NASA SBIR 2018-II Solicitation

Proposal Summary


PROPOSAL NUMBER:
 18-2- S1.08-4652
PHASE 1 CONTRACT NUMBER:
 80NSSC18P2042
SUBTOPIC TITLE:
 In-situ Sensors and Sensor Systems for Earth Science
PROPOSAL TITLE:
 An Airborne Continuous Flow Diffusion Chamber for Measuring Ice Nucleating Particles
SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Handix Scientific, LLC
5485 Conestoga Court, Suite 104B
Boulder, CO 80301
(720) 724-7658

PRINCIPAL INVESTIGATOR (Name, E-mail, Mail Address, City/State/Zip, Phone)
Gavin McMeeking
gavin@handixscientific.com
5485 Conestoga Court, Suite 104B
Boulder, CO 80301 - 2981
(970) 310-5186

BUSINESS OFFICIAL (Name, E-mail, Mail Address, City/State/Zip, Phone)
Gavin McMeeking
gavin@handixscientific.com
5485 Conestoga Court, Suite 104B
Boulder, CO 80301 - 2981
(970) 310-5186

Estimated Technology Readiness Level (TRL) :
Begin: 4
End: 7
Technical Abstract (Limit 2000 characters, approximately 200 words)

Quantifying atmospheric aerosol, clouds and precipitation processes are critical needs for understanding climate and environmental change, a NASA objective. The formation of ice in the atmosphere depends on the nature and abundance of ice nucleating particles (INP), and has major implications for precipitation and cloud properties. Observational capabilities are required to advance understanding of INP, and there is a substantial gap between current needs within NASA and existing instruments and capabilities. This project seeks to develop a new commercial instrument for airborne INP measurements based on the continuous flow diffusion chamber (CFDC) concept. The CFDC approach involves exposing sampled aerosol to a region between two ice-covered walls and measuring ice crystals that form from sampled INP. Phase I work assessed a measurement chamber made from anodized aluminum and found it was suitable for INP measurements. Phase II will build on this work by completing a prototype instrument featuring an aluminum-walled chamber. Research and development efforts will include testing and design of a new inlet system to reduce sampling artifacts, incorporation of a new refrigeration system for use on aircraft, and implementation of several automation features into the overall instrument design. The prototype instrument will be thoroughly tested using aerosol standards, including previously characterized INP, and compared with state-of-the-art measurement methods available from our project partner, Colorado State University. At the end of the project we will provide NASA with a characterized, prototype instrument capable of INP measurements aboard the NASA aircraft fleet. The project directly addresses the NASA need for measurement capabilities to support current satellite and model validation by providing an instrument capable of measuring INP concentration in an airborne deployment, as identified in subtopic S1.08, In Situ Sensors and Sensor Systems for Earth Science.

Potential NASA Applications (Limit 1500 characters, approximately 150 words)

By supporting this project, NASA would obtain airborne INP measurement capabilities that would support model validation and airborne science program field campaigns, similar to those discussed in the ROSES-2018 solicitation. Suitable platforms include the DC-8, P-3, C-20A and G-V. Relevant campaigns include any that include a focus on aerosol-cloud interactions, similar to FIREChem, NAAMES, ORACLES, ARISE II, and CAMP2Ex, and future EVS studies examining aerosol-cloud interactions.

Potential Non-NASA Applications (Limit 1500 characters, approximately 150 words)

Domestically, agencies with an interest in measuring INP from aircraft include the Department of Energy ASR/ARM, NOAA CSD, and NSF/NCAR atmospheric chemistry programs. Foreign government organizations include the UK MetOffice (BAe-146) and German DLR (G-V). We also see potential for significant interest from the atmospheric research and weather modification community in Asia.

Duration: 24

Form Generated on 05/13/2019 13:33:05