Specific Impulse

Specific Impulse is a performance metric in propulsion systems that quantifies the impulse produced per unit of propellant consumed, typically expressed as thrust force per unit weight flow rate of propellant, distinguishing it from other efficiency measures by directly reflecting the propellant efficiency of rocket and jet engines.

1K

Publications

33.2K

Citations

2.6K

Authors

648

Institutions

Publications per year

2017–2026

225

Authors

2.6K

  1. RR
    Richard R. Hofer

    Jet Propulsion Laboratory, United States

    18 publications · 751 citations

    16

    h-index

  2. JK
    Jiro Kasahara

    Keio University, Japan

    12 publications · 490 citations

    12

    h-index

  3. TH
    Thomas Haag

    Glenn Research Center, United States

    15 publications · 482 citations

    12

    h-index

  4. HK
    Hani Kamhawi

    Glenn Research Center, United States

    13 publications · 334 citations

    11

    h-index

  5. SK
    Stanley K. Borowski

    Glenn Research Center, United States

    10 publications · 275 citations

    10

    h-index

1–5 of 2.6K

Venues

  1. Journal of Propulsion and Power

    144 publications · 5.6K citations

    41

    h-index

  2. Propellants Explosives Pyrotechnics

    28 publications · 751 citations

    19

    h-index

  3. AIAA Journal

    24 publications · 1K citations

    18

    h-index

  4. IEEE Transactions on Plasma Science

    21 publications · 949 citations

    16

    h-index

  5. NASA Technical Reports Server (NASA)

    Repository · 25 publications · 529 citations

    16

    h-index

1–5