Combined-cycle Propulsion

Combined-Cycle Propulsion is a propulsion system that integrates multiple thermodynamic cycles within a single engine platform to enable efficient operation across a broad speed range by leveraging the distinct performance characteristics of each cycle in its respective flight regime.

178

Publications

5.3K

Citations

481

Authors

144

Institutions

Publications per year

2017–2026

59

Variants

CceCombined-cycle Engine

Authors

481

  1. FQ
    Fei Qin

    Northwestern Polytechnical University, China

    10 publications · 309 citations

    10

    h-index

  2. GH
    Guoqiang He

    Northwestern Polytechnical University, China

    9 publications · 292 citations

    9

    h-index

  3. ST
    Sadatake Tomioka

    Japan Aerospace Exploration Agency, Japan

    8 publications · 167 citations

    9

    h-index

  4. TK
    Takeshi Kanda

    Japan Aerospace Exploration Agency, Japan

    8 publications · 251 citations

    8

    h-index

  5. SU
    Shuichi Ueda

    Japan Aerospace Exploration Agency, Japan

    6 publications · 122 citations

    7

    h-index

1–5 of 481

Venues

  1. Acta Astronautica

    13 publications · 384 citations

    13

    h-index

  2. Journal of Propulsion and Power

    11 publications · 459 citations

    11

    h-index

  3. Energy

    8 publications · 251 citations

    8

    h-index

  4. Applied Thermal Engineering

    8 publications · 318 citations

    8

    h-index

  5. NASA Technical Reports Server (NASA)

    Repository · 6 publications · 127 citations

    7

    h-index

1–5