Paper information

Paper code

IAC-22,C4,IPB,1,x70242

Order

1

Room

IP Area

Title

Numerical Model for the Prediction of the Regression Rate in Hybrid Rocket Kick-Motors Working with Liquid Nitrous Oxide

abstract

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Session

IPB. Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM

symposium

C4. IAF SPACE PROPULSION SYMPOSIUM

congress

IAC-22

Type of presentation

interactive

Main author

Dr. Giuseppe Gallo, Hokkaido University, Italy

Co-authors

Dr. Landon Kamps, Hokkaido University, Japan;

Mr. Shota Hirai, Hokkaido University, Japan;

Dr. Carmine Carmicino, University of Naples "Federico II", Italy;

Prof. Harunori Nagata, Hokkaido University, Japan;