NASA SBIR 2015 Solicitation

FORM B - PROPOSAL SUMMARY


PROPOSAL NUMBER: 15-2 H7.02-9691
PHASE 1 CONTRACT NUMBER: NNX15CA32P
SUBTOPIC TITLE: Diagnostic Tools for High Velocity Testing & Analysis
PROPOSAL TITLE: Short Pulsed Laser Methods for Velocimetry and Thermometry in High Enthalpy Facilities

SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
MetroLaser, Inc.
22941 Mill Creek Drive
Laguna Hills, CA 92653 - 1215
(949) 553-0688

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Jacob George
jageorge@metrolaserinc.com
22941 Mill Creek Drive
Laguna Hills, CA 92653 - 1215
(949) 553-0688 Extension :222

CORPORATE/BUSINESS OFFICIAL (Name, E-mail, Mail Address, City/State/Zip, Phone)
Christina L Arnold
carnold@metrolaserinc.com
22941 Mill Creek Drive
Laguna Hills, CA 92653 - 1215
(949) 553-0688 Extension :241

Estimated Technology Readiness Level (TRL) at beginning and end of contract:
Begin: 2
End: 6

Technology Available (TAV) Subtopics
Diagnostic Tools for High Velocity Testing & Analysis 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)
A suite of pulsed laser diagnostics is proposed for studying aspects of planetary entry and Earth atmospheric reentry in arc jets. For example, dissociation of molecules impacts the flow-field physics, including surface heat flux and catalytic surface reactions. Results obtained during the Phase I effort point to three promising diagnostic techniques: Rayleigh Scattering Polarimetry (RSP) for dissociation fraction, Thermal Acoustic Wave (TAW) thermometry for gas temperature, and Radar Resonance Enhanced Multi-photon Ionization (Radar REMPI) for gas temperature and velocity. The RSP technique is based on the differences in the polarization of Rayleigh-scattered light between atoms and molecules. The TAW technique is based on the determination of wave speed from the propagation of an acoustic wave generated by a laser spark from the focused beam of a pulsed laser. In the case of Radar REMPI, temperature and velocity are obtained through the spectral broadening and frequency shift associated with two-photon resonance interactions in atomic oxygen and nitrogen.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
The proposed diagnostics are needed in test programs for atmospheric reentry and planetary entry at NASA's arc jet facilities, hypersonic wind tunnels, and shock tunnels. Non-intrusive unseeded measurements of temperature, velocity, and dissociation are required for validating fluid/chemistry models that incorporate real-gas kinetics, including those used to predict planetary entry aerothermodynamics. The diagnostics can serve as tools in very high enthalpy flow experiments that focus on testing the integrity of thermal protection systems.

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
The unique capability to measure temperature, velocity, and dissociation fraction in high enthalpy flows will be attractive to the private space industry, including low Earth orbit and planetary exploration. Programs include delivery of cargo and astronauts to the ISS, and deep space exploration, i.e. involving Mars. Other applications are combustion diagnostics in premixed and diffusion flames.

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.)
Aerodynamics
Entry, Descent, & Landing (see also Planetary Navigation, Tracking, & Telemetry)
Spacecraft Design, Construction, Testing, & Performance (see also Engineering; Testing & Evaluation)

Form Generated on 03-10-16 12:21