Abstract
We describe the background and status of a Shuttle mission to measure the heat capacity of helium confined by parallel plates with 57-μm spacing very close to the superfluid transition. The purpose of the experiment is to compare the results with the emerging theory of confined systems with emphasis on the behavior during crossover from three to two dimensions. The experiment will use a cylindrical copper calorimeter of very high thermal conductivity, partly filled with evenly spaced thin silicon plates. It will be attached to a pair of high-resolution, fast-response paramagnetic salt thermometers with rms noise levels below 0.1 nK/Hz1/2 and suspended from a high-stability thermal isolation system previously used on the Shuttle. We expect to obtain heat capacity data to within 1 nK of the lambda point. In addition, wide-range data containing information on the behavior of the surface specific heat will be collected.
| Original language | English |
|---|---|
| Pages (from-to) | 154-159 |
| Number of pages | 6 |
| Journal | Journal of Spacecraft and Rockets |
| Volume | 33 |
| Issue number | 1 |
| DOIs | |
| State | Published - 1996 |
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