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003 OCoLC;

005 20141208173902.0;

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035 a| (Sirsi) o167963838;

035 a| (OCoLC)167963838;

040 a| GPOc| GPOd| MvId| UtOrBLW;

049 a| ERE$;

074 a| 0830-D (MF);

086 0 a| NAS 1.15:87653;

100 1 a| Siemers, Paul M.=| ^A695784;

245 10 a| Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the AEDC 16T propulsion wind tunnel /c| Paul M. Siemers, III and Martin W. Henry.;

260 a| Hampton, Va. :b| National Aeronautics and Space Administration, Langley Research Center,c| [1986];

300 a| 1 volume.;

336 a| text2| rdacontent;

337 a| microform2| rdamedia;

338 a| microfiche2| rdacarrier;

490 1 a| NASA technical memorandum ;v| 87653;

650 0 a| Space shuttles.=| ^A192620;

650 0 a| Aerodynamic load.=| ^A613621;

650 7 a| Forebodies.2| nasat;

650 7 a| Pressure distribution.2| nasat;

650 7 a| Space shuttle orbiters.2| nasat;

650 7 a| Wind tunnel tests.2| nasat;

700 1 a| Henry, Martin W.?| UNAUTHORIZED;

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

830 0 a| NASA technical memorandumv| 87653.=| ^A467613;

596 a| 1;

998 a| 1269409;

999 a| NAS 1.15:87653w| SUDOCc| 1i| MQ2263701l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 10/17/2007x| MICROFORMz| JFEDDOCSo| .STAFF. 0;

Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the AEDC 16T propulsion wind tunnel / Paul M. Siemers, III and Martin W. Henry.

Author/creator	Siemers, Paul M.
Other author	Henry, Martin W.
Other author	Langley Research Center.
Format	Book
Publication Info	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
Description	1 volume.
Subjects	Space shuttles. Aerodynamic load.

Series	NASA technical memorandum ; 87653 NASA technical memorandum 87653. ^A467613
Reproduction note	Joyner- Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1986. 5 microfiches.
GPO item number	0830-D (MF)
Govt. docs number	NAS 1.15:87653

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Library	Location	Call Number	Status	Item Actions
Joyner	Microforms B300	NAS 1.15:87653	✔ Available

Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the AEDC 16T propulsion wind tunnel / Paul M. Siemers, III and Martin W. Henry.

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