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An assessment of variable geometry spacecraft performance potential.Variable geometry features applied to lifting spacecraft to overcome inherent incompatibility and provide low speed and tangential landing capabilities
Document ID
19690035573
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Coward, K. S.
Henry, B. Z.
Date Acquired
August 5, 2013
Publication Date
December 1, 1968
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS.
Subject Category
Space Vehicles
Report/Patent Number
AIAA PAPER 68-1164
Report Number: AIAA PAPER 68-1164
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, ENTRY VEHICLE SYSTEMS AND TECHNOLOGY MEETING
Location: WILLIAMSBURG, VA
Start Date: December 3, 1968
End Date: December 5, 1968
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
69A13562
Distribution Limits
Public
Copyright
Other

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