3.8 Proceedings Paper

Optical Modem Enabling Broadband Datacom Links for Crewed Cis-Lunar Missions

Journal

FREE-SPACE LASER COMMUNICATIONS XXXIV
Volume 11993, Issue -, Pages -

Publisher

SPIE-INT SOC OPTICAL ENGINEERING
DOI: 10.1117/12.2613748

Keywords

laser communication; space qualification; fiber laser; pulse position modulation; erbium/ytterbium; deep-space communications; optical modem; free-space optical communications

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This article reports on the design, development, and testing of a high-power broadband optical modem for NASA's crewed Artemis-2 mission. The modem, known as O2O, provides a bi-directional optical link back to earth while en route to the moon. It features a full-duplex design with a high-power optical transmitter and receiver optimized for serially-concatenated pulse-position modulation (SCPPM). The modem has passed rigorous environmental testing and has been declared at Technology Readiness Level (TRL) 6.
We report on the design, development, and testing of our high-power broadband optical modem supporting NASA's crewed Artemis- 2 mission. The O2O modem will be mounted in the crewed Orion module and provide a broadband 505,000 km bi-directional optical link back to earth while en route to the moon. The full-duplex modem consists of a high-power optical transmitter and receiver optimized for serially-concatenated pulse-position modulation (SCPPM). The transmitter is a master-oscillator power-amplifier optical architecture using efficient cladding-pumped amplification in erbium-ytterbium co-doped fiber. The transmitter outputs up to 1 W at approximate to 1550 nm (limited for eye safety) and supports 6 different user-rates ranging from 20.39 Mb/s to 260.95 Mb/s using PPM16 and PPM32 modulation formats. The optical receiver supports two user-rates: 10.19 Mb/s and 20.39 Mb/s with both rates employing PPM32. The narrowband receiver filtering is optimized to simultaneously accept four separate wavelength channels to mitigate atmospherics through spatial diversity. A configurable interleaver provides additional protection against atmospherics-based signal fading and a powerful soft-decision error correction scheme enables highly sensitive detection. The measured sensitivities at the two bit-rates are - 73.8 and -71.8 dBm, respectively. The architecture was designed for reliable operation in space, featuring automatic hardware interlocks, pump sparing for the amplifiers, and autonomous operation of all internal hardware and software control loops. The protoflight unit (PFU) was put through rigorous environmental testing which included pyroshock, vibration, electromagnetic interference/compatibility, and thermal-vacuum testing. The modem successfully passed all the environmental screening and has been declared at Technology Readiness Level (TRL) 6.

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