Tools

LEADER 02445cam 2200577Ka 4500

001 ocm39682343;

003 OCoLC;

005 20161027124535.0;

008 980812s1996 dcu b f000 0 eng d;

019 a| 83143335;

035 a| (Sirsi) o39682343;

037 a| 19960035853b| NASA;

049 a| ERE$;

074 a| 0830-D (MF);

086 0 a| NAS 1.15:107270;

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

245 10 a| Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f] thrust combustion chamber /c| Mary F. Wadel and Michael L. Meyer.;

300 a| 1 volume.;

336 a| textb| txt2| rdacontent;

337 a| microformb| h2| rdamedia;

338 a| microficheb| he2| rdacarrier;

490 1 a| NASA technical memorandum ;v| 107270;

500 a| Shipping list no.: 98-0769-M.;

500 a| CRDP Project record.;

650 0 a| Rocket engines.=| ^A313534;

650 0 a| Combustion chambers.=| ^A420746;

650 0 a| Liquid hydrogen.=| ^A426333;

650 0 a| Cooling.=| ^A424609;

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

650 7 a| Cooling.2| fast0| (OCoLC)fst00878073;

650 7 a| Liquid hydrogen.2| fast0| (OCoLC)fst00999588;

650 7 a| Rocket engines.2| fast0| (OCoLC)fst01099299;

650 7 a| Rocket engines.2| nasat;

650 7 a| Combustion chambers.2| nasat;

650 7 a| Thrust chambers.2| nasat;

650 7 a| Mass flow.2| nasat;

650 7 a| Liquid hydrogen.2| nasat;

650 7 a| Cooling.2| nasat;

650 7 a| High aspect ratio.2| nasat;

650 7 a| Performance tests.2| nasat;

700 1 a| Meyer, Michael L.=| ^A426645;

710 1 a| United States.b| National Aeronautics and Space Administration.=| ^A5437;

776 08 i| Online version:a| Wadel, Mary F.t| Validation of high aspect ratio cooling in a 89 kN (20,000 lbf) thrust combustion chamberw| (OCoLC)953734717;

830 0 a| NASA technical memorandumv| 107270.=| ^A467613;

949 a| NAS 1.15:107270w| sudoch| joyner32;

596 a| 1;

998 a| 4472686;

999 a| NAS 1.15:107270w| SUDOCc| 1i| 4472686-1001l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 7/15/2016x| MICROFORMz| JFEDDOCSo| .STAFF. jjlm;

Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f] thrust combustion chamber / Mary F. Wadel and Michael L. Meyer.

Author/creator	Wadel, Mary F.
Other author	Meyer, Michael L.
Other author	United States. National Aeronautics and Space Administration.
Format	Book
Publication Info	[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va.] : [National Technical Information Service, distributor], [1996]
Description	1 volume.
Subjects	Rocket engines. Combustion chambers. Liquid hydrogen. Cooling.

Series	NASA technical memorandum ; 107270 NASA technical memorandum 107270. ^A467613
General note	Shipping list no.: 98-0769-M.
General note	CRDP Project record.
Reproduction note	Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997]. 1 microfiche.
Issued in other form	Online version: Wadel, Mary F. Validation of high aspect ratio cooling in a 89 kN (20,000 lbf) thrust combustion chamber
GPO item number	0830-D (MF)
Govt. docs number	NAS 1.15:107270
Stock number	19960035853 NASA

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Library	Location	Call Number	Status	Item Actions
Joyner	Microforms B300	NAS 1.15:107270	✔ Available

Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f] thrust combustion chamber / Mary F. Wadel and Michael L. Meyer.

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