Effects of solar panels on Aerodynamics of a small satellite with deployable aero-brake-Reference-Cited by-同舟云学术

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Effects of solar panels on Aerodynamics of a small satellite with deployable aero-brake

Published:2018-10 Issue: Volume:151 Page:456-466
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Mungiguerra S.,Zuppardi G.,Spanò Cuomo L.,Savino R.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference31 articles.

1. Inflatable Re-entry and descent Technology (IRDT) – further developments;Wilde,2001

2. Structural analysis and testing of the inflatable Re-entry vehicle experiment (IRVE);Lindell,2006

3. Nanosat de-orbit and recovery system to enable new missions;Andrews,2011

4. The parashield entry vehicle concept: basic theory and flight test developments;Akin,1990

5. A small re-entry capsule BREMSAT 2;Wiegand,1996

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1. Inflatable aerodynamic decelerator for CubeSat reentry and recovery: Altitude effects on the flowfield structure;Aerospace Science and Technology;2023-07

2. The State of the Art of Information Integration in Space Applications;IEEE Access;2022

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