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001 ocn858246018;

003 OCoLC;

005 20171023100139.0;

006 m o d f ;

007 cr b|||||a|a||;

008 130912e200003 caua obt f000 0 eng c;

042 a| pcc;

049 a| ERE#;

074 a| 0830-D (online);

086 0 a| NAS 1.15:209021;

100 1 a| Gilyard, Glenn B.e| author.=| ^A420723;

245 10 a| Optimal pitch thrust-vector angle and benefits for all flight regimes /c| Glenn B. Gilyard, Alexander Bolonkin.;

264 1 a| Edwards, California :b| National Aeronautics and Space Administration, Dryden Flight Research Center,c| March 2000.;

300 a| 1 online resource (22 pages) :b| illustrations.;

336 a| textb| txt2| rdacontent;

337 a| computerb| c2| rdamedia;

338 a| online resourceb| cr2| rdacarrier;

490 1 a| NASA/TM ;v| 2000-209021;

500 a| "March 2000.";

500 a| "Performing organization: NASA Dryden Flight Research Center"--Report documentation page.;

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

504 a| Includes bibliographical references (page 22).;

513 a| Technical memorandum.;

536 a| Sponsored by the National Aeronautics and Space Administrationd| WU 522-16-14-00-39-00-LIOd| H-2402;

588 a| Description based on online resource; title from PDF title page (NASA, viewed Oct. 23, 2017).;

650 7 a| Pitch (Inclination)2| nasat;

650 7 a| Thrust vector control.2| nasat;

650 7 a| Automatic flight control.2| nasat;

650 7 a| Angles (Geometry)2| nasat;

700 1 a| Bolonkin, Alexander,e| author.=| ^A454450;

710 2 a| Hugh L. Dryden Flight Research Centere| issuing body.=| ^A425209;

776 08 i| Print version:a| Gilyard, Glenn B.t| Optimal pitch thrust-vector angle and benefits for all flight regimesw| (OCoLC)45534249;

776 08 i| Microfiche version:a| Gilyard, Glenn B.t| Optimal pitch thrust-vector angle and benefits for all flight regimesw| (OCoLC)45009655;

830 0 a| NASA technical memorandumv| 2000-209021.=| ^A467613;

856 40 u| https://purl.fdlp.gov/GPO/gpo85803;

949 a| Click on web addressw| asish| joyner94;

596 a| 1;

998 a| 4789907;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 4789907-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 11/21/2017x| EDOCUMENTz| JERESOURCE;

Optimal pitch thrust-vector angle and benefits for all flight regimes / Glenn B. Gilyard, Alexander Bolonkin.

Author/creator	Gilyard, Glenn B. author.
Other author	Bolonkin, Alexander, author.
Other author	Hugh L. Dryden Flight Research Center issuing body.
Format	Electronic
Publication	Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, March 2000.
Description	1 online resource (22 pages) : illustrations.
Supplemental Content	https://purl.fdlp.gov/GPO/gpo85803

Series	NASA/TM ; 2000-209021 NASA technical memorandum 2000-209021. ^A467613
General note	"March 2000."
General note	"Performing organization: NASA Dryden Flight Research Center"--Report documentation page.
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (page 22).
Report note	Technical memorandum.
Funding information	Sponsored by the National Aeronautics and Space Administration WU 522-16-14-00-39-00-LIO H-2402
Source of description	Description based on online resource; title from PDF title page (NASA, viewed Oct. 23, 2017).
Issued in other form	Print version: Gilyard, Glenn B. Optimal pitch thrust-vector angle and benefits for all flight regimes
Issued in other form	Microfiche version: Gilyard, Glenn B. Optimal pitch thrust-vector angle and benefits for all flight regimes
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:209021

Library	Location	Call Number	Status	Item Actions
	Electronic Resources	Access Content Online	✔ Available

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