NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Geostationary earth science platform conceptsThe new concepts are presented for the Geostationary Earth Science Platform. Bus and payload arrangements, with instrument locations on the payload module and basic payload dimensions, are depicted and compared for each concept. The Titan 4 SRMU (with solid rocket motor upgrage) launch vehicle is described and compared to the standard Titan 4. The upgraded Titan 4 is capable of launching a 13,500 lb payload to GEO. The launch configuration showing each concept packaged within the 16 ft diameter payload envelope is presented. This presentation is represented by viewgraph only.
Document ID
19900009936
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Herardian, M. M.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1989
Publication Information
Publication: NASA, Langley Research Center, Earth Science Geostationary Platform Technology
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
90N19252
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available