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Properties and Improved Space Survivability of POSS (Polyhedral Oligomeric Silsesquioxane) Polyimides

Published online by Cambridge University Press:  01 February 2011

Sandra J. Tomczak
Affiliation:
AFRL/PRSM, Materials Applications Branch, Air Force Research Laboratory, 10 E. Saturn Blvd, Bldg. 8451, Edwards AFB, CA 93524, USA
Darrell Marchant
Affiliation:
ERC Incorporated, Materials Applications Branch, Air Force Research Laboratory, 10 East Saturn, Blvd, Bldg 8451, Edwards AFB, CA 93524, USA
Steve Svejda
Affiliation:
AFRL/PRSM, Materials Applications Branch, Air Force Research Laboratory, 10 E. Saturn Blvd, Bldg. 8451, Edwards AFB, CA 93524, USA
Timothy K. Minton
Affiliation:
Department of Chemistry and Biochemistry, Montana State University, 108 Gaines Hall, Bozeman, MT 59717, USA, tminton@montana.edu
Amy L. Brunsvold
Affiliation:
Department of Chemistry and Biochemistry, Montana State University, 108 Gaines Hall, Bozeman, MT 59717, USA, tminton@montana.edu
Irina Gouzman
Affiliation:
Space Environment Section, Soreq NRC, Yavne 81800, Israel
Eitan Grossman
Affiliation:
Space Environment Section, Soreq NRC, Yavne 81800, Israel
George C. Schatz
Affiliation:
Department of Chemistry, Northwestern University, Evanston, IL. 60208–3113USA, schatz@chem.northwestern.edu
Diego Troya
Affiliation:
Department of Chemistry, Northwestern University, Evanston, IL. 60208–3113USA, schatz@chem.northwestern.edu
LiPeng Sun
Affiliation:
Department of Chemistry, Northwestern University, Evanston, IL. 60208–3113USA, schatz@chem.northwestern.edu
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Abstract

Kapton polyimide (PI) is widely used on the exterior of spacecraft as a thermal insulator. Atomic oxygen (AO) in lower earth orbit (LEO) causes severe degradation in Kapton resulting in reduced spacecraft lifetimes. One solution is to coat the polymer surface with SiO2 since this coating is known to impart remarkable oxidation resistance. Imperfections in the SiO2 application process and micrometeoroid / debris impact in orbit damage the SiO2 coating, leading to erosion of Kapton.

A self passivating, self healing silica layer protecting underlying Kapton upon exposure to AO may result from the nanodispersion of silicon and oxygen within the polymer matrix. Polyhedral oligomeric silsesquioxane (POSS) is composed of an inorganic cage structure with a 2:3 Si:O ratio surrounded by tailorable organic groups and is a possible delivery system for nanodispersed silica. A POSS dianiline was copolymerized with pyromellitic dianhydride and 4, 4′-oxydianiline resulting in POSS Kapton Polyimide. The glass transition temperature (Tg) of 5 to 25 weight % POSS Polyimide was determined to be slightly lower, 5 – 10 %, than that of unmodified polyimides (414 °C). Furthermore the room temperature modulus of polyimide is unaffected by POSS, and the modulus at temperatures greater than the Tg of the polyimide is doubled by the incorporation of 20 wt % POSS.

To simulate LEO conditions, POSS PI films underwent exposure to a hyperthermal O-atom beam. Surface analysis of exposed and unexposed films conducted with X-ray photoelectron spectroscopy, atomic force microscopy, and surface profilometry support the formation of a SiO2 self healing passivation layer upon AO exposure. This is exemplified by erosion rates of 10 and 20 weight % POSS PI samples which were 3.7 and 0.98 percent, respectively, of the erosion rate for Kapton H at a fluence of 8.5 × 1020 O atoms cm-2. This data corresponds to an erosion yield for 10 wt % POSS PI of 4.8 % of Kapton H. In a separate exposure, at a fluence of 7.33 × 1020 O atoms cm-2, 25 wt % POSS Polyimide showed the erosion yield of about 1.1 % of that of Kapton H. Also, recently at a lower fluence of 2.03 × 1020 O atoms cm-2, in going from 20 to 25 wt % POSS PI the erosion was decreased by a factor of 2 with an erosion yield too minor to be measured for 25 wt % POSS PI.

Type
Research Article
Copyright
Copyright © Materials Research Society 2005

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References

REFERENCES

1. de Groh, K. K., Banks, B. A., “Techniques for Measuring Low Earth Orbital Atomic Oxygen Erosion of Polymers,” 2002 Symposium and Exhibition sponsored by the Society for the Advancement of Materials and Process Engineering, Long Beach, CA, May 12–16, 2002.Google Scholar
2. Koontz, S. L., Leger, L. J., Visentine, J. T., Hunton, D. E., Cross, J. B., and Hakes, C. L., “EOIM-III Mass Spectroscopy and Polymer Chemistry: STS 46, July – August 1992,” Journal of Spacecraft and Rockets, Vol. 32, No. 3, 1995, pp. 483 – 495.Google Scholar
3. de Groh, K. K., and Banks, B. A., “Automic-Oxygen Undercutting of Long Duration Exposure Facility Aluminized-Kaption Multilayer Insulation,” Journal of Spacecraft and Rockets, Vol. 31, No., 4. 1994, pp. 656 – 664.Google Scholar
4. Banks, B. A., Rutledge, S. K., de Groh, K. K., Mirtich, M. J., Gebauer, L., Olle, R., and Hill, C. M., “The Implication of the LDEF Results on Space Freedom Power System Materials, “Proceedings of the 5th International Symposium on Material in a Space Environment”, Cannes-Mandelieu, France, 1991, p. 137 Google Scholar
5. Tennyson, R. C., “Protective Coatings for Spacecraft Materials, “Surface and Coatings Technology”, 68/69 (1994) 519 – 527. p. 45.Google Scholar
6. Gilman, J.W., Schlitzer, D. S., Lichtenhan, J. D., “Low Earth Orbit Resistant Siloxane Copolymers,” Journal of Applied Polymer Science, Vol. 60, p. 591 – 596. (1996)Google Scholar
7. Grobner, J. and Kerr, J. B., “Ground-Based Determination of the Spectral Ultraviolet Extraterrestrial Soalar Irradiance: Providing a Link Between Space-Based and Ground-Based Solar UV Measurements, “Journal of Grophysical Research-Atmospheres,” 2001. 106(D7): p. 7211 - 7217.Google Scholar
8. Mather, P.T., Jeon, H.G., Romo-Uribe, A., Haddad, T.S., and Lichtenhan, J.D., “Mechanical Relaxation and Microstructure of Poly(Norbornyl- POSS) Copolymers,” Macromolecules, 1999. 32(4): p. 11941203.Google Scholar
9. Wright, M. E., Schorzman, D. A., Feher, F.J., and Jin, R. Z., “Synthesis and Thermal Curing of Aryl-Ethynyl-Terminated coPOSS Imide Oligomers: NewInorganic/Organic Hybrid Resins,” Chemistry of Materials. 2003, 15, 264268 Google Scholar
10. Feher, F.J., Nguyen, F., Soulivong, D., and Ziller, J.W., “A New Route to Incompletely Condensed Silsesquioxanes: Acid- Mediated Cleavage and Rearrangement of (c-C6H11)(6)Si6O9 to C-2-[(c-C6H11)(6)Si6O8X2],” Chemical Communications, 1999(17): p. 17051706.Google Scholar
11. Feher, F.J., Terroba, R., and Ziller, J.W., “A New Route to Incompletely-Condensed Silsesquioxanes: Base- Mediated Cleavage of Polyhedral Oligosilsesquioxanes,” Chemical Communications, 1999(22): p. 23092310.Google Scholar
12. Feher, F.J., Soulivong, D., and Eklund, A.G., “Controlled Cleavage of R8Si8O12 Frameworks: A Revolutionary New Method for Manufacturing Precursors to Hybrid Inorganic-Organic Materials,” Chemical Communications, 1998(3): p. 399400.Google Scholar
13. Blanski, R.L., Phillips, S. H., Chaffee, K., Lichtenhan, J. D.,, Lee, A., and Geng, H.P., “The Preparation and Properties of Organic/Inorganic Hybrid Materials by Blending POSS into Organic Polymers,” Polymer Preprints, 2000. 41(1): p. 585.Google Scholar
14. Brunsvold, Amy L., Minton*, Timothy K., Gouzman, Irina, Grossman, Eitan, and Gonzalez, Rene The Journal of High Performance Polymers, Special Edition, Publication, 2004, 16(2), p. 303318.Google Scholar
15. Gonzalez, R. I., “Synthesis and In-Situ Atomic Oxygen Erosion Studies of Space-Survivable Hybrid Organic/Inorganic POSS Polymers,” Ph.D. Dissertation, Chem Eng Department, University of Florida, 2002. http://purl.fcla.edu/fcla/etd/UFE1000127 Google Scholar
16. Gonzalez, R. I., Phillips, S. H., Hoflund, G. B., “In Situ Oxygen–Atom Erosion Study of polyhedral oligomeric silsesquioxane-Siloxane Copolymer,” Journal of Spacecraft and Rockets, 2000, 37(4), p. 463467.Google Scholar
17. Minton, T. K., and Garton, D. J., “Dynamics of Atomic-Oxygen-Induced Polymer Degradation in Low-Earth Orbit,” in Advanced Series in Physical Chemistry: Chemical Dynamics in Extreme Environments, edited by Dressler, R. A. (World Scientific, Singapore, 2001), pp. 420489.Google Scholar
18. Dooling, D. and Finckenor, M. M., “Material Selection Guidelines to Limit Atomic Oxygen Effects on Spacecraft Surfaces, NASA/TP – 1999 -209260, p.Google Scholar
19. Garton, D J, Minton, T K, Maiti, B, Troya, D, and Schatz, G C 2003 Journal of Chemical Physics 118 1585–8Google Scholar
20. Troya, Diego and Schatz, George C., J. Chem. Phys., 120, 76967707 (2004).Google Scholar
21. Cornelius, C.J. and Marand, E., Polymer 2002; 43: 2385.Google Scholar
22. Mauritz, K.A. and Warren, M., Macromolecules 1989; 22: 1730.Google Scholar
23. Matos, M.C., Ilharco, L.M. and Almeida, R.M. J Non-Cryst Solids 1992; 147, 148: 232–7.Google Scholar
24. Cowie, J.M.G. Polymers: chemistry and physics of modern materials. 2nd Ed. New York: Blackie/Chapman & Hall, 1994.Google Scholar
25. Menard, K.P. Dynamic Mechanical Analysis: A Practical Introduction New York: CRC Press, 1999.Google Scholar
26. Adrova, N.A., Bessonov, M.I., Laius, L.A. and Rudakov, A.P. Polyimides: A New Class of Heat-resistant Polymers Jerusalem: IPST Press, 1969 Google Scholar