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Parameter optimization and the space shuttleDesign parameter optimization for two-stage space shuttle atmospheric flight from spherical nonrotating earth by sequential straight line approximation
Document ID
19710063418
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Johnson, I. L.
Kamm, J. L.
Date Acquired
August 6, 2013
Publication Date
January 1, 1971
Publication Information
Publisher: INST. OF ELECTRICAL AND ELECTRONICS ENGINEERS, INC.,
Subject Category
Space Vehicles
Meeting Information
Meeting: JOINT AUTOMATIC CONTROL CONFERENCE
Location: ST. LOUIS, MO
Start Date: August 11, 1971
End Date: August 13, 1971
Accession Number
71A44115
Distribution Limits
Public
Copyright
Other

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