Angle-of-attack measurements of a hypersonic reentry vehicle derivedfrom flight test pressure data.
CASSANTO, J. M. /GENERAL ELECTRIC CO., MISSILE AND SPACE DIV., KING OF PRUSSIA, PA./.
JOURNAL OF SPACECRAFT AND ROCKETS ; 3 , 11 ; 1685-1686
1966-01-01
2 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
AIAA 2006-0582 Hypersonic Reentry Vehicle Wake Flow Fields at Angle of Attack
British Library Conference Proceedings | 2006
|Hypersonic reentry vehicle Patent
NTRS | 1967
|