Paper
1 March 2006 Mars laser communication demonstration: what it would have been
A. Biswas, D. Boroson, B. Edwards
Author Affiliations +
Abstract
The Mars Laser Communications Demonstration Project completed a preliminary system design for sending data at 1-30 Mbps from a spacecraft orbiting Mars. The flight transceiver diameter was 30.6 cm, transmitting 5 W average laser power at 1064 nm and using 32- and 64-ary pulse position modulation (PPM). A ground network comprised of two receive terminals (5-m and 1.6-m effective diameter) and two transmit terminals for sending 1076 nm lasers would have been used to communicate with the transceiver.
© (2006) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
A. Biswas, D. Boroson, and B. Edwards "Mars laser communication demonstration: what it would have been", Proc. SPIE 6105, Free-Space Laser Communication Technologies XVIII, 610502 (1 March 2006); https://doi.org/10.1117/12.669551
Lens.org Logo
CITATIONS
Cited by 24 scholarly publications.
Advertisement
Advertisement
RIGHTS & PERMISSIONS
Get copyright permission  Get copyright permission on Copyright Marketplace
KEYWORDS
Telescopes

Mars

Sensors

Space telescopes

Receivers

Laser communications

Molybdenum

RELATED CONTENT

The Lunar Laser OCTL Terminal (LLOT)
Proceedings of SPIE (March 19 2013)
LLCD operations using the Lunar Lasercom Ground Terminal
Proceedings of SPIE (March 06 2014)
Low cost Earth attitude sensor
Proceedings of SPIE (November 21 2017)
Deep-space optical terminals (DOT)
Proceedings of SPIE (March 01 2011)

Back to Top