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LEADER 02541cam 2200529Ia 4500

001 ocm29019896;

003 OCoLC;

005 20080416075727.0;

007 he bmb024bbca;

008 931015s1989 vaua bb f000 0 eng d;

037 a| N 89-27671b| NASA;

049 a| ERE$;

074 a| 0830-D (MF);

074 a| 0830-D (online);

086 0 a| NAS 1.15:101605;

100 1 a| Suit, William T.q| (William Tull),d| 1937-=| ^A754764;

245 10 a| Summary of longitudinal stability and control parameters as determined from space shuttle Challenger flight test data /c| William T. Suit.;

300 a| 27 p. :b| ill.;

336 a| textb| txt2| rdacontent;

337 a| microformb| h2| rdamedia;

338 a| microficheb| he2| rdacarrier;

490 1 a| NASA technical memorandum ;v| 101605;

500 a| "July 1989.";

500 a| GPO Cataloging Record Distribution Program (CRDP).;

504 a| Includes bibliographical references (p. 9).;

530 a| Also available via Internet from the NTRS web site. Address as of 04/15/08: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890018300%5F1989018300.pdf ; current access is available via PURL.;

650 0 a| Stability of space vehicles.=| ^A333124;

650 0 a| Space shuttlesx| Testing.=| ^A192620;

650 7 a| Aerodynamic coefficients.2| nasat;

650 7 a| Challenger (Orbiter)2| nasat;

650 7 a| Force distribution.2| nasat;

650 7 a| Longitudinal stability.2| nasat;

650 7 a| Pitching moments.2| nasat;

650 7 a| Spacecraft control.2| nasat;

650 7 a| Spacecraft stability.2| nasat;

710 2 a| Langley Research Center.=| ^A192893;

830 0 a| NASA technical memorandumv| 101605.=| ^A467613;

856 41 u| https://purl.fdlp.gov/GPO/LPS93085;

949 a| NAS 1.15:101605w| sudoch| joyner32;

596 a| 1;

998 a| 1357022;

999 a| NAS 1.15:101605w| SUDOCc| 1i| MQ2515042l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 6/26/2008x| MICROFORMz| JFEDDOCSo| .STAFF. 0;

999 a| NAS 1.15:101605w| SUDOCc| 2i| MQ2515118l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 6/26/2008x| MICROFORMz| JFEDDOCSo| .STAFF. 0;

999 a| NAS 1.15:101605w| SUDOCc| 3i| MQ2515193l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 6/26/2008x| MICROFORMz| JFEDDOCSo| .STAFF. 0;

Summary of longitudinal stability and control parameters as determined from space shuttle Challenger flight test data / William T. Suit.

Author/creator	Suit, William T., 1937-
Other author	Langley Research Center.
Format	Microform
Publication Info	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, VA : For sale by the National Technical Information Service, 1989]
Description	27 p. : ill.
Supplemental Content	https://purl.fdlp.gov/GPO/LPS93085
Subjects	Stability of space vehicles. Space shuttles--Testing.

Series	NASA technical memorandum ; 101605 NASA technical memorandum 101605. ^A467613
General note	"July 1989."
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (p. 9).
Other forms	Also available via Internet from the NTRS web site. Address as of 04/15/08: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890018300%5F1989018300.pdf ; current access is available via PURL.
Reproduction note	Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1989. 1 microfiche : negative.
GPO item number	0830-D (MF)
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:101605
Stock number	N 89-27671 NASA

Availability

Library	Location	Call Number	Status
Joyner	Microforms B300	NAS 1.15:101605	✔ Available
Joyner	Microforms B300	NAS 1.15:101605	✔ Available
Joyner	Microforms B300	NAS 1.15:101605	✔ Available

Summary of longitudinal stability and control parameters as determined from space shuttle Challenger flight test data / William T. Suit.

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