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Aerodynamic enhancement of space transportation systemsThe results of a number of recent investigations are reviewed and used to demonstrate gains in launch, orbital transfer, and planetary vehicle performance and economy that can result from the proper exploitation of aerodynamic phenomena. For launch vehicles, application of control-configured design is shown to allow substantial reduction in wing and vertical fin area (and hence, weight) while maintaining acceptable vehicle performance and control. For orbital transfer and planetary vehicles, the use of aerodynamic lift and drag to reduce retropropulsion requirements is shown to produce payload increases of up to 100 percent and to enable some planetary missions that are not feasible with all-propulsive vehicles. Finally, the application of various advanced technologies to a complete set of launch and orbit transfer vehicles in an early space industrialization mission scenario is considered.
Document ID
19810062879
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Walberg, G. D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 11, 2013
Publication Date
September 1, 1981
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
IAF PAPER 81-3
Accession Number
81A47283
Distribution Limits
Public
Copyright
Other

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