A Hybrid Propulsion-Based Mission Architecture for the Removal of Debris from Low-Earth Orbit

A Hybrid Propulsion-Based Mission Architecture for the Removal of Debris from Low-Earth Orbit

Satellite technology has advanced with rising demand from the service sector, but increased accessibility also raises risks to the orbital environment. Space debris in low-Earth orbit (LEO) poses a major threat to satellite operations and access to space. Potential solutions for debris removal inclu...

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Bibliographic Details
Main Authors: Sasi Kiran Palateerdham, Abdul Rahman, Emiliano Ortore, Antonella Ingenito
Format: Article
Language:English
Published: MDPI AG 2025-03-01
Series:Engineering Proceedings
Subjects:
space debris
active removal method
hybrid rocket
mission design
Online Access:https://www.mdpi.com/2673-4591/90/1/4
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