Effect of aerodynamic and angle-of-attack uncertainties on the blended entry flight control system of the space shuttle from Mach 10 to 2.5
Resource Information
The work Effect of aerodynamic and angle-of-attack uncertainties on the blended entry flight control system of the space shuttle from Mach 10 to 2.5 represents a distinct intellectual or artistic creation found in Indiana State Library. This resource is a combination of several types including: Work, Language Material, Books.
The Resource
Effect of aerodynamic and angle-of-attack uncertainties on the blended entry flight control system of the space shuttle from Mach 10 to 2.5
Resource Information
The work Effect of aerodynamic and angle-of-attack uncertainties on the blended entry flight control system of the space shuttle from Mach 10 to 2.5 represents a distinct intellectual or artistic creation found in Indiana State Library. This resource is a combination of several types including: Work, Language Material, Books.
- Label
- Effect of aerodynamic and angle-of-attack uncertainties on the blended entry flight control system of the space shuttle from Mach 10 to 2.5
- Statement of responsibility
- Howard W. Stone and Richard W. Powell
- Language
- eng
- Cataloging source
- GPO
- Government publication
- federal national government publication
- Illustrations
- illustrations
- Index
- no index present
- Literary form
- non fiction
- Nature of contents
-
- technical reports
- bibliography
- Series statement
- NASA technical paper
- Series volume
- 2283
Context
Context of Effect of aerodynamic and angle-of-attack uncertainties on the blended entry flight control system of the space shuttle from Mach 10 to 2.5Work of
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.library.in.gov/resource/9YGEAExYBfk/" typeof="CreativeWork http://bibfra.me/vocab/lite/Work"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.in.gov/resource/9YGEAExYBfk/">Effect of aerodynamic and angle-of-attack uncertainties on the blended entry flight control system of the space shuttle from Mach 10 to 2.5</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.in.gov/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.in.gov/">Indiana State Library</a></span></span></span></span></div>
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.library.in.gov/resource/9YGEAExYBfk/" typeof="CreativeWork http://bibfra.me/vocab/lite/Work"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.in.gov/resource/9YGEAExYBfk/">Effect of aerodynamic and angle-of-attack uncertainties on the blended entry flight control system of the space shuttle from Mach 10 to 2.5</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.in.gov/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.in.gov/">Indiana State Library</a></span></span></span></span></div>
