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Spaceborne CO2 laser communications systemsProjections of the growth of earth-sensing systems for the latter half of the 1980's show a data transmission requirement of 300 Mbps and above. Mission constraints and objectives lead to the conclusion that the most efficient technique to return the data from the sensing satellite to a ground station is through a geosynchronous data relay satellite. Of the two links that are involved (sensing satellite to relay satellite and relay satellite to ground), a laser system is most attractive for the space-to-space link. The development of CO2 laser systems for space-to-space applications is discussed with the completion of a 300 Mpbs data relay receiver and its modification into a transceiver. The technology and state-of-the-art of such systems are described in detail.
Document ID
19750022469
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mcelroy, J. H.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Mcavoy, N.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Johnson, E. H.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Goodwin, F. E.
(Hughes Aircraft Co.)
Peyton, B. J.
(Airborne Instr. Lab.)
Date Acquired
September 3, 2013
Publication Date
July 1, 1975
Subject Category
Lasers And Masers
Report/Patent Number
X-723-75-171
NASA-TM-X-70947
Report Number: X-723-75-171
Report Number: NASA-TM-X-70947
Accession Number
75N30542
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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