Design of a passive safety system for a nuclear thermal rocket

Author:

Khatry Jivan,Aydogan Fatih,Ilyas Muhammad,Houts Michael

Publisher

Elsevier BV

Subject

Nuclear Energy and Engineering

Reference34 articles.

1. Akyuzlu, K.M., 2014. A numerical study of high temperature and high velocity gaseous hydrogen flow in a cooling channel of a nuclear thermal rocket core. In: ASME 2014 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, pp. 1–13).

2. AZO Materials, 2016. Zirconium Carbide. Retrieved August 27, 2016, from AZO Materials website: http://www.azom.com/properties.aspx?ArticleID=261.

3. Borowski, S.K., McCurdy, D.R., Packard, T.W., 2012Nuclear Thermal Propulsion (NTP): a proven growth technology for human NEO/Mars exploration missions. In: Aerospace Conference, 2012 IEEE, pp. 1–20.

4. Borowski, S.K., McCurdy, D.R., Packard, T.W., 2009Nuclear thermal rocket/vehicle characteristics and sensitivity trades for NASA’s mars design reference architecture (DRA) 5.0 study. In: Proceedings of Nuclear and Emerging Technologies for Space.

5. Bugby, D.C., Cepeda-Rizo, J., Rodriguez, J.I., 2011. Thermal Switching Cryogenic Heat Pipe. Georgia Institute of Technology.

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