V. Lopez & D. Thomas, “Proposed metric for complexity assessment using SysML,” Aerospace. October 2022. DOI: https://doi.org/10.3390/aerospace9100612
Grumbach & D. Thomas, “Quantitative Validation of the Principles of Complex System Integration,” Systems Engineering. DOI: 10.1002/sys.21641
S. Rawlins, Y. Kim, & D. Thomas, “Feasibility of Low-Enriched Uranium Fueled Nuclear Thermal Propulsion in the Low-Thrust Region Below 16klbf,” Annals of Nuclear Energy, 179(22), December 2022. DOI: 10.1016/j.anucene.2022.109368.
J. Grumbach & D. Thomas,” Systems Integration Implications of Component Reuse” Systems Engineering. DOI: 10.1002/sys.21636.
D. Nikitaev & D. Thomas, “Impacts of In-Situ Alternative Propellant Utilization on Mars Vehicle Architectures Using Nuclear Thermal Propulsion,” AIAA Journal of Spacecraft and Rockets. DOI: 10.2514/1.A35399.
S. Kumar, D. Thomas, & J. Cassibry, “Decoding the Mission Design Problem for NTP Systems for Outer Planet Robotic Missions,” Nuclear Technology. DOI: 10.1080/00295450.2022.2096388.
D. Thomas, M. Houts, W. Walters, K. Hollingsworth, R. Frederick, & J. Cassibry, “Toward the Engineering Feasibility of the Centrifugal Nuclear Thermal Rocket,” Journal of the British Interplanetary Society, 75(5) May 2022, pp. 181-188.
D. Nikitaev & D. Thomas, Alternative Propellant NTP Vehicle Architectures, AIAA Journal of Spacecraft and Rockets. https://arc.aiaa.org/doi/10.2514/1.A35289
D. Nikitaev & D. Thomas, “Preliminary Results for In-Situ Alternative Propellants for Nuclear Thermal Propulsion,” Nuclear Technology.
S. Kumar, D. Thomas, & J. Cassibry, “Nuclear Thermal Propulsion for Jupiter and Saturn Rendezvous Missions,” AIAA Journal of Spacecraft and Rockets. February 2022. https://arc.aiaa.org/doi/10.2514/1.A35212