Rsrc
J-GLOBAL ID:201110024205157066   Research Resource code:5000002685 Update date:Jan. 11, 2005

Cryogenic Inducer Test Facility

極低温インデューサ試験施設
Owning Organization:
Contact: SHIMURA Takashi
Resource classification: Experience equipment, Facilities, etc
Research area  (1): Fluidics
Overview:
Purpose: Tests of thermodynamic effects in cavitating
inducers using liquid nitrogen or liquid hydrogen.
Performance: Electric motor output (1,400kw), Maximum
rotational speed of inducer (LN2: 35,000rpm,
LH2: 62,000rpm), Maximum flow rate (LN2: 0.18m3/s,
LH2: 0.24m3/s), Maximum pressure (4MPa),
Run tank capacity (LN2: 20m3, LH2: 15m3),
Function of temperature control of LN2(Increase by
pressurerization and circulation, Decrease by vacuum
pumping and circulation )
Built: 2003
Research field : Rocket Engine Turbopumps
User environment and conditions:
Test models are needed.
User procedures and method:
-Procedure of use
Inquire details from the Program Support Division.

Return to Previous Page