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Skylab is falling - Strategies for reentryPlanning for the Skylab reentry, options for influencing the reentry, and a discussion of the Penn State drag modulation scheme are presented. The history of and risks in connection with Skylab reentry, and the NASA and the Penn State schemes for extending Skylab life are discussed. Coordinate systems and equations of motions describing the Skylab attitude motion, aerodynamic damping, and six-degree-of-freedom simulation are considered to derive structural damping models for Skylab, and to determine if stabilization is possible, and if it is, if the TACS (attitude-control) system can retumble the vehicle. It is concluded that at least 12 hours are required to carry out the Penn State drag modulation, and natural stabilization after a period of tumbling is possible but cannot be confirmed due to limitations in the modeling of aerodynamic properties, internal damping, and atmospheric density.
Document ID
19790063233
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kaplan, M. H.
(Pennsylvania State Univ. University Park, PA, United States)
Alexander, S. G.
(Pennsylvania State University University Park, Pa., United States)
Date Acquired
August 9, 2013
Publication Date
June 1, 1979
Subject Category
Astrodynamics
Report/Patent Number
AAS PAPER 79-170
Report Number: AAS PAPER 79-170
Meeting Information
Meeting: American Astronautical Society and American Institute of Aeronautics and Astronautics, Astrodynamics Specialist Conference
Location: Provincetown, MA
Start Date: June 25, 1979
End Date: June 27, 1979
Sponsors: American Astronautical Society, American Institute of Aeronautics and Astronautics
Accession Number
79A47246
Funding Number(s)
CONTRACT_GRANT: NASW-3256
Distribution Limits
Public
Copyright
Other

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