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Tethered Satellite System-2 - A proposed programA second mission (TSS-2) has been proposed for the reusable Tethered Satellite System (TSS) being developed jointly by the U.S. and Italy. The TSS-2 flight demonstration would use the TSS deployer/retriever system to deploy a research spacecraft attached to the end of a 100-km-long tether. The deployment would take place downward from the Space Shuttle into the outer atmosphere to an altitude of approximately 130 km. The objectives of the mission would be to demonstrate the atmospheric deployment of a tethered system, conduct scientific and aerothermodynamic research measurements, and conduct engineering measurements to verify flight system performance. Analytical studies have shown the feasibility of the TSS-2 mission from both the technology and operational dynamics standpoint. The TSS-1 mission (a 20 km tether deployed upward to conduct electrodynamic experiments) will validate the TSS itself as well as deployment and retrieval operations.
Document ID
19890052820
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Anderson, John L.
(NASA Headquarters Washington, DC United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Astronautics (General)
Report/Patent Number
AIAA PAPER 89-1561
Meeting Information
Meeting: International Conference on Tethers in Space - Toward Flight
Location: San Francisco, CA
Country: United States
Start Date: May 17, 1989
End Date: May 19, 1989
Accession Number
89A40191
Distribution Limits
Public
Copyright
Other

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