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001 ocn760962522;

003 OCoLC;

005 20140910083736.0;

006 m o d f ;

007 cr bn|||||||||;

008 111114e198012 dcua obt f000 0 eng c;

035 a| (Sirsi) o760962522;

042 a| pcc;

049 a| ERE#;

074 a| 0830-H-15 (online);

086 0 a| NAS 1.60:1785;

100 1 a| Camarda, Charles J.,e| author.=| ^A444305;

245 10 a| Tests of graphite/polyimide sandwich panels in uniaxial edgewise compression /c| Charles J. Camarda.;

264 1 a| Washington, District of Columbia :b| National Aeronautics and Space Administration, Scientific and Technical Information Branch,c| December 1980.;

300 a| 1 online resource (76 pages) :b| illustrations.;

336 a| textb| txt2| rdacontent;

337 a| computerb| c2| rdamedia;

338 a| online resourceb| cr2| rdacarrier;

490 1 a| NASA technical paper ;v| 1785;

500 a| Title from title screen (viewed Sept. 10, 2014).;

500 a| "December 1980.";

504 a| Includes bibliographical references.;

536 a| Sponsored by National Aeronautics and Space Administrationd| 506-53-63-04d| L-13998;

650 0 a| Structural stability.=| ^A162244;

650 0 a| Buckling (Mechanics)=| ^A53375;

650 0 a| Graphitex| Testing.=| ^A54927;

650 0 a| Space vehiclesx| Design and construction.=| ^A332419;

650 0 a| Sandwich construction.=| ^A814441;

650 7 a| Buckling (Mechanics)2| fast0| (OCoLC)fst00840001;

650 7 a| Graphitex| Testing.2| fast0| (OCoLC)fst00946673;

650 7 a| Sandwich construction.2| fast0| (OCoLC)fst01104954;

650 7 a| Space vehiclesx| Design and construction.2| fast0| (OCoLC)fst01127992;

650 7 a| Structural stability.2| fast0| (OCoLC)fst01135711;

776 08 i| Print version:a| Camarda, Charles J.t| Tests of graphite/polymide sandwich panels in uniaxial edgewise compressionw| (OCoLC)7318474;

830 0 a| NASA technical paperv| 1785.=| ^A367864;

856 40 u| https://purl.fdlp.gov/GPO/gpo51871;

949 a| Click on web addressw| ASISh| JOYNER94;

998 a| 3652225;

998 a| u3652225;

596 a| 1;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 3652225-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 10/22/2014x| EDOCUMENTz| JERESOURCE;

Tests of graphite/polyimide sandwich panels in uniaxial edgewise compression / Charles J. Camarda.

Author/creator	Camarda, Charles J. author.
Other author	United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch issuing body.
Format	Electronic
Publication	Washington, District of Columbia : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
Description	1 online resource (76 pages) : illustrations.
Supplemental Content	https://purl.fdlp.gov/GPO/gpo51871
Subjects	Structural stability. Buckling (Mechanics) Graphite--Testing. Space vehicles--Design and construction. Sandwich construction.

Series	NASA technical paper ; 1785 NASA technical paper 1785. ^A367864
General note	Title from title screen (viewed Sept. 10, 2014).
General note	"December 1980."
Bibliography note	Includes bibliographical references.
Funding information	Sponsored by National Aeronautics and Space Administration 506-53-63-04 L-13998
Issued in other form	Print version: Camarda, Charles J. Tests of graphite/polymide sandwich panels in uniaxial edgewise compression
GPO item number	0830-H-15 (online)
Govt. docs number	NAS 1.60:1785

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Tests of graphite/polyimide sandwich panels in uniaxial edgewise compression / Charles J. Camarda.

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