Orbital test results of a vaned liquid acquisition device

Author:

Dominick S.1,Tegart J.1

Affiliation:

1. Martin Marietta Astronautics, Denver, CO

Publisher

American Institute of Aeronautics and Astronautics

Cited by 27 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Experimental Investigation of Liquid Interface Stability During the Filling of a Tank in Microgravity;Microgravity Science and Technology;2023-04-29

2. NUMERICAL INVESTIGATION OF INTERFACE STABILITY IN REDUCED GRAVITY FOR THE APPLICATION OF ON-ORBIT REFUELING OF SPACECRAFT TANKS;International Journal of Energetic Materials and Chemical Propulsion;2023

3. Effect of Wicking Capability on the Reseal Pressure of Woven Screens for On-Orbit Cryogenic Propellants Management;Proceedings of the 28th International Cryogenic Engineering Conference and International Cryogenic Materials Conference 2022;2023

4. Space Liquid Transport Experiments in Tianyuan-1;Microgravity Science and Technology;2022-10-12

5. Testing Liquid Distribution in a Vane-Type Propellant Tank under Conditions of Microgravity Using a Drop Tower Test;International Journal of Aerospace Engineering;2020-11-17

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