Exploratory investigation at mach number of 2.01 of the longitudinal stability and control characteristics of a winged reentry configuration

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035	⊔	⊔	‡asdr-uiuc6357409
035	⊔	⊔	‡a(OCoLC)502142154
040	⊔	⊔	‡aCSL ‡cTEF
049	⊔	⊔	‡aUIUU
050	⊔	4	‡aTL1050 ‡b.F67 1959
100	1	⊔	‡aFoster, Gerald V.
245	1	0	‡aExploratory investigation at mach number of 2.01 of the longitudinal stability and control characteristics of a winged reentry configuration / ‡cby Gerald V. Foster.
260	⊔	⊔	‡aWashington [D.C.] : ‡bNational Aeronautics and Space Administration, ‡c[1959]
300	⊔	⊔	‡a21 p. : ‡b8 ill. ; ‡c27 cm.
490	0	⊔	‡aNASA technical memorandum ; ‡vX-178
500	⊔	⊔	‡a"December 1959."
500	⊔	⊔	‡aCover title.
504	⊔	⊔	‡aIncludes bibliographical references (p. 7).
538	⊔	⊔	‡aMode of access: Internet.
650	⊔	0	‡aAerodynamics, Supersonic.
650	⊔	0	‡aSpace vehicles ‡xAtmospheric entry.
650	⊔	0	‡aStability of space vehicles.
710	1	⊔	‡aUnited States. ‡bNational Aeronautics and Space Administration.
CID	⊔	⊔	‡a011424007
DAT	0	⊔	‡a20101001093005.0 ‡b20141013010000.0
DAT	1	⊔	‡a20141112173021.0 ‡b2024-01-17T02:06:49Z
CAT	⊔	⊔	‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020
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974	⊔	⊔	‡bUIU ‡cUIUC ‡d20240117 ‡sgoogle ‡uuiug.30112106659060 ‡y1959 ‡rpd ‡qbib ‡tUS fed doc