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

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
Creator
Contributor
Subject
Language
eng
Member of
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
Instantiates
Publication
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
Publication
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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