NASA SBIR 2016 Solicitation

FORM B - PROPOSAL SUMMARY


PROPOSAL NUMBER: 16-2 S1.01-8414
PHASE 1 CONTRACT NUMBER: NNX16CL58P
SUBTOPIC TITLE: Lidar Remote Sensing Technologies
PROPOSAL TITLE: Spaceflight 1.94 Micron Tm Fiber Laser Transmitter

SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Fibertek, Inc.
13605 Dulles Technology Drive
Herndon, VA 20171 - 4603
(703) 471-7671

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Dr. Doruk Engin
dengin@fibertek.com
13605 Dulles Technology Drive
Herndon, VA 20171 - 4603
(703) 471-7671

CORPORATE/BUSINESS OFFICIAL (Name, E-mail, Mail Address, City/State/Zip, Phone)
Ms. Tracy Perinis
tperinis@fibertek.com
13605 Dulles Technology Drive
Herndon, VA 20171 - 4603
(703) 471-7671

Estimated Technology Readiness Level (TRL) at beginning and end of contract:
Begin: 4
End: 6

Technology Available (TAV) Subtopics
Lidar Remote Sensing Technologies 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)
Fibertek will develop a spaceflight prototype 1940 nm, 100 W thulium (Tm) laser suitable for NASA spaceflight and long-duration unmanned aerial vehicle (UAV) missions. The proposal is innovative because it demonstrates 100 W of polarization maintaining (PM) performance at 1940 nm. We expect a 2x to 3x improvement in efficiency compared to available commercial off-the-shelf (COTS) unpolarized Tm fiber lasers, and the laser will be packaged for high reliability for spaceflight operation. This SBIR leverages commercial Tm laser technology, published scientific test data, available optical components, and Fibertek's validated Tm fiber laser model. A spaceflight 100 W PM Tm laser is enabling and provides a path to space for a pulsed, Q-switched 2 um Ho:YLF laser with up to 80 mJ/pulse at 100-200 Hz. Lidar performance design studies from a low earth orbit (LEO) satellite indicate that 80 mJ of pulsed 2 um energy enables the simultaneous measurements of CO2 and water vapor using Integrated Path Differential Absorption (IPDA) and global wind light detection and ranging (lidar). NASA laser experiments have shown the 100 W of 1940 nm peak pump power is needed to generate 80 mJ/pulse.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
Satellite, ISS, UAS, Aircraft-Based Carbon Dioxide, Water Vapor, and Methane Lidar Coherent Lidar, Clouds, and 3D Wind Lidar

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
Coherent lidar for wind or hard-target velocity detection Infrared countermeasures (IRCM) DoD market Coherent 3D imaging lidar

TECHNOLOGY TAXONOMY MAPPING (NASA's technology taxonomy has been developed by the SBIR-STTR program to disseminate awareness of proposed and awarded R/R&D in the agency. It is a listing of over 100 technologies, sorted into broad categories, of interest to NASA.)
Entry, Descent, & Landing (see also Astronautics)
Entry, Descent, & Landing (see also Planetary Navigation, Tracking, & Telemetry)
Fiber (see also Communications, Networking & Signal Transport; Photonics)
Gratings
Infrared
Lasers (Ladar/Lidar)
Lasers (Measuring/Sensing)
Optical
Optical/Photonic (see also Photonics)
Ranging/Tracking

Form Generated on 03-07-17 15:43