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Utilization of Space Station by the Large Deployment ReflectorThe Large Deployable Reflector (LDR), a NASA concept of a very large, orbiting, far infrared submillimeter telescope is described. To be launched in the 1990s, LDR has a projected life of 10 years and is to be serviced every 2 to 3 years. A System Concept and Technology Definition Study of LDR for NASA Ames is currently being conducted. Study results indicate that launch of a 20 m LDR, operating in a 700 to 800 km orbit, requires two shuttle loads. The components of LDR are assembled in a lower parking orbit, and the system is checked out and then transferred to the operational orbit. Furthermore, for servicing, LDR may have to be retrieved to the same lower orbit (and later returned to operational altitude) by an orbit transfer vehicle. These requirements bring up the question of a suitable assembly, checkout, and servicing platform. The deployment process is time consuming and may require special equipment not necessarily available from the orbiter itself. The SS is an attractive choice for that platform.
Document ID
19850015546
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bandermann, L. W.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Alff, W. H.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Date Acquired
August 12, 2013
Publication Date
April 1, 1985
Publication Information
Publication: NASA. Langley Research Center Large Space Antenna Systems Technol., 1984, Pt. 2
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
85N23857
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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