Longitudinal stability analysis of a suborbital re-entry demonstrator for a deployable capsule

In the field of atmospheric re-entry technology several research and industrial projects are based on the design of deployable, umbrella-like Thermal Protection Systems (TPSs) and aero-brakes. These systems are made of flexible, high temperature resistant fabrics, folded at launch and deployed in sp...

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Veröffentlicht in:	Acta astronautica 2015-01, Vol.106, p.101-110
Hauptverfasser:	Iacovazzo, Michele, Carandente, Valerio, Savino, Raffaele, Zuppardi, Gennaro
Format:	Artikel
Sprache:	eng
Schlagworte:	Atmospherics CFD method Continuums Deployable aero-braking capsule Deployable structures DSMC method Flight Launches Longitudinal stability Spacecraft Suborbital demonstrative entry mission Thermal protection
Online-Zugang:	Volltext
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