Tools

LEADER 02109cam 2200469 i 4500

001 ocm56388022;

003 OCoLC;

005 20220425150541.0;

007 he bmb024baca;

008 040830e199801 ohua bbt f000 0 eng d;

035 a| (Sirsi) o56388022;

049 a| ERE$;

074 a| 0830-D;

086 0 a| NAS 1.15:1998-206313;

100 1 a| Wadel, Mary F.,e| author.=| ^A431894;

245 10 a| Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber with development of an optimized design /c| Mary F. Wadel.;

264 1 a| Cleveland, Ohio :b| National Aeronautics and Space Administration, Lewis Research Center,c| January 1998.;

300 a| 1 volume :b| illustrations.;

336 a| textb| txt2| rdacontent;

337 a| microformb| h2| rdamedia;

338 a| microficheb| he2| rdacarrier;

490 1 a| NASA/TM ;v| 1998-206313;

500 a| "January 1998.";

500 a| Shipping list no.: 1999-0238-M.;

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

504 a| Includes bibliographical references (page 11).;

650 0 a| Rocket enginesx| Combustion.=| ^A680280;

650 7 a| Combustion chambers.2| fast0| (OCoLC)fst00869044;

650 7 a| Rocket enginesx| Combustion.2| fast0| (OCoLC)fst01099300;

650 7 a| Combustion chambers.2| nasat;

650 7 a| Aspect ratio.2| nasat;

650 7 a| Rocket engines.2| nasat;

710 2 a| Lewis Research Center,e| issuing body.=| ^A367825;

776 08 i| Online version:a| Wadel, Mary Ft| Comparison of high aspect ratio cooling channel designs for a rocket combustion chamberw| (OCoLC)981463550;

830 0 a| NASA technical memorandum ;v| 1998-206313.=| ^A467613;

922 a| UNREPORTEDPUBSASKGPO;

949 a| NAS 1.15:1998-206313w| sudoch| joyner32;

596 a| 1;

998 a| 5796736;

999 a| NAS 1.15:1998-206313w| SUDOCc| 1i| 5796736-1001l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 3/14/2022x| MICROFORMz| JFEDDOCS;

Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber with development of an optimized design / Mary F. Wadel.

Author/creator	Wadel, Mary F. author.
Other author	Lewis Research Center, issuing body.
Format	Microform
Publication	Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, January 1998.
Description	1 volume : illustrations.
Subjects	Rocket engines--Combustion.

Series	NASA/TM ; 1998-206313 NASA technical memorandum ; 1998-206313. ^A467613
General note	"January 1998."
General note	Shipping list no.: 1999-0238-M.
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (page 11).
Reproduction note	Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998]. 1 microfiche : negative.
Issued in other form	Online version: Wadel, Mary F Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber
GPO item number	0830-D
Govt. docs number	NAS 1.15:1998-206313

Availability

Library	Location	Call Number	Status	Item Actions
Joyner	Microforms B300	NAS 1.15:1998-206313	✔ Available

Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber with development of an optimized design / Mary F. Wadel.

Click here for more information about this title

Availability