggered the necessity to evaluate aerodynamic forces and moments, which can significantly affect satellite orbit. The present paper evaluates the aerodynamic forces and pitching moment on a satellite design using the test parti...

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Bibliographic Details
Main Authors: Ramesh, Sai Sudha, Elhadidi, Basman, Khoo, Boo Cheong, Chan, Wai Lee
Other Authors: School of Mechanical and Aerospace Engineering
Format: Article
Language:English
Published: 2025
Subjects:
Earth and Environmental Sciences
Very low Earth orbit
Satellite drag
Online Access:https://hdl.handle.net/10356/182134
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Institution: Nanyang Technological University
Language: English

Internet

https://hdl.handle.net/10356/182134

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