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, Howard W. Stone and Richard W. Powell
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, Howard W. Stone and Richard W. Powell
Resource Information
The item 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, Howard W. Stone and Richard W. Powell represents a specific, individual, material embodiment of a distinct intellectual or artistic creation found in Indiana State Library.This item is available to borrow from 1 library branch.
Resource Information
The item 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, Howard W. Stone and Richard W. Powell represents a specific, individual, material embodiment of a distinct intellectual or artistic creation found in Indiana State Library.
This item is available to borrow from 1 library branch.
- Language
- eng
- Extent
- iii, 287 pages
- Note
-
- Distributed to depository libraries in microfiche
- "April 1984"--Cover
- Subject category 08
- 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
- Title
- 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
- http://library.link/vocab/creatorName
- Stone, Howard W
- Government publication
- federal national government publication
- Illustrations
- illustrations
- Index
- no index present
- Literary form
- non fiction
- Nature of contents
-
- technical reports
- bibliography
- http://library.link/vocab/relatedWorkOrContributorName
-
- Powell, Richard W
- United States
- Series statement
- NASA technical paper
- Series volume
- 2283
- http://library.link/vocab/subjectName
-
- Space vehicles
- Space vehicles
- Space shuttles
- 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, Howard W. Stone and Richard W. Powell
- Note
-
- Distributed to depository libraries in microfiche
- "April 1984"--Cover
- Subject category 08
- Bibliography note
- Includes bibliographical references
- Carrier category
- volume
- Carrier category code
- nc
- Carrier MARC source
- rdacarrier
- Content category
- text
- Content type code
- txt
- Content type MARC source
- rdacontent
- Control code
- 17085788
- Dimensions
- 28 cm.
- Extent
- iii, 287 pages
- Media category
- unmediated
- Media MARC source
- rdamedia
- Media type code
- n
- Other physical details
- illustrations
- 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, Howard W. Stone and Richard W. Powell
- Note
-
- Distributed to depository libraries in microfiche
- "April 1984"--Cover
- Subject category 08
- Bibliography note
- Includes bibliographical references
- Carrier category
- volume
- Carrier category code
- nc
- Carrier MARC source
- rdacarrier
- Content category
- text
- Content type code
- txt
- Content type MARC source
- rdacontent
- Control code
- 17085788
- Dimensions
- 28 cm.
- Extent
- iii, 287 pages
- Media category
- unmediated
- Media MARC source
- rdamedia
- Media type code
- n
- Other physical details
- illustrations
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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/portal/Effect-of-aerodynamic-and-angle-of-attack/uCWjGgGD9-Q/" typeof="Book http://bibfra.me/vocab/lite/Item"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.in.gov/portal/Effect-of-aerodynamic-and-angle-of-attack/uCWjGgGD9-Q/">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, Howard W. Stone and Richard W. Powell</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/portal/Effect-of-aerodynamic-and-angle-of-attack/uCWjGgGD9-Q/" typeof="Book http://bibfra.me/vocab/lite/Item"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.in.gov/portal/Effect-of-aerodynamic-and-angle-of-attack/uCWjGgGD9-Q/">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, Howard W. Stone and Richard W. Powell</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>
