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Shuttle derived launch vehicle wind tunnel testsStudies are being conducted regarding new launch vehicle configurations which may effectively and economically share the delivery of payloads to orbit with the present Space Transportation System (STS). The role envisaged for these launch vehicles is related to the execution of missions whose requirements exceed the STS Shuttle capabilities, taking into account the delivery of much heavier or larger payloads. One class of advanced launch vehicles is configured to take advantage of the existing Shuttle hardware and facilities. Such vehicles are referred to as Shuttle Derived Vehicles (SDV). One version of an SDV consists of two STS elements, including the external tank (ET) and solid rocket boosters, and a cargo carrier. Attention is given to wind tunnel tests, which are being conducted with SDV sidemount configurations incorporating various size payload modules.
Document ID
19860026331
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tewell, J. R.
(Martin Marietta Aerospace New Orleans, LA, United States)
Buell, D. N.
(Martin Marietta Aerospace New Orleans, LA, United States)
Date Acquired
August 12, 2013
Publication Date
October 1, 1985
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 85-5021
Accession Number
86A11069
Funding Number(s)
CONTRACT_GRANT: NAS8-34183
Distribution Limits
Public
Copyright
Other

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