TITLE
Design, construction and testing of a new shock freezing system during parabolic flight
AUTHOR
Horn, Astrid
DEPARTMENT
Space Science, Kiruna
SUMMARY
Background: Fixation of tissue is a common method to stop biological
processes and preserve a status of interest for later examination. Popular
done with liquid nitrogen, this is not possible during parabolic flight
investigations, due to safety issues. However, for the investigation of the
direct effects of gravity, respectively the absence of it, it is necessary
to fixate the tissue during or right after the experience of weightlessness.
Hence the aim of this thesis was to invent and establish a method for shock
freezing biological samples during parabolic flight.
A carbon dioxide based freezing system was designed and constructed. Tissue
was frozen in a steel tube where dry ice was created from carbon dioxide out
of two gas cylinders conducted over a pressure system.
The method was tested on Arabidopsis thaliana seedlings and compared to
known freezing techniques, like chemical fixation and liquid nitrogen.
In a comparison of quality and quantity the RNA of deep frozen material was
analyzed.
Results: A system was constructed where samples are deep frozen by dry ice
in
a steel cylinder. Gaseous carbon dioxide from a gas cylinder is conducted
over a pressure line into a steel cylinder, where dry ice is formed due to a
pressure gradient. Arising gas is conducted out of the chamber by a pressure
system.
The whole system is fixed on a rack construction, which can be mounted on
the air craft. The quality of the new system was found to be comparable to
other methods. Analyzed RNA was found to be of good quality. Time until
shock freezing could be reduced to under a minute and duration of freezing
could be guaranteed long enough for a whole flight day during a parabolic
flight campaign.
Conclusion: The Pre-testing on ground gives evidence that the system can be
used during in flight configuration. The system is now to be used in the
10th parbolic flight campaign of the DLR for a first operational test. In
future campaigns it will be available to different research groups as
fixation method.
ISSN 1653-0187 / ISRN LTU-PB-EX--07/058--SE / NR 2007:058
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