Thermal conductivity measurements near T Lamda of Helium-4 in restricted geometries
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Engineering topics
Publications and source records attributed to Liu, F. C..
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The Low Temperature Microgravity Physics Facility currently in the design phase is a multiple user and multiple flight facility intended to provide a long duration low temperature environment onboard the International Space Station.
Descriptions of the payload safety requirements and processes that attached payloads must satisfy to meet to fly on the Shuttle or HTV and to be attached to the ISS from the perspective of a payload safety engineer are presented.
This paper will describe areas of research planned for early missions of LTMPF, as well as LTMPF science requirements, design capabilities and current status.
The Low Temperature Microgravity Physics Facility (LTMPF) is a state of the art facility for conducting fundamental research in a microgravity environment at low temperatures.
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The objective of this investigation is to make analytical determination of the acceleration produced by crew motion in an orbiting space station and define design parameters for the suspension system of microgravity experiments. A simple structural model for simulation of the IOC space station is proposed. Mathematical formulation of this model provides the engineers a simple and direct tool for designing an effective suspension system.
Dynamics of two cable connected space stations
Dynamic response of rectangular plate to series of moving loads
Dynamic response of elastic rectangular plate to series of moving loads
Elastic stability of slender bar with free-free ends under dynamic loading - spacecraft stability
Elastic stability of slender bar under dynamic load for space rocket applications
Transient response of multistage space vehicle to external load
Nonlinear partial differential equations of two variables for vibratory motions of beam