Paper
6 August 1993 LITE engineering model-II: the flight-qualified subsystems
Allen D. Pillsbury
Author Affiliations +
Proceedings Volume 1866, Free-Space Laser Communication Technologies V; (1993) https://doi.org/10.1117/12.149256
Event: OE/LASE'93: Optics, Electro-Optics, and Laser Applications in Scienceand Engineering, 1993, Los Angeles, CA, United States
Abstract
A space-based optical communications system requires the development of high-precision yet rugged electro-optical hardware. Lincoln Laboratory has built and assembled an engineering model of a high-data-rate heterodyne laser communication satellite crosslink to demonstrate the fabrication, integration, and test methods required of an actual flight system. A description of the hardware that has been developed and the testing program to which it has been subjected is presented.
© (1993) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Allen D. Pillsbury "LITE engineering model-II: the flight-qualified subsystems", Proc. SPIE 1866, Free-Space Laser Communication Technologies V, (6 August 1993); https://doi.org/10.1117/12.149256
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CITATIONS
Cited by 3 scholarly publications.
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KEYWORDS
Mirrors

Sensors

Servomechanisms

Transmitters

Optical fabrication

Diagnostics

Electro optical modeling

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