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001 ocm24900172;

003 OCoLC;

005 20060728084750.0;

007 he bmb024bbca;

008 911206s1989 dcua bbt f000 0 eng d;

037 a| N 90-11741b| NASA;

049 a| ERE$;

074 a| 0830-D (MF);

074 a| 0830-D (online);

086 0 a| NAS 1.15:4140;

088 a| H-1556;

100 1 a| Conners, Timothy R.?| UNAUTHORIZED;

245 10 a| Measurement effects on the calculation of in-flight thrust for an F404 turbofan engine /c| Timothy R. Conners.;

300 a| 21 p. :b| ill. ;c| 28 cm.;

336 a| textb| txt2| rdacontent;

337 a| microformb| h2| rdamedia;

338 a| microficheb| he2| rdacarrier;

490 1 a| NASA technical memorandum ;v| 4140;

500 a| Shipping list no.: 90-0398-M.;

530 a| Also available via Internet from the NASA Technical Report Server web site. Address as of 7/28/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900002425%5F1990002425.pdf; current access available via PURL.;

504 a| Includes bibliographical references (p. 8).;

500 a| "Performing organization report no.: H-1556"--Technical rept. documentation p.;

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

536 h| RTOP 533-02-51;

650 0 a| Airplanesx| Turbofan enginesx| Testing.=| ^A589846;

650 7 a| Afterburning.2| nasat;

650 7 a| In-flight monitoring.2| nasat;

650 7 a| Thrust measurement.2| nasat;

650 7 a| Turbofan engines.2| nasat;

710 1 a| United States.b| National Aeronautics and Space Administration.b| Scientific and Technical Information Division.=| ^A634451;

830 0 a| NASA technical memorandumv| 4140.=| ^A467613;

856 41 u| https://purl.fdlp.gov/GPO/LPS72304;

949 a| NAS 1.15:4140w| sudoch| joyner32;

596 a| 1;

998 a| 1055287;

999 a| NS 1.15:4140w| SUDOCc| 1i| MQ1857927d| 8/7/2007l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 9/19/2006x| MICROFORMz| JFEDDOCSo| .STAFF. 0;

Measurement effects on the calculation of in-flight thrust for an F404 turbofan engine / Timothy R. Conners.

Author/creator	Conners, Timothy R.
Other author	United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Format	Microform
Publication Info	[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, VA : For sale by the National Technical Information Service], 1989.
Description	21 p. : ill. ; 28 cm.
Supplemental Content	https://purl.fdlp.gov/GPO/LPS72304
Subjects	Airplanes--Motors. --Thrust. --Measurement. Airplanes--Turbofan engines. --Testing.

Series	NASA technical memorandum ; 4140 NASA technical memorandum 4140. ^A467613
General note	Shipping list no.: 90-0398-M.
General note	"Performing organization report no.: H-1556"--Technical rept. documentation p.
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (p. 8).
Other forms	Also available via Internet from the NASA Technical Report Server web site. Address as of 7/28/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900002425%5F1990002425.pdf; current access available via PURL.
Reproduction note	Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1990] 1 microfiche : negative.
Funding information	RTOP 533-02-51
Technical rpt number	H-1556
GPO item number	0830-D (MF)
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:4140
Stock number	N 90-11741 NASA

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Library	Location	Call Number	Status	Item Actions
Joyner	Microforms B300	NS 1.15:4140	✔ Available

Measurement effects on the calculation of in-flight thrust for an F404 turbofan engine / Timothy R. Conners.

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