抄録
Cryogenic Inducer Test Facility(CITF) was constructed in JAXA kakuda Rocket Engine Research Center. The test facility gas been operated since 2003. Liquid nitrogen and liquid gydrogen are used as working fluid for the experiments of rocket engine turbopump inducers, therefore the themodynamic effect on cavitation could be examinged. The faculty of CITF was verified from the elemental and comprehensive tests. In this paper, the vilification test results and the future programs are presented.
