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Design and analysis study of a spacecraft optical transceiver packageA detailed system level design of an Optical Transceiver Package (OPTRANSPAC) for a deep space vehicle whose mission is outer planet exploration is developed. In addition to the terminal design, this study provides estimates of the dynamic environments to be encountered by the transceiver throughout its mission life. Optical communication link analysis, optical thin lens design, electronic functional design and mechanical layout and packaging are employed in the terminal design. Results of the study describe an Optical Transceiver Package capable of communicating to an Earth Orbiting Relay Station at a distance of 10 Astronomical Units (AU) and data rates up to 100 KBPS. The transceiver is also capable of receiving 1 KBPS of command data from the Earth Relay. The physical dimensions of the terminal are contained within a 3.5' x 1.5' x 2.0' envelope and the transceiver weight and power are estimated at 52.2 Kg (115 pounds) and 57 watts, respectively.
Document ID
19870004044
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lambert, S. G.
(McDonnell-Douglas Astronautics Co. Saint Louis, MO, United States)
Date Acquired
September 5, 2013
Publication Date
August 19, 1985
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
JPL-9950-1240
NASA-CR-179958
NAS 1.26:179958
Report Number: JPL-9950-1240
Report Number: NASA-CR-179958
Report Number: NAS 1.26:179958
Accession Number
87N13477
Funding Number(s)
CONTRACT_GRANT: JPL-957061
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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