NASA STTR 2008 Solicitation


PROPOSAL NUMBER: 08-1 T3.01-9974
RESEARCH SUBTOPIC TITLE: Technologies for Space Power and Propulsion
PROPOSAL TITLE: Advanced Radiative Emitters for Radioisotope Thermophotovoltaic Power Systems

NAME: Creare, Inc. NAME: Massachusetts Institute of Technology
STREET: P.O. Box 71 STREET: 77 Massachusetts Avenue
CITY: Hanover CITY: Cambridge
STATE/ZIP: NH  03755 - 0071 STATE/ZIP: MA  02139 - 4301
PHONE: (603) 643-3800 PHONE: (617) 258-5015

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Richard Kaszeta
P.O. Box 71
Hanover, NH 03755 - 0071
(603) 640-2441

Expected Technology Readiness Level (TRL) upon completion of contract: 3 to 4

TECHNICAL ABSTRACT (Limit 2000 characters, approximately 200 words)
Radioisotope Power Systems (RPS) are critical for future flagship exploration missions in space and on planetary surfaces. Small improvements in the RPS performance, weight, size, and/or reliability can have a dramatic effect on the scientific capability of the vehicle and the overall mission costs. Radioisotope Thermophotovoltaic (RTPV) energy converters are a particular type of RPS that directly convert the heat produced by a General Purpose Heat Source (GPHS) to electrical power using a specialized Photovoltaic (PV) cell. A key element in an RTPV system is the radiative emitter that converts GPHS thermal energy to radiative energy that illuminates the PV cell. In this project, Creare and the Massachusetts Institute of Technology (MIT) propose to develop an advanced, 2-D, photonic crystal radiative emitter that is optimized for RTPV systems. The emitter will provide high emittance in the bandgap of the PV cell with low emittance elsewhere that, when coupled with advanced PV cell filter technology, will provide high system efficiency. In Phase I, we will design the emitter and fabricate test samples, which will be fully characterized for high-temperature emittance and durability. We will also assess the impact of this new emitter on the overall RTPV system design and performance.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
Exploration missions that extend much beyond the earth's orbit around the sun are severely limited by the amount of power that can be generated by conventional solar panels. Radioisotope power systems are, therefore, required to enable flagship missions to the outer solar system and in some cases to the inner solar system (e.g., the lunar poles). RTPV systems offer the potential for high specific power and high efficiency, both of which can lead to vehicles with more science capability at lower cost and lower launch mass. RTPV offers the potential reliability and low vibration of a static conversion process like thermoelectrics with efficiency approaching that of dynamic systems like Stirling and Brayton energy converters. RTPV could, therefore, be a viable alternative for any NASA exploration mission requiring an RPS.

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
Radioisotope power systems are used for a number of military applications. RTPV-based systems would be a viable alternative to the current thermoelectric-based systems. There is also current interest in small nuclear powered batteries based on RTPV. The emitter technology developed on this project could be readily applied in both these military applications. TPV with combustion-based heat sources has long been considered for a number of industrial and consumer applications. The technology developed on this project would have potential application in many of these systems if a commercial TPV system were ever marketed. Most likely, this would be a low power energy scavenging application(s) (e.g., self-powered sensor).

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.

Nuclear Conversion
Photovoltaic Conversion
Thermodynamic Conversion
Thermoelectric Conversion

Form Generated on 11-24-08 11:59