Stability analysis and minimum thrust vector control requirements of booster vehicles during atmospheric flight

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041 0 ‡aeng
049 ‡aUIUU
086 0 ‡aNAS 1.14:D-4593
088 ‡aNASA-TN-D-4593
100 1 ‡aBorsody, Janos.
245 1 0 ‡aStability analysis and minimum thrust vector control requirements of booster vehicles during atmospheric flight / ‡cJanos Borsody, Fred Teren.
246 3 ‡aNASA TN D-4593
260 ‡aWashington, D. C. : ‡bNational Aeronautics and Space Administration ; ‡aSpringfield, Va. : ‡bfor sale by the Clearinghouse for Federal Scientific and Technical Information, ‡c1968.
300 ‡aii, 42 p. : ‡bill. ; ‡c26 cm.
490 0 ‡aNASA technical note ; ‡vD-4593
500 ‡aCover title.
500 ‡a"May 1968."
504 ‡aIncludes bibliographical references (p. 42).
538 ‡aMode of access: Internet.
650 0 ‡aLiquid propellant rockets ‡xDesign and construction.
650 0 ‡aBoundary layer.
650 0 ‡aRocket engines ‡xThrust.
650 0 ‡aStability of rockets.
700 1 ‡aTeren, Fred.
710 2 ‡aLewis Research Center.
710 1 ‡aUnited States. ‡bNational Aeronautics and Space Administration.
CID ‡a011446415
DAT 0 ‡a20101104152556.0 ‡b20141009010000.0
DAT 1 ‡a20141112165512.0 ‡b2023-03-13T18:14:57Z
CAT ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020
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