Design of a Novel Hypersonic Inflatable Aerodynamic Decelerator for Mars Entry, Descent, and Landing
AIAA Atmospheric Flight Mechanics Conference
01.01.2017
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Uncertainty Analysis of Mars Entry Flows over a Hypersonic Inflatable Aerodynamic Decelerator
Online Contents | 2015
|British Library Conference Proceedings | 2011
|Morphing Hypersonic Inflatable Aerodynamic Decelerator
British Library Conference Proceedings | 2013
|