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Peter Kittel
University of California-Berkeley
pkittel@cal.berkeley.edu
Space Cryogenics is the application of cryogenics to space missions.
These applications fall into two broad areas, supporting space science
missions and supporting the space transportation infrastructure.
Science applications: The atmosphere is opaque to much of the
electro-magnetic spectrum. In space, the absence of an atmosphere has
been a great boon to doing astronomy at these wavelengths. Being in
space has enabled Earth and atmospheric science missions to gather global
data. Many of these science missions use infrared, gamma ray, and x-ray
detectors that operate at cryogenic temperatures. The detectors are
cooled to increase their sensitivity. Astronomy missions often use
cryogenic telescopes to reduce the thermal emissions of the telescope,
permitting very faint objects to be seen. A broad range of cryogenic
technology is needed to support these missions. For instance, materials
change their properties (strength, dimensions, thermal, electrical, magnetic,
and optical properties all change). These changes need to be considered
when building an instrument for space. It is a challenge to design a
telescope that is assembled at room temperature and then cooled to 20 kelvin
(-253°C) or so and launched into space. After surviving the high
vibration environment of launch and the dimensional changes of cooling down,
the instrument must be in focus and provide an undistorted image. All of
this, while being well insulated and having very low mass.
Then there is the matter of how to cool the instrument. Radiators
(blackened surfaces shielded from the Sun and Earth) can cool instruments to
the 100 kelvin (-173°C) range in Earth orbit. In orbits far from the
Earth (such Spitzer uses) 30k (-243°C) can be reached. For lower
temperatures, instruments have used stored solid cryogens (such as nitrogen,
neon, or hydrogen). Solid hydrogen will work for requirements down to
6 kelvin (-267°C). For lower temperatures, liquid helium can be used
in the 1-2 kelvin range. Containing liquids while venting the effluent
vapor has been a challenge. The disadvantage of using a stored cryogen
is that it is converted to vapor by heat dissipated in the instrument or that
comes in through the supports and insulation. Eventually, the cryogen is
consumed, ending the mission. Recently there have been many advances in
building closed cycle refrigerators for space applications. These
coolers have extended mission durations and extended the range of
temperatures available to 0.05 kelvin. These coolers are required to be
long lived, 5-10 years, have a very low system mass (including the mass of
solar cells and electronics to power the coolers and radiators to reject heat)
and, often, have very low vibration.
Another area of space science, which makes use of cryogenics, is sample
preservation. This includes the preservation of biological samples from
experiments on the Shuttle and the Station and the preservation of material
gathered from comets, asteroids, and other planets. These applications
have used phase change materials (solid to liquid transition) or liquid
nitrogen absorbed in fine pore as coolants. Closed cycle coolers are now
being developed for these applications.
Space transportation: Liquid hydrogen and liquid oxygen are used in the
main engines of the Shuttle because they offer a very high specific impulse
(thrust per unit mass of propellant consumed). These propellants are
cryogenic with normal boiling points of 20 kelvin (-253°C) and 90 kelvin
(-183°C) respectively. For the Shuttle, these propellants are stored
in the poorly insulated external tank. There is interest in extending
the storage time of cryogenic propellants from a few hours to many years and
in being able to resupply rockets with these propellants from depots in
space. While, in principle, this can be achieved, the techniques
discussed above, the size of transportation systems, many tons of propellants,
require new engineering approaches.
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