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Shuttle tethered satellite programFeatures and applications of the Shuttle tethered satellite system (TSS) are outlined. The TSS would be mounted on a normal cargo pallet and used to deploy or retrieve payloads weighing up to 500 kg from the Orbiter by reeling in or unreeling a tether line extended along the gravity gradient vertical. Attaching a conducting wire to the tether would permit electrodynamic measurements of space plasma. An initial mission under development is to deploy an instruments package 20 km above the Orbiter with a conducting wire tether, thereby obtaining data on low frequency hydromagnetic waves generated by tether passage through the space plasma. An aerodynamics package could also be lowered to 130 km, where measurements can be made with magnetometers for geoscience data, atmospheric composition, and cosmic dust can be collected. Details of engineering assignments for the TSS divided up between NASA and the Italian National Research Council are discussed.
Document ID
19850031126
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Nolan, M. B.
(NASA Headquarters Washington, DC United States)
Hudson, R.
(NASA Headquarters Washington, DC United States)
Sisson, J. M.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Crouch, D. S.
(Martin Marietta Aerospace Denver, CO, United States)
Vignoli, M.
(Aeritalia S.p.A. Naples, Italy)
Date Acquired
August 12, 2013
Publication Date
October 1, 1984
Subject Category
Space Transportation
Report/Patent Number
IAF PAPER 84-437
Report Number: IAF PAPER 84-437
Accession Number
85A13277
Distribution Limits
Public
Copyright
Other

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