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Real-Time Micro-Miniature Dosimeter

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNC06CA73C
Agency Tracking Number: 054401
Amount: $69,945.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: N/A
Solicitation Number: N/A
Timeline
Solicitation Year: N/A
Award Year: 2006
Award Start Date (Proposal Award Date): N/A
Award End Date (Contract End Date): N/A
Small Business Information
2851 Commerce Street
Blacksburg, VA 24060
United States
DUNS: 627132913
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Robert Fielder
 Principal Investigator
 (540) 552-5128
 submissions@lunainnovations.com
Business Contact
 Crystal Woodruff
Title: Business Official
Phone: (540) 552-5128
Email: submissions@lunainnovations.com
Research Institution
N/A
Abstract

The new Presidential directive to place humans on Mars and establish bases on the moon will require advances in nuclear thermal propulsion and power generation. Nuclear thermal propulsion has a combined advantage in power density, ISP and low fuel/mass ratio over other propulsion means for these missions. To meet the needs of reactor safety, health monitoring and performance, light-weight, real-time, in-core neutron and gamma monitoring sensors need to be developed. Luna is proposing to develop a real-time miniature gamma and neutron dosimeter. This hybrid sensor will measure gamma and neutron dose independently, as well as temperature, along a single optical fiber at the same location. The transducer will be less than 5mm long and 1mg in mass. This dosimeter will enable real-time determination of reactor power level, health and remaining fuel as well as shielding effectiveness. The design will be based on EFPI measurement techniques developed by Luna and demonstrated in high-radiation and temperature environments. During the Phase I, Luna will demonstrate feasibility of the proposed dosimeter in a nuclear reactor. Phase II will optimize the sensors and demodulation system for performance and cost, considering space hardening constraints, and demonstrate the system in high radiation and high temperature environments.

* Information listed above is at the time of submission. *

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