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Comparative Study
. 1997 Dec 9;94(25):13885-90.
doi: 10.1073/pnas.94.25.13885.

Tissue engineering of cartilage in space

Affiliations
Comparative Study

Tissue engineering of cartilage in space

L E Freed et al. Proc Natl Acad Sci U S A. .

Abstract

Tissue engineering of cartilage, i.e., the in vitro cultivation of cartilage cells on synthetic polymer scaffolds, was studied on the Mir Space Station and on Earth. Specifically, three-dimensional cell-polymer constructs consisting of bovine articular chondrocytes and polyglycolic acid scaffolds were grown in rotating bioreactors, first for 3 months on Earth and then for an additional 4 months on either Mir (10(-4)-10(-6) g) or Earth (1 g). This mission provided a unique opportunity to study the feasibility of long-term cell culture flight experiments and to assess the effects of spaceflight on the growth and function of a model musculoskeletal tissue. Both environments yielded cartilaginous constructs, each weighing between 0.3 and 0.4 g and consisting of viable, differentiated cells that synthesized proteoglycan and type II collagen. Compared with the Earth group, Mir-grown constructs were more spherical, smaller, and mechanically inferior. The same bioreactor system can be used for a variety of controlled microgravity studies of cartilage and other tissues. These results may have implications for human spaceflight, e.g., a Mars mission, and clinical medicine, e.g., improved understanding of the effects of pseudo-weightlessness in prolonged immobilization, hydrotherapy, and intrauterine development.

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Figures

Figure 1
Figure 1
Experimental design. Cartilage cells were seeded onto polymer scaffolds, and the resulting constructs were cultivated in rotating bioreactors first for 3 months on Earth and then for 4 additional months either on the Mir Space Station (10−4–10−6 g) or on Earth (1 g).
Figure 2
Figure 2
Cell viability postflight. Cells isolated from a 7-month construct from the Mir group after 2 days of monolayer culture. (×200.) Intracellular esterase activity is indicated by green color.
Figure 3
Figure 3
Construct structure. (A and B) Full cross sections of constructs from Mir and Earth groups. (×10.) (C and D) Representative areas at the construct surfaces. (×200.) GAG is stained red with safranin-O.
Figure 4
Figure 4
Construct ultrastructure. Transmission electron micrographs of constructs from Mir (A) and Earth (B) groups at magnifications of ×3,500 and ×120,000 (Inset).

References

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