SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
AOSense, Inc.
929 East Arques Avenue
Sunnyvale, CA 94085 - 4521
(408) 735-9500

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Arman Cingoz
acingoz@aosense.com
929 East Arques Avenue
Sunnyvale, CA 94085 - 4521
(408) 636-2612

CORPORATE/BUSINESS OFFICIAL (Name, E-mail, Mail Address, City/State/Zip, Phone)
Jason Burke
jburke@aosense.com
929 East Arques Avenue
Sunnyvale, CA 94085 - 4521
(408) 636-2643

Estimated Technology Readiness Level (TRL) at beginning and end of contract:
Begin: 4
End: 5

Technology Available (TAV) Subtopics
Flight Dynamics and Navigation Systems is a Technology Available (TAV) subtopic that includes NASA Intellectual Property (IP). Do you plan to use the NASA IP under the award?
No

TECHNICAL ABSTRACT (Limit 2000 characters, approximately 200 words)
AOSense proposes a free-space, two-way optical time transfer system compatible with global-scale synchronization of current-generation optical atomic clocks. In Phase I, we have demonstrated the requisite performance using existing hardware coupled with off-the-shelf control electronics. Based on our results, we have designed a fully-integrated module capable of disseminating timing signals with sub-femtosecond error from 1-10,000 s. In Phase II, we will package the device and deliver it for external testing. Our system is expected to improve ground-to-satellite synchronization a million-fold over current RF-based time transfer systems, enabling applications including clock-based geodesy, very long baseline interferometry, coherent LIDAR arrays, and tests of general relativity.
The Phase I breadboard demonstration performance is consistent with a timing jitter of 3 fs @ 1s and integrates down to 700 as at 30 seconds. The corresponding fractional timing instability is 3 x 10^-15 @ 1 second, which flickers at 2.7 x 10^-17 out to 2000 seconds. We have identified the systematic effects that limit both short and long term stability and incorporated the improvements into the Phase II design. With these improvements, we expect a 10x improvement in both short and long terms stability of the system.
In addition, we reviewed and formalized the laser driver and control electronics specifications. The initial schematic capture for critical analog sub sections was completed and a suitable FPGA/microprocessor combination was chosen to control the system and process the timing information. Based on these designs, power and size estimates were used to complete the mechanical enclosure model for the time-transfer system. For maximum flexibility in the final architecture of the overall free-space time transfer system, each frequency comb sub-unit that includes the laser and control electronics will be housed in a 1U rack mount enclosure.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
Optical atomic clocks; clock based geodesy; very long baseline interferometry; test of general relativity; deep-space navigation; coherent LIDAR

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
Ultra low-phase noise microwave generation; High resolution coherent radar; communication systems insensitive to jamming; extended mission duration in GPS-denied environments