Paper information

Paper code

IAC-26,C4,8-B4.5A,6,x107124

Date

2026-10-08

Time

15:40

Order

6

Room

E6

Title

Development of Dual Mode Thruster for 2U-size Microsatellite-Friendly Multi-Purpose Propulsion System (MFMP-PROP) for Collision Avoidance Maneuver (CAM) and Post Mission Disposal (PMD)

abstract

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Session

8-B4.5A. Joint Session between IAA and IAF for Small Satellite Propulsion Systems

symposium

C4. IAF SPACE PROPULSION SYMPOSIUM

congress

IAC-26

Type of presentation

oral

Main author

Dr. Toshiaki Iizuka, National Institute of Technology, Oyama College, Japan

Co-authors

Mr. Sota Chubachi, National Institute of Technology, Oyama College, Japan;

Dr. Shun Katsube, Tokyo University of Science, Japan;

Prof. Hironori Sahara, Tokyo Metropolitan University, Japan;