Numerical investigation on sealing behaviors of an extremely high-speed two-stage impellers structure in cryogenic rockets

Author:

Ma Yuan1,Li Yanzhong12,Xie Fushou1ORCID,Wang Lei1,Zhu Kang1

Affiliation:

1. Institute of Refrigerating and Cryogenic Engineering; Xi'an Jiaotong University; Xi'an China

2. State Key Laboratory of Technologies in Space Cryogenic Propellants; Chinese Academy of Sciences; Beijing China

Funder

China Postdoctoral Science Foundation

Research Fund of State Key Laboratory of Technologies in Space Cryogenic Propellants

National Natural Science Foundation of China

Publisher

Wiley

Subject

Waste Management and Disposal,Renewable Energy, Sustainability and the Environment,General Chemical Engineering

Reference28 articles.

1. Investigation on no-vent filling process of liquid hydrogen tank under microgravity condition;Ma;Int J Hydrogen Energy,2017

2. Effects of leaking rate on turbopump end-face sealing performance;Bai;J Rocket Propul,2010

3. Research on elastic metal sealing technology for high-pressure staged combustion LOX/kerosene engine;Lei;J Rocket Propul,2014

4. An investigation of the operation and failure of mechanical face seals;Orcutt;J Lubr Technol,1969

5. Research in mechanical seals;Nau;Proc Inst Mech Eng Part C,1990

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