Investigation of Transient Temperature Oscillations of a Propylene Loop Heat Pipe 2001-01-2235

A technology demonstration propylene Loop Heat Pipe (LHP) has been tested extensively in support of the implementation of this two-phase thermal control technology on NASA’s Earth Observing System (EOS) Tropospheric Emission Spectrometer (TES) instrument. This cryogenic instrument is being developed at the Jet Propulsion Laboratory (JPL) for NASA. This paper reports on the transient characterization testing results showing low frequency temperature oscillations. Steady state performance and model correlation results can be found elsewhere. Results for transient startup and shutdown are also reported elsewhere.

In space applications, when LHPs are used for thermal control, the power dissipation components are typically of large mass and may operate over a wide range of power dissipations; there is a concern that the LHP evaporator may see temperature oscillations at low powers and over some temperature range. In addition, the LHP may not start when power is applied to the component until a significant temperature overshoot from the equilibrium temperature is developed. In most space applications, the temperature oscillation will pose a problem because the maximum allowable flight temperatures (AFTs) may be exceeded and the long-term reliability of equipment is compromised. When equipment temperature stability is important, this becomes a serious issue. Its important to understand the LHP behavior in such a situation in order to mitigate potential problems and design predictable two-phase thermal control systems.

A test program was developed at JPL to characterize the transient behavior of a propylene LHP with a large mass attached to the evaporator and at low powers and low sink temperatures. The LHP was tested in a horizontal orientation with heat loads ranging from 15 to 75 watts and condenser temperatures from -30°C to 0°C. In addition, a small heater and temperature sensor were placed on the LHP compensation chamber to provide close loop temperature control and was tested under similar conditions. Transient results show repeatable low frequency temperature oscillations for a range of conditions. When temperature control is applied to the compensation chamber, the evaporator temperature oscillations disappear. Recommendations are made for additional research on this topic.