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The Space Station Freedom microgravity environmentThe SSF microgravity environment is discussed focusing on requirements derived from initial specifications proposed by the NASA Office of Space Science and Applications and on microgravity assessment methods including quasi-steady, structural dynamic, and vibroacoustic methods. Preliminary results indicate that the flight dynamics of the vehicle meet the requirements for both scientific and engineering communities, but that a number of vibroacoustic disturbance sources violate the criteria. The assessment updates along with planned on-orbit acceleration measurements and crew disturbance characterizations are being carried out to clearly define and understand the acceleration environment.
Document ID
19930040904
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Del Basso, Steve
(Grumman Corp. Space Station Integration Div., Reston, VA, United States)
Bogert, Philip B.
(NASA Space Station Freedom Program Office Reston, VA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Subject Category
Astronautics (General)
Report/Patent Number
AIAA PAPER 93-0831
Meeting Information
Meeting: AIAA, Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 11, 1993
End Date: January 14, 1993
Sponsors: AIAA
Accession Number
93A24901
Distribution Limits
Public
Copyright
Other

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