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LEADER 02578cam a2200601Ka 4500

001 ocm38069266;

003 OCoLC;

005 20170609133719.0;

007 he bmb024b|ca;

008 971211s1996 vau b f000 0 eng d;

035 a| (Sirsi) o38069266;

037 a| N 97-13263b| NASA;

049 a| ERE$;

074 a| 0830-D (MF);

086 0 a| NAS 1.15:110296;

100 1 a| Blosser, Max L.=| ^A428915;

245 10 a| Development of metallic thermal protection systems for the reusable launch vehicle /c| Max L. Blosser.;

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| 110296;

500 a| Shipping list no.: 97-0960-M.;

500 a| CRDP Program record.;

650 0 a| Measuring instruments.=| ^A66121;

650 0 a| Honeycomb structures.=| ^A424669;

650 0 a| Heat resistant alloys.=| ^A257282;

650 0 a| Aerodynamic heating.=| ^A420455;

650 7 a| Aerodynamic heating.2| fast0| (OCoLC)fst00798175;

650 7 a| Heat resistant alloys.2| fast0| (OCoLC)fst00953953;

650 7 a| Honeycomb structures.2| fast0| (OCoLC)fst00959975;

650 7 a| Measuring instruments.2| fast0| (OCoLC)fst01013181;

650 7 a| Thermal protection.2| nasat;

650 7 a| Structural analysis.2| nasat;

650 7 a| Reusable launch vehicles.2| nasat;

650 7 a| Measuring instruments.2| nasat;

650 7 a| Payloads.2| nasat;

650 7 a| Loads (Forces)2| nasat;

650 7 a| Hypervelocity impact.2| nasat;

650 7 a| Honeycomb structures.2| nasat;

650 7 a| Heat resistant alloys.2| nasat;

650 7 a| Aerodynamic heating.2| nasat;

650 7 a| Acoustic fatigue.2| nasat;

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

776 08 i| Online version:a| Blosser, Max L.t| Development of metallic thermal protection systems for the reusable launch vehiclew| (OCoLC)973491877;

830 0 a| NASA technical memorandumv| 110296.=| ^A467613;

949 a| NAS 1.15:110296w| sudoch| joyner32;

596 a| 1;

998 a| 4473431;

999 a| NAS 1.15:110296w| SUDOCc| 1i| 4473431-1001l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 7/18/2016x| MICROFORMz| JFEDDOCSo| .STAFF. jjlm;

Development of metallic thermal protection systems for the reusable launch vehicle / Max L. Blosser.

Author/creator	Blosser, Max L.
Other author	Langley Research Center.
Format	Microform
Publication Info	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va.] : [National Technical Information Service, distributor], [1996]
Description	1 volume.
Subjects	Measuring instruments. Honeycomb structures. Heat resistant alloys. Aerodynamic heating.

Series	NASA technical memorandum ; 110296 NASA technical memorandum 110296. ^A467613
General note	Shipping list no.: 97-0960-M.
General note	CRDP Program record.
Reproduction note	Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997]. 1 microfiche.
Issued in other form	Online version: Blosser, Max L. Development of metallic thermal protection systems for the reusable launch vehicle
GPO item number	0830-D (MF)
Govt. docs number	NAS 1.15:110296
Stock number	N 97-13263 NASA

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Library	Location	Call Number	Status	Item Actions
Joyner	Microforms B300	NAS 1.15:110296	✔ Available

Development of metallic thermal protection systems for the reusable launch vehicle / Max L. Blosser.

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