Wake closure characteristics and afterbody heating on a Mars sample return orbiter

Aeroheating wind-tunnel tests were conducted on a 0.028 scale model of an orbiter concept considered for a possible Mars sample return mission. The primary experimental objectives were to characterize hypersonic near wake closure and determine if shear layer impingement would occur on the proposed o...

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Bibliographische Detailangaben

Hauptverfasser:	Horvath, T J, Cheatwood, F M, Wilmoth, R G, Alter, S J
Format:	Tagungsbericht
Sprache:	eng
Online-Zugang:	Volltext
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