Rarefied-flow shuttle aerodynamics flight model

A model of the Shuttle Orbiter rarefied-flow aerodynamic force coefficients has been derived from the ratio of flight acceleration measurements. The in situ, low-frequency (less than 1 Hz), low-level (1) x 10 exp -6 g) acceleration measurements are made during atmospheric re-entry. The experiment eq...

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Bibliographische Detailangaben

Veröffentlicht in:	Journal of spacecraft and rockets 1994-07, Vol.31 (4), p.550-556
Hauptverfasser:	Blanchard, Robert C, Larman, Kevin T, Moats, Christina D
Format:	Artikel
Sprache:	eng
Online-Zugang:	Volltext
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