Load relief autopilot analysis to minimize launch vehicle peak thrust vector deflection requirements

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005 20141009010000.0
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035 ‡asdr-uiuc6401311
035 ‡a(OCoLC)52303226
040 ‡aEGM ‡cEGM ‡dOCLCQ
049 ‡aUIUU
050 4 ‡aTL521 ‡b.A3525 no. 4786
100 1 ‡aScalzott, Leslie L.
245 1 0 ‡aLoad relief autopilot analysis to minimize launch vehicle peak thrust vector deflection requirements / ‡cLeslie L. Scalzott and Fred Teren.
246 3 ‡aNASA TN D-4786
260 ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration : ‡b[For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], ‡c1968.
300 ‡aii, 39 p. : ‡bill. ; ‡c27 cm.
490 0 ‡aNASA technical note ; ‡vD-4786
504 ‡aIncludes bibliographical references (p. 39).
538 ‡aMode of access: Internet.
650 0 ‡aAutomatic pilot (Airplanes)
700 1 ‡aTeren, Fred.
710 1 ‡aUnited States. ‡bNational Aeronautics and Space Administration.
CID ‡a011444279
DAT 0 ‡a20101109112150.0 ‡b20141009010000.0
DAT 1 ‡a20141112165512.0 ‡b2024-01-26T18:54:03Z
CAT ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020
FMT ‡aBK
HOL ‡0sdr-uiuc6401311 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106745943 ‡sUIU ‡16401311
974 ‡bUIU ‡cUIUC ‡d20240126 ‡sgoogle ‡uuiug.30112106745943 ‡y1968 ‡ric ‡qbib ‡tUS bib date1 >= 1929