NASA STTR 2017 Solicitation

FORM B - PROPOSAL SUMMARY


PROPOSAL NUMBER: 171 T3.01-9959
RESEARCH SUBTOPIC TITLE: Energy Harvesting, Transformation and Multifunctional Power Dissemination
PROPOSAL TITLE: Electrical Power from Thermal Energy Scavenging in High Temperature Environments

SMALL BUSINESS CONCERN (SBC): RESEARCH INSTITUTION (RI):
NAME: Physical Sciences, Inc. NAME: Purdue University
STREET: 20 New England Business Center STREET: 155 S. Grant Street
CITY: Andover CITY: West Lafayette
STATE/ZIP: MA  01810 - 1077 STATE/ZIP: IN  47907 - 2114
PHONE: (978) 689-0003 PHONE: (765) 494-6204

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Dr. Prakash B. Joshi
joshi@psicorp.com
20 New England Business Center
Andover, MA 01810 - 1077
(978) 738-8202

CORPORATE/BUSINESS OFFICIAL (Name, E-mail, Mail Address, City/State/Zip, Phone)
Dr. B. David Green
green@psicorp.com
20 New England Business Center
Andover, MA 01810 - 1077
(978) 689-0003

Estimated Technology Readiness Level (TRL) at beginning and end of contract:
Begin: 2
End: 3

Technology Available (TAV) Subtopics
Energy Harvesting, Transformation and Multifunctional Power Dissemination 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)
Physical Sciences Inc. and Purdue University propose to develop a novel approach to scavenging heat from high intensity thermal environments encountered during space missions and converting this thermal power to electrical power at high efficiency. Examples include extremely hot heat shields during vehicle entry into planetary atmospheres (Mars/Venus probes) and during high speed ascent through planetary atmospheres (Sample return from Mars/Venus), hot claddings of radioisotope thermoelectric generators used for powering outer planetary spacecraft and multi-decade planetary bases (Mars/Venus/Lunar), as well as combustors and nozzles of space and launch propulsion systems. In this STTR we will develop an integrated metal hydride system and spectrally-tuned thermophotovoltaic power converter system that can extract heat during periods of high thermal intensity (tens of seconds), and convert it to electricity at greater than 25 percent efficiency. Following the end of this period, the system can continue to generate useful power for additional tens of minutes.

In Phase I, for the power converter system, we will demonstrate feasibility of fabricating a critical component in larger areas (5 cm x 5 cm), and for the metal hydride (MH) system, we will experimentally characterize the MH decomposition/recombination reactions that enable continual electrical power generation for a useful duration after the period of high thermal intensity has ended. In Phase II, we will produce an engineering prototype of the integrated heat scavenging electrical power generator system, fully tested in laboratory environment and in simulated operational thermal environment, together with an analytical model of a functional system.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
The proposed heat scavenging electrical power converter will find applications in NASA exploration missions to planets with atmospheres, such as Venus, Mars, and likely others. Example missions include small, power-limited probes released from an orbiter to enter the atmosphere, gather data during descent, land on the surface, and continue data gathering operations for some time. The proposed technology would generate electrical power during the hot atmospheric descent as well as surface operations. Another example would be a planetary sample return mission, where a small probe ascends a high speed through the atmosphere, with the converter providing power generated from scavenging heat from the vehicle's heat shield. Planetary missions to Venus and Mars are presently a part of the NASA roadmaps. Other applications of the proposed heat scavenging power converter include generation of electricity from hot cladding of radioisotopes used in radioisotope thermoelectric generators on years-long planetary missions and proposed to be used on decades-long planetary bases.

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
The proposed compact power generator devices have several aerospace and commercial applications. For example, power generator can be adapted for long range hypersonic vehicles reentering the earth's atmosphere. The customers for this application are the U.S. Air Force and the Navy. Compact, portable power generators are particularly suited for power generation on a small scale, such as for individual soldiers and campers/backpackers. In these applications, the hot source would be a burner consuming hydrocarbon fuel such as a portable propane cylinder, camping stove, etc. The government customers for this application include the U.S. Army, the U.S. Special Operations Command, and the Marines. Manufacturers of camping equipment would form a very large commercial customer base for this technology. The regenerative hydrides capability of our technology will have wide commercial applications in hydrogen storage systems for a variety of uses in the future hydrogen economy, including automobiles. Customers include various DoD agencies as well as a range of commercial manufacturers.

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.)
Active Systems
Conversion
Heat Exchange
Storage

Form Generated on 04-19-17 12:45