Loading…
Design of an Intake and a Thruster for an Atmosphere-Breathing Electric Propulsion System
Challenging space missions include those at very low altitudes, where the atmosphere is source of aerodynamic drag on the spacecraft that finally defines the missions lifetime unless way to compensate for it is provided. This environment is named Very Low Earth Orbit (VLEO) and is defined for \(h
Saved in:
Published in: | arXiv.org 2022-11 |
---|---|
Main Authors: | , , , , , , , , , , , , , , , , , , , , , , , , , , , |
Format: | Article |
Language: | English |
Subjects: | |
Online Access: | Get full text |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Summary: | Challenging space missions include those at very low altitudes, where the atmosphere is source of aerodynamic drag on the spacecraft that finally defines the missions lifetime unless way to compensate for it is provided. This environment is named Very Low Earth Orbit (VLEO) and is defined for \(h |
---|---|
ISSN: | 2331-8422 |
DOI: | 10.48550/arxiv.2211.10079 |