Numerical Study of Porous Cylindrical Containment for the Fuel Element of a Centrifugal Nuclear Thermal Rocket

Author:

Bhat Pramatha1ORCID,Adams Kendall R.2,Herring Stephen J.3,Kirkwood Brad3

Affiliation:

1. Texas A&M University, Department of Nuclear Engineering, College Station, Texas

2. Boise State University, Department of Electrical and Computer Engineering, Boise, Idaho

3. Universities Space Research Association, Center for Space Nuclear Research, Washington, DC

Funder

National Aeronautics and Space Administration

Publisher

Informa UK Limited

Reference34 articles.

1. R. A. BRAEUNIG “Rocket Propellants ” Rocket & Space Technology; http://www.braeunig.us/space/propel.htm (current as of Sep. 4 2023).

2. Nuclear Thermal Propulsion (NTP): A proven growth technology for human NEO/Mars exploration missions

3. D. L. BLACK and S. V. GUNN, “A Technical Summary of Engine and Reactor Subsystem Design Performance During the NERVA Program,” presented at the Conf. on Advanced SEI Technologies, Cleveland, Ohio, September 4−6, 1991.

4. J. MCCARTHY “Nuclear Reactors for Rockets ” Jet Propuls. 24 1 (1954).

5. J. ALLEN et al., “Overview of High-Performance Centrifugal Nuclear Thermal Rocket Propulsion System,” presented at the ANS Virtual Winter Mtg., November 2020.

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