Propellant Heating Systems

Propellant Heating System is a nuclear thermal propulsion subsystem that belongs to the class of spacecraft propulsion technologies and is specifically characterized by its function of transferring thermal energy from a nuclear reactor to a propellant to increase its enthalpy and generate thrust through expansion in a nozzle.

11

Publications

300

Citations

22

Authors

10

Institutions

Publications per year

2017–2026

0

Authors

22

  1. KA
    Kurt A. Polzin

    Marshall Space Flight Center, United States

    1 publications · 22 citations

    1

    h-index

  2. SC
    S.K. Chou

    National University of Singapore, Singapore

    1 publications · 69 citations

    1

    h-index

  3. HA
    Hui An

    The University of Queensland, Australia

    1 publications · 69 citations

    1

    h-index

  4. WY
    Wenming Yang

    National University of Singapore, Singapore

    1 publications · 69 citations

    1

    h-index

  5. JL
    Jack L. Kerrebrock

    Massachusetts Institute of Technology, United States

    1 publications · 54 citations

    1

    h-index

1–5 of 22

Venues

  1. AIAA Journal

    1 publications · 15 citations

    1

    h-index

  2. 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference

    Conference · 1 publications · 22 citations

    1

    h-index

  3. Journal of Materials Chemistry

    1 publications · 72 citations

    1

    h-index

  4. Applied Energy

    1 publications · 69 citations

    1

    h-index

  5. 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

    Conference · 1 publications · 10 citations

    1

    h-index

1–5