Item Details

The Effect of Finite Thrust and Heating Constraints on the Synergetic Plane Change Maneuver for a Space Shuttle Orbiter-Class Vehicle

by E.D. Dickmanns
Format
Book; Government Document; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by National Technical Information Service], 1973.
Language
English
Series
NASA Technical Note
Description
vii, 38 p. : ill. ; 27 cm.
Mode of access: Internet.
Notes
  • Prepared at George C. Marshall Space Flight Center.
  • Cover title.
  • Bibliography: p. 37-38.
Series Statement
NASA technical note ; NASA TN D-7211
Logo for Copyright Not EvaluatedCopyright Not Evaluated
Technical Details

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    a| The effect of finite thrust and heating constraints on the synergetic plane change maneuver for a space shuttle orbiter-class vehicle / c| by E.D. Dickmanns.
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    a| Washington, D.C. : b| National Aeronautics and Space Administration ; a| [Springfield, Va. : b| For sale by National Technical Information Service], c| 1973.
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    a| Prepared at George C. Marshall Space Flight Center.
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    a| Bibliography: p. 37-38.
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    a| Space vehicles x| Atmospheric entry.
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    a| Space shuttles x| Trajectories x| Computer simulation.
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    a| Orbital transfer (Space flight) x| Computer simulation.
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