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1

The NASA scope and subject category guide:

United States. National Aeronautics and Space Administration. Scientific and Technical Information Office. Center for Aerospace Information
http://hdl.handle.net/2027/pst.000045008962.  , 2000
Link: http://hdl.handle.net/20..
 
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2

Life and Biomedical Sciences and Applications Advisory Subc..:

Frankel, Paula Burnett ; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office ; United States. Office of Life and Microgravity Sciences and Applications.
http://hdl.handle.net/2027/pst.000025492743.  , 1995
Link: http://hdl.handle.net/20..
 
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3

An application of retroduction to anlyzing and testing the ..:

Kerley, James J ; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
http://hdl.handle.net/2027/uiug.30112106566224.  , 1987
Link: http://hdl.handle.net/20..
 
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4

Structural concepts for large solar concentrators:

Hedgepeth, John M ; Miller, Richard K. (Richard Keith), 1949- ; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office..
http://hdl.handle.net/2027/uiug.30112106862292.  , 1987
Link: http://hdl.handle.net/20..
 
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5

Ground and flight test results of a total main rotor isolat..:

Halwes, Dennis R ; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
http://hdl.handle.net/2027/uiug.30112106862235.  , 1987
Link: http://hdl.handle.net/20..
 
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6

Static internal performance of a two-dimensional convergent..:

Bare, E. Ann ; Reubush, David E ; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
http://hdl.handle.net/2027/uiug.30112106605816.  , 1987
Link: http://hdl.handle.net/20..
 
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7

Effects of aerosols and surface shadowing on bidirectional ..:

Bowker, David E ; Davis, Richard E ; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
http://hdl.handle.net/2027/uiug.30112106606046.  , 1987
Link: http://hdl.handle.net/20..
 
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8

Quick-look guide to the Crustal Dynamics Project's Data Inf..:

Noll, Cary E ; Linder, Henry G ; Behnke, Jeanne M.
http://hdl.handle.net/2027/uiug.30112106616185.  , 1987
Link: http://hdl.handle.net/20..
 
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9

Effect of planform taper on hover performance of an advance..:

Kelley, Henry L ; United States. Army Aviation Research and Technology Activity ; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
http://hdl.handle.net/2027/uiug.30112018023447.  , 1987
Link: http://hdl.handle.net/20..
 
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10

Continuous prediction of spartan visibility from orbiter ov..:

King, Joseph C ; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
http://hdl.handle.net/2027/uiug.30112005560740.  , 1987
Link: http://hdl.handle.net/20..
 
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11

Problems in merging earth sensing satellite data sets:

Smith, Paul H ; Goldberg, Michael J ; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
http://hdl.handle.net/2027/uiug.30112106616284.  , 1987
Link: http://hdl.handle.net/20..
 
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12

Evolution, calibration, and operational characteristics of ..:

Ladson, Charles L ; Ray, Edward J ; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
http://hdl.handle.net/2027/uiug.30112106606186.  , 1987
Link: http://hdl.handle.net/20..
 
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13

Survey of currently available high-resolution raster graphi..:

Jones, Denise R ; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
http://hdl.handle.net/2027/uiug.30112018287869.  , 1987
Link: http://hdl.handle.net/20..
 
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14

IMAGES : a digital computer program for interactive modal a..:

Jones, Ruben L ; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
http://hdl.handle.net/2027/uiug.30112106569897.  , 1984
Link: http://hdl.handle.net/20..
 
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15

Static and dynamic structural-sensitivity derivative calcul..:

Camarda, Charles J., 1952- ; Adelman, Howard M ; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
http://hdl.handle.net/2027/uiug.30112106569988.  , 1984
Link: http://hdl.handle.net/20..
 
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