Text Size
OpNom:
Overview | Description | Applications | Operations | Results | Publications | Imagery
Experiment OverviewMISSE-1 and 2 are a test bed for materials and coatings attached to the outside of the ISS is being evaluated for the effects of atomic oxygen, direct sunlight, and extremes of heat and cold. This experiment allows the development and testing of new materials to better withstand the rigors of space environments. Results will provide a better understanding of the durability of various materials when they are exposed to the space environment. Many of the materials may have applications in the design of future spacecraft.
Principal Investigator(s)
Information Pending
Developer(s)
Boeing, Phantom Works, Renton, WA, United States
Langley Research Center, Hampton, VA, United States
Marshall Space Flight Center, Huntsville, AL, United States
National Aeronautics and Space Administration (NASA)
Sponsoring OrganizationTechnology Demonstration Office (TDO)
Research BenefitsInformation Pending
ISS Expedition Duration:August 2001 - October 2005
Expeditions Assigned3,4,5,6,7,8,9,10,11
Previous ISS MissionsNASA has conducted a series of space experiments to determine the best materials to survive in the space environment. During mission STS-76, the shuttle crew attached the Mir Environmental Effects Payload (MEEP) on Mir. One and a half years later the crew of the STS-86 mission retrieved the MEEP and brought it back to earth for analysis. Shuttle flight STS-85 featured the Evaluation of Space Environment and Effects on Materials study which tested thin polymer films that contained phenylphosphine oxide which, when exposed to space conditions, formed a phosphate barrier that protected the films from further attacks of atomic oxygen. The Long Duration Exposure Facility (LDEF) was another materials test in the space environment. It orbited in space for five and a half years before being returned to Earth for analysis of the materials that were tested.
Researchers from the private and public sector prepared a wide range of samples for the first externally mounted
experiment on ISS. MISSE-1 and -2 were testbeds for more than
400 materials and coatings samples, testing their survivability under the corrosive effects of the space environment;
including micrometeoroid and orbital debris strikes, atomic oxygen
attack, intense ultraviolet radiation from the sun, and extreme
temperature swings. Results will provide a better understanding
of the durability of various materials in this environment. Many
of the materials may have applications in the design of future
spacecraft.
Both MISSE-1 and -2 were deployed in August 2001 on
Expedition 3 and were planned for a one-year exposure. Due to
the delays incurred following the Columbia accident, they were
not retrieved until four years later during ISS Expedition 11 in
August 2005. Follow-on samples testing new materials, new
technologies and with increasingly complex missions were part of subsequent MISSE experiments mounted on the
station (MISSE-5, MISSE-3, MISSE-4, and MISSE-6).
Results will provide a better understanding of the durability of various materials when they are exposed to the space environment. Many of the materials may have applications in the design of future spacecraft.
Earth ApplicationsThe new advanced materials and components that will be demonstrated in MISSE will improve the performance, increase the useful life, and reduce the costs of future space operations of commercial weather, communication and Earth observation satellites that we all now depend on.
MISSE is mounted to the Station's exterior on the airlock. It is a passive experiment requiring no power or crew interaction. The critical interaction is between the samples and the space environment.
Operational ProtocolsDuring extravehicular activity (EVA) on August 16, 2001, astronauts installed the MISSE PEC 1 and 2 on the Quest airlock of ISS. During subsequent EVAs, crewmembers captured snapshots of the MISSE PECs, if time permitted. In August 2005, during an EVA, Increment 11 crewmembers retrieved the MISSE PECs. The samples were returned to the investigators, who will carefully examine each to determine how the materials fared.
In late 2005, 35 investigators taking part in MISSE-1 and -2 traveled to NASA Langley Research Center to inspect their samples and prepare them for return to their respective laboratories for further analysis. Researchers taking part in this investigation have interests in polymers, thermal control coatings, nano-composites, radiation shielding, environmental monitors, and marking processes designed to label parts that will be exposed to the space environment. The primary data from MISSE will be obtained by comparing the preflight laboratory characterization of the test specimens with postflight laboratory characterizations made after the specimens are retrieved.
Some particulate contamination was observed. Optical property changes in thermal control materials were also
observed. Several materials did well in the harsh environment. Lack of widespread molecular contamination on
MISSE gives confidence in using station for future material studies. A number of results are anticipated to be
released over the next few years. While the samples are still under investigation, researchers indicate that over 100
micrometeoroid and space debris strikes were found. Many polymer film samples were completely eroded by atomic
oxygen, but some samples survived and are undergoing analysis.
Many of the experiments provide space-validated
results for ground-based experiments, such as the
durability of materials to withstand atomic Oxygen
erosion (AO) (deGroh et al. 2008). Because AO
erosion is the primary weathering force to spacecraft
materials, and true space environmental conditions are
difficult to replicate on Earth, MISSE provides a
valuable test platform that enables methods for
correlating and extrapolating ground results. Snyder
et al. (2006) discuss results from MISSE-2 testing of
AO erosion of SiOx coated Kapton compared to
uncoated Kapton (the atomic Oxygen erosion profile of
Kapton is well documented). They calculated mass loss.
De Groh et al. (2006) analyzed 41 different polymers
called PEACE (Polymer Erosion and Contamination Experiment) Polymers, with the objective to determine the
atomic oxygen erosion yield for a variety of materials such as Kevlar, polyethelene, Lucite, Kapton and Teflon that are used in spacecraft and exposed to the space environment. The erosion yield data are immediately
applicable to spacecraft designs. Even though the length of exposure was four times longer than planned, the
sample preparation method of stacking many thin layers allowed for meaningful data even after four years: not
all of the material had eroded away. Samples masses were weighed after flight and compared with preflight
masses to calculated erosion yields.
Other investigators studied specific polymers with various compositional additives or coatings to test resistance
to atomic oxygen erosion (e.g. Tomczak et al. 2007, Juhl et al. 2007). One approach (Tomczak et al. 2007) is to
embed polymers with nano-sized SiO2. With Atomic Oxygen exposure, a silica pasivation layer is formed.
In addition to testing various materials, experiments were also set up to measure the geometry of atomic oxygen
scattering from oxidized Aluminum surfaces.
MISSE-1 and -2 materials, and insights into atomic oxygen erosion have resulted in several patents and spin-offs
ranging from cleaning artwork, etching parts to be used in human grafts, developing new methodologies for testing
blood sugar, and more. Because MISSE assembles partners across industry and DoD, in addition to NASA
scientists and academic partners, many of the results are proprietary. (Evans et al. 2009)
Snyder A, Waters DL, Banks BA. Undercutting Studies of Protected Kapton H Exposed to In-Space and Ground-Based Atomic Oxygen. NASA Technical Memorandum; 2006 August.
Harvey GA, Kinard WH. MISSE 1 and 2 Tray Temperature measurements. Proceedings of MISSE Post Retrieval Conference and the 2006 National Space and Missile Materials Symposium, Orlando, FL; 2006 June
Dever JA, Jaworske DA, Sechkar EA, Panko SR, Miller SK, Banks BA, de Groh KK. NASA Glenn Research Center's Materials International Space Station Experiments (MISSE 1-7). NASA Technical Memorandum; 2008 Dec.
Backus JA, Manno MV, Waters DL, Cameron KC, Banks BA, de Groh KK. Atomic Oxygen Erosion Yield Prediction for Spacecraft Polymers in Low Earth Orbit. NASA Technical Memorandum; 2009.
McCarthy CE, Rucker RN, Roberts LM, Berger LA, Banks BA, de Groh KK. MISSE 2 PEACE Polymers Atomic Oxygen Erosion Experiment on the International Space Station. Sage. 2008; 20: 388. DOI: 10.1177/0954008308089705.
Rice N, Shepp A, Haghighat R, Connell JW. Durable TOR Polymers on MISSE. National Space and Missile Materials Symposium, Keystone, CO; 2007 [ITAR Restricted]
Dever JA, Sechkar EA, Wittberg TN, Miller SK. Space Environment Exposure of Polymer Films on the Materials International Space Station Experiment: Results from MISSE 1 and MISSE 2. Sage. 2008; 20: 371. DOI: 10.1177/0954008308089704.
McCarthy CE, Rucker RN, Roberts LM, Berger LA, Banks BA, de Groh KK. MISSE PEACE Polymers Atomic Oxygen Erosion Results. NASA Technical Memorandum; 2006.
Finckenor MM. The Materials on International Space Station Experiment (MISSE): First Results from MSFC Investigations. 44th Aerospace Sciences Meeting and Exhibit. Reno, NV; 2006
Juhl SB, Akinlemibola B, Kasten L, Vaia R. Durability of Poly(Caprolactam) (Nylon 6) and Poly(Caprolactam) Nanocomposites in Low Earth Orbit. National Space and Missile Materials Symposium, Keystone, CO; 2007 [ITAR Restricted]
Watson KA, Ghose S, Lillehei PT, Smith Jr. JG, Connell JW. Effect of LEO Exposure on Aromatic Polymers Containing Phenylphosphine Oxide Groups. Proceedings of the 9th International Conference: Protection of Materials and Structures From Space Environment, Toronto, Cnnada; 2008 291-299. [ITAR Restricted]
Tomczak SJ, Vij V, Minton TK, Brunsvold AL, Marchant D, Wright ME, Petteys BJ, Guenthner AJ, Yandek GR, Mabry JM. Studies of POSS-Polyimides Flown on MISSE-1. National Space and Missile Materials Symposium, Keystone, CO; 2007 [ITAR Restricted]
Tollis G, Dever JA, Messer R, Sechkar EA, Miller SK. Exposure of Polymer Film Thermal Control Materials on the Materials International Space Station Experiment (MISSE). NASA Technical Memorandum; 2002.
Hammerstrom AM, Youngstrom EE, Kaminski C, Marx LM, Fine ES, Gummow JD, Wright D, Banks BA, de Groh KK. MISSE PEACE Polymers: An International Space Station Environmental Exposure Experiment. NASA Technical Memorandum; 2001.
Hunt P. Return From Space: The PEACE Team Eight Years In. Hathaway Brown Alumnae Magazine. 2006; 2: 34-35.
NASA Image: ISS003E5863 - Close up of the experiment trays in MISSE, open and exposed to space.
NASA Image: ISS006E46361 - Oblique view of MISSE attached to the ISS airlock.
ISS004E8043 - Location of one of the MISSE PECs on the ISS.
NASA Image: ISS009E22432 - Close up of MISSE with Earth backdrop.
NASA Image: ISS009E22435 - MISSE on the ISS, over cloud tops.
NASA Image: ISS005E17107 - Oblique view of MISSE with Earth and space background.
NASA Image: STS105-346-007 - Astronaut Patrick G. Forrester, during the second STS-105 extravehicular activity, prepares to work with the Materials International Space Station Experiment (MISSE). The experiment was installed on the outside of the Quest Airlock during the first extravehicular activity (EVA) of the STS-105 mission. MISSE will collect information on how different materials weather in the environment of space.