The Resource Static aerodynamic characteristics of a single-stage-to-orbit vehicle with low planform loading at Mach numbers from 0.3 to 4.63, Delma C. Freemand, Jr. and Roger H. Fournier

Static aerodynamic characteristics of a single-stage-to-orbit vehicle with low planform loading at Mach numbers from 0.3 to 4.63, Delma C. Freemand, Jr. and Roger H. Fournier

Label
Static aerodynamic characteristics of a single-stage-to-orbit vehicle with low planform loading at Mach numbers from 0.3 to 4.63
Title
Static aerodynamic characteristics of a single-stage-to-orbit vehicle with low planform loading at Mach numbers from 0.3 to 4.63
Statement of responsibility
Delma C. Freemand, Jr. and Roger H. Fournier
Creator
Contributor
Joint author
Subject
Language
eng
http://library.link/vocab/creatorName
Freeman, Delma C
Government publication
federal national government publication
Illustrations
illustrations
Index
no index present
Literary form
non fiction
Nature of contents
bibliography
http://library.link/vocab/relatedWorkOrContributorName
  • Fournier, Roger H.
  • United States
Series statement
NASA technical memorandum ; 74056
http://library.link/vocab/subjectName
Stability of space vehicles
Label
Static aerodynamic characteristics of a single-stage-to-orbit vehicle with low planform loading at Mach numbers from 0.3 to 4.63, Delma C. Freemand, Jr. and Roger H. Fournier
Instantiates
Publication
Note
Issued Nov. 1977
Bibliography note
Includes bibliographical references
Control code
16971445
Dimensions
27 cm.
Extent
66 p.
Other physical details
ill.
Label
Static aerodynamic characteristics of a single-stage-to-orbit vehicle with low planform loading at Mach numbers from 0.3 to 4.63, Delma C. Freemand, Jr. and Roger H. Fournier
Publication
Note
Issued Nov. 1977
Bibliography note
Includes bibliographical references
Control code
16971445
Dimensions
27 cm.
Extent
66 p.
Other physical details
ill.

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      39.77004 -86.164015

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