Propulsion System Redundancy

Propulsion System Redundancy is a propulsion system design principle that incorporates duplicate or alternative propulsion components, pathways, or mechanisms to ensure continued operational functionality in the event of partial system failure during maneuvering.

24

Publications

608

Citations

62

Authors

24

Institutions

Publications per year

2017–2026

10

Authors

62

  1. HK
    Hiroyuki Koizumi

    The University of Tokyo, Japan

    2 publications · 34 citations

    2

    h-index

  2. SZ
    Shisheng Zhong

    Harbin Institute of Technology, China

    1 publications · 13 citations

    1

    h-index

  3. RL
    Roger Longstaff

    Reaction Engines (United Kingdom), United Kingdom

    1 publications · 34 citations

    1

    h-index

  4. WX
    Wei Xu

    University of Hong Kong, Hong Kong SAR China

    1 publications · 31 citations

    1

    h-index

  5. LW
    Lei Wang

    China University of Petroleum, East China, China

    1 publications · 35 citations

    1

    h-index

1–5 of 62

Venues

  1. Acta Astronautica

    1 publications · 19 citations

    2

    h-index

  2. Journal of Propulsion and Power

    2 publications · 36 citations

    2

    h-index

  3. Energy

    1 publications · 35 citations

    1

    h-index

  4. Journal of Aircraft

    1 publications · 19 citations

    1

    h-index

  5. 1

    h-index

1–5