Surface tension discharge mechanism for space propulsion fuel tanks.
Design and development of a surface tension discharge mechanism for propellant tanks used in artificial satellites, with numerous flight performance records.
Design and development of surface tension discharge mechanisms (PMD) for various types of propellant tanks for artificial satellites. Conducted design and development of discharge functions that utilize the surface tension of propellants such as hydrazine, MMH, MON, NTO, and ADN to supply propellants to engines and thrusters in microgravity and zero-gravity conditions.
- Company：Advanced Technology Institute, LLC 本社
- Price：Other
