TY - GEN
T1 - Coating development on graphite-based composite fuel for nuclear thermal propulsion
AU - Jolly, Brian C.
AU - Trammell, Michael P.
AU - Qualls, Arthur L.
N1 - Publisher Copyright:
© 2015, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2015
Y1 - 2015
N2 - ORNL is currently recapturing graphite-based fuel forms for Nuclear Thermal Propulsion (NTP). Previous work at ORNL focused on reviewing historic fuel technology developed during the ROVER/NERVA programs and performing coating development at the lab scale. The current effort focuses on transitioning the coating work from the lab scale to an intermediate length, and coating an element with a more prototypic geometry to include a hexagonal cross section and multiple internal channels. A new vertical multi-zone furnace capable of coating 16“ length elements was installed and the ability to deposit a ZrC coating along the full length of the element demonstrated. A chemical vapor deposition (CVD) process was used to apply a ZrC coating where zirconium metal was chlorinated in-situ forming ZrCl4 as the Zr precursor and CH4 was used for the carbon source. The coating and additional diluent gases were directed through the internal channels using custom fixtures. While processing conditions were not fully optimized, good progress was made in coating development. Between the information gained and new capabilities installed, an excellent foundation for further fuel development and eventual qualification has been put into place.
AB - ORNL is currently recapturing graphite-based fuel forms for Nuclear Thermal Propulsion (NTP). Previous work at ORNL focused on reviewing historic fuel technology developed during the ROVER/NERVA programs and performing coating development at the lab scale. The current effort focuses on transitioning the coating work from the lab scale to an intermediate length, and coating an element with a more prototypic geometry to include a hexagonal cross section and multiple internal channels. A new vertical multi-zone furnace capable of coating 16“ length elements was installed and the ability to deposit a ZrC coating along the full length of the element demonstrated. A chemical vapor deposition (CVD) process was used to apply a ZrC coating where zirconium metal was chlorinated in-situ forming ZrCl4 as the Zr precursor and CH4 was used for the carbon source. The coating and additional diluent gases were directed through the internal channels using custom fixtures. While processing conditions were not fully optimized, good progress was made in coating development. Between the information gained and new capabilities installed, an excellent foundation for further fuel development and eventual qualification has been put into place.
UR - http://www.scopus.com/inward/record.url?scp=85086949889&partnerID=8YFLogxK
U2 - 10.2514/6.2015-3777
DO - 10.2514/6.2015-3777
M3 - Conference contribution
AN - SCOPUS:85086949889
SN - 9781624103216
T3 - 51st AIAA/SAE/ASEE Joint Propulsion Conference
BT - 51st AIAA/SAE/ASEE Joint Propulsion Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 51st AIAA/SAE/ASEE Joint Propulsion Conference, 2015
Y2 - 27 July 2015 through 29 July 2015
ER -