Open Access

A transmission electron microscope study of Itokawa regolith grains

Earth, Planets and Space201466:71

https://doi.org/10.1186/1880-5981-66-71

Received: 27 February 2014

Accepted: 10 June 2014

Published: 15 July 2014

Abstract

Analyses of two olivine-rich particles from asteroid 25143 Itokawa returned by the Hayabusa mission (RA-QD02-0125 and RA-QD02-0211) show evidence for space weathering processes that occurred in the Itokawa regolith. Submicrometer impact-derived crystalline and glassy grains are observed adhering to the surfaces of the particles, including albite, orthopyroxene, olivine, augite, pyrrhotite, troilite, melt splashes, and melt spherules. Both particles are surrounded by 50- to 100-nm-thick disordered rims that are nanocrystalline, not amorphous, and compositionally similar to the grain cores. A pyrrhotite grain attached to RA-QD02-0125 also shows a disordered rim that is sulfur-depleted with nanophase Fe metal grains decorating the outermost surface. The structurally disordered rims on the Hayabusa particles likely result from atomic displacement damage from solar wind ions given the similarity of the rim thickness compared to the implantation depth of solar wind ions. The outermost few nanometers of the disordered rims are more Si-rich and Mg- and Fe-depleted relative to the cores of the grains and likely represent a minor accumulation of impact-generated vapors or sputter deposits. Nanophase Fe metal particles are present in the rim on RA-QD02-0211 but were not detected in the rim on RA-QD02-0125. Solar flare particle tracks are observed in RA-QD02-0211 but were not observed in RA-QD02-0125, suggesting short surface exposure times for the particles, on the order of approximately 103 to 104 years. This result implies that the optical effects of space weathering develop far more rapidly than was previously recognized.

Keywords

HayabusaItokawaSpace weatheringIrradiationMicrometeorite impactSolar flare tracksTransmission electron microscopy

Findings

Background

In a remarkable engineering achievement, the JAXA space agency successfully recovered the Hayabusa spacecraft in June 2010, following a non-optimal encounter and surface sampling mission to asteroid 25143 Itokawa. So far, several thousand regolith grains have been recovered from the collection canister (e.g., Tsuchiyama et al. 2011). These are the first direct samples ever obtained and returned from the surface of an asteroid, and the Hayabusa samples thus present a special opportunity to directly investigate the evolution of asteroidal surfaces, from the development of the regolith to the study of space weathering effects.

Preliminary analyses of the Hayabusa samples show that their mineralogy and composition are consistent with an LL5-LL6 ordinary chondrite parent body with some less equilibrated LL4 petrographic-type material (Nakamura et al. 2011). Because they directly sample the optical surface of Itokawa, the Hayabusa samples hold the key to resolving one of the most vexing problems in cosmochemistry: identifying the asteroidal sources of ordinary chondrites, the most abundant type of meteorites (Chapman 2004). The mineralogy of asteroids is largely inferred by matching their visible near-IR reflectance spectra with those obtained from meteorites. However, the optical properties of airless bodies in the Solar System are modified over time through exposure to the space environment by a group of processes known as space weathering. Space weathering modifies the reflectance spectra of materials by attenuating absorption features, changing the spectral slope (reddening), and lowering albedos. These spectral changes obscure the underlying mineralogy of the bodies to such an extent that direct spectral matches between asteroids and meteorites are generally difficult to impossible. Spacecraft encounters, laboratory modeling, and analyses of gas-rich meteorites and lunar samples have yielded insights into asteroidal space weathering processes, but the detailed chemical and mineralogical alteration of asteroidal surfaces is still uncertain (Gaffey 2010).

The surface of Itokawa has regions of both coarse and finer-grained material. The locations of the finer-grained material correspond to areas with gravitational potential lows; this material may have concentrated by seismic shaking (Miyamoto et al. 2007). The coarser regions that include large boulders with distinct morphologies, many of which appear to be breccias, suggest a complex collisional history (Noguchi et al. 2010). No well-defined large craters are present, but numerous micrometeroid impact pits (centimeter-sized and smaller) are observed on boulder surfaces in the highest-resolution images (Abe et al. 2006; Miyamoto et al. 2007; Takeuchi et al. 2009).

Abe et al. (2006) presented near-infrared spectral data for Itokawa showing surface variations of up to 10% in absorption band depths and albedo that result from differences in space weathering effects and physical properties (e.g., grain size). Hiroi et al. (2006) explored these variations through modeling and showed that different amounts of nanophase Fe metal (npFe0) produced via space weathering could account for the albedo and absorption depth variations. Noguchi et al. (2011) showed transmission electron microscope (TEM) data from several Hayabusa grains (olivine and pyroxene) with surfaces decorated with npFe0 as well as nanophase FeS grains (presumably troilite). These nanophase inclusions were all <5 nm in diameter, similar to the size distribution observed in vapor-deposited rims on lunar soil grains and much smaller than those in agglutinitic melt glass (Keller and Clemett 2001). Major questions remain regarding the origin of these space-weathered components - are they deposits of material sputtered from neighboring grains or vapors condensing from nearby micrometeorite impacts? Noguchi et al. (2011) described space-weathered surface layers up to 60-nm thick, similar to those on lunar soil grains that accumulate in 104 to 106 years. If the rims on the Hayabusa grains are formed through radiation processes, then one would also expect solar flare track densities to be similar to those in lunar grains with analogous rims (e.g., Zhang and Keller 2011).

While several Hayabusa grains have evidence of space weathering effects on their surfaces, they also have some unexpected properties (Noguchi et al. 2011, 2013). Here we report on our preliminary TEM measurements on two Itokawa samples.

Methods

We were allocated particles RA-QD02-0125 and RA-QD02-0211. Both particles were embedded in low-viscosity epoxy and thin sections (approximately 60-nm thick) were prepared using ultramicrotomy. High-resolution images, bright-field/dark-field images, and electron diffraction data were obtained using a JEOL 2500SE 200-kV field-emission scanning transmission electron microscope (STEM; JEOL Ltd., Tokyo, Japan) equipped with a Thermo-Noran thin-window energy-dispersive x-ray (EDX) spectrometer (Thermo Fisher Scientific, Hudson, NH, USA). The JEOL 2500SE STEM was used to measure chemical compositions using EDX as well as to acquire quantitative elemental maps (spectrum images) of individual grains. Spectrum images contain a high-count EDX spectrum in each pixel, enabling the determination of quantitative element abundances in addition to displaying the spatial distribution of major and minor elements. For the spectrum imaging, we rastered a 4-nm-diameter incident probe (9 nA) with a dwell time of 50 μs/pixel to limit beam damage and element diffusion during the experiment. The size of the rastered area was typically 256 × 204 pixels at a magnification that was optimized to limit over- or under-sampling with the 4-nm probe. Successive image layers of each region were acquired and combined in order to achieve better than 10% counting statistics for major elements in each pixel. Element line profiles were extracted from the spectrum images.

Results and discussion

Particle RA-QD02-0125 is an approximately 37-μm olivine single crystal that contains micrometer-sized inclusions of FeS and is surrounded by a microstructurally complex rim that shows a mottled contrast in TEM images. The particle is rounded in shape and has numerous submicrometer grains attached to its surface including pyrrhotite, albite, olivine, augite, orthopyroxene, and rare melt droplets. The composition of the olivine by TEM-EDX analyses is Mg1.4Fe0.6SiO4(Fo70) and is homogeneous. Solar flare tracks have not been observed within the olivine, and only an upper limit (<109 cm−2) can be placed on the track density given the limitation imposed by the size of the fragments in the microtome thin sections. The particle is surrounded by a continuous approximately 50-nm thick, structurally disordered rim that is nanocrystalline with minor amorphous material between crystalline domains (Figure 1). We have not observed npFe0 grains within the disordered rim. Compositional profiles obtained from the core of the grain through the rim show no major chemical differences except for the outermost 5 nm, which shows a slight Si enrichment (Figure 1). The adhering melt droplets are dominated by Fe sulfides, although a few melt droplets are immiscible mixtures of silicate glass (approximately chondritic) with Fe metal/Fe sulfide blebs (Figure 2).
Figure 1

Dark-field STEM image of the disordered rim in particle RA-QD02-0125 and corresponding element ratio profiles. A dark-field STEM image of the disordered rim in particle RA-QD02-0125 (left) and corresponding element ratio profiles from the core through the rim of the grain, indicated by the yellow arrow in the STEM image (right).

Figure 2

Bright-field STEM image of a melt droplet and RGB images showing the elemental distribution. A bright-field STEM image of a melt droplet on the surface of particle RA-QD02-0125 (left) and two composite RGB images showing the elemental distribution of the mixed silicate-sulfide melts (right).

One of the surface-adhering grains is a pyrrhotite grain that exhibits a strained rim on its exposed surface. Energy-dispersive x-ray mapping of the strained/disordered rim shows that the outer approximately 8- to 10-nm-wide zone is sulfur-depleted (Figure 3), with npFe0 grains (<5 nm) decorating the outermost surface (Figure 4). The microstructure of the sulfur-depleted layer on the pyrrhotite grain in RA-QD02-0125 is similar to that observed in troilite irradiated with 4 kV He+ ions to a fluence of approximately 1018 ions cm−2 (Loeffler et al. 2008; Keller et al. 2010). The pyrrhotite also displays a complex superstructure in its core that is absent in the sulfur-depleted rim (Figure 4). Prolonged ion irradiation has been shown to disorder pyrrhotite such that the superstructure reflections are lost (Christoffersen and Keller 2011).
Figure 3

High-resolution TEM, selected-area electron diffraction, and FFT pattern of pyrrhotite grain in RA-QD02-0125. A high-resolution TEM of the space-weathered pyrrhotite grain in RA-QD02-0125 (left). The outermost surface of the grain is armored with a thin layer of nanophase Fe metal grains. The selected-area electron diffraction from the core of the grain (labeled ‘core,’ upper right) shows strong superstructure reflections (arrowed) that are absent in the fast-Fourier transform (FFT) pattern from the rim (labeled ‘rim,’ lower right). In addition, the FFT pattern from the rim shows reflections that are consistent with the (110) spacings of iron metal (small dashed circles).

Figure 4

Quantitative element ratio plots across the space-weathered rim of a pyrrhotite grain. Quantitative element ratio plots across the space-weathered rim of a pyrrhotite grain exposed on the surface of particle RA-QD02-0125, which show a zone of sulfur depletion and iron enrichment in the outermost approximately 10 nm of the grain. Element ratio profiles were extracted from the spectrum images.

Particle RA-QD02-0211 is an angular, approximately 41-μm olivine single crystal that contains micrometer-sized inclusions of FeS and solar flare particle tracks, and also shows a structurally disordered, approximately 100-nm-thick rim (Figure 5). The solar flare track density is approximately 2 × 1010 cm−2 (Figure 6). The disordered rim is nanocrystalline with minor amorphous material between crystalline domains. Quantitative element maps show that the outermost approximately 10 nm of the disordered rim is Si-rich with lower Mg/Si and Fe/Si than the core of the grain and likely represents vapor- or sputter-deposited material (Figure 5). We observed regions within the rim that contain npFe0 particles (2 to 5 nm) in high-resolution TEM images, but they are not uniformly distributed throughout the rim (Figure 6).
Figure 5

Bright-field STEM image of the rim in particle RA-QD02-0211 and corresponding element ratio profiles. A bright-field STEM image of the disordered rim in particle RA-QD02-0211 (left) and corresponding element ratio profiles from the core through the rim of the grain, indicated by the yellow arrow in the STEM image (right). The element profiles show a thin outermost later that is Si-enriched.

Figure 6

Dark-field STEM image of solar flare tracks in particle RA-QD02-0211 and high-resolution TEM image. A dark-field STEM image of the disordered rim in particle RA-QD02-0211 showing solar flare particle tracks (left, arrowed) and a high-resolution TEM image of the rim showing tiny (<5 nm diameter) nanophase Fe metal particles in the rim (right).

Surface exposure

Solar flare energetic particles have a penetration depth of millimeter to centimeter and leave a trail of ionization damage in insulating materials. The solar flare track density correlates with exposure age as long as the grain was within a few centimeters of the parent body surface. From the analyses of lunar rock samples, the solar flare track production rate at 1 AU is approximately 6 × 105 year−1 for a 2π exposure (Blanford et al. 1975). Asteroid Itokawa has a semi-major axis of 1.324 AU and so we use the Blanford et al. rate for the Hayabusa samples. Based on this track production rate and assuming that the particles had a single stage exposure in the Itokawa regolith, the track density in particle RA-QD02-0211 corresponds to a minimum surface exposure of approximately 3 × 104 years. We can only place an upper limit constraint on RA-QD02-0125 of <103 years, given its lack of observable tracks. Low track densities are difficult to measure in microtome thin sections owing to the chatter and disruption that results from the cutting process. We have developed a focused ion beam approach to preparing thin sections of Hayabusa particles that will enable more accurate measurement of track densities in the approximately 108 to 109 cm−2 range (Berger and Keller 2014).

The structurally disordered rims on the Hayabusa particles likely result from atomic displacement damage from solar wind ions given the similarity of the rim thickness compared to the implantation depth of solar wind ions. If the short surface exposure times we observe in these two particles are typical of Itokawa regolith grains in general, it implies that the optical effects of space weathering develop far more rapidly than previous estimates (Vernazza et al. 2009) by several orders of magnitude.

Comparison to olivine grains from lunar soils

We also analyzed microtome thin sections of olivine grains from a 20- to 45-μm-size fraction of Apollo 17 soil sample 71501 to compare the microstructures of these grains to those that we observed in the Hayabusa grains. The 71501 soil is classified as submature and we observed a range of solar flare densities (approximately 1 to 5 × 1010 cm−2) in the grains. The 71501 olivines show disordered rims up to 100 nm wide that are highly strained, but only the outermost 10 to 15 nm is amorphous (Figure 7). We obtained compositional profiles across the rims of four olivines with similar track densities and all show an accumulation of elements that are not derived from the host olivine (e.g., Ca, Al, and Ti) in addition to a strong Si enrichment in the outer approximately 15 nm of the rims (Figure 7). The outmost layer likely represents a deposited layer from the condensation of impact-generated vapors similar to those observed on other lunar soil grains (Keller and McKay 1997). The underlying disordered material is compositionally similar to the core of the grain and is consistent with the solar-wind-damaged layers we observe on the Hayabusa olivine grains. Olivine grains from mature lunar soils show higher solar flare track densities (approximately 1011 cm−2) and more extensive development of damaged rims, thicker rims of vapor-deposited material, and a higher density of npFe0 particles.
Figure 7

Dark-field STEM image of the disordered rim in a lunar olivine grain and element profiles. A dark-field STEM image of the disordered rim in an olivine grain from lunar soil 71501 (left). The olivine grain contains solar flare tracks (red arrows) with a density similar to that in RA-QD02-0211. The disordered rim shows a similar microstructure as the Hayabusa olivine grains, except that the outermost 10 to 15 nm of the rim is dominated by vapor-deposited material enriched in Ca, Al, Ti, and Si as shown in the element profiles through the rim (right), indicated by the yellow arrow in the STEM image.

Conclusions

Both Hayabusa particles described here record the effects of space weathering processes on Itokawa, which include the presence of microstructurally disordered rims that are still largely crystalline and thin (5 to 10 nm) outer layers of Si-rich vapor-deposited materials. Noguchi et al. (2011, 2013) proposed that the disordered rims observed on Itokawa particles largely result from solar wind radiation damage with a minor component of vapor-deposited elements. We arrive at a similar conclusion for the particles we analyzed. We observed solar flare tracks in only one of the particles and the track density is consistent with short surface exposures. The Hayabusa grains appear to lack the abundant melt spherules and vapor deposits that are common in lunar soil grains with a similar exposure history.

Abbreviations

EDX: 

energy-dispersive x-ray

FFT: 

fast-Fourier transform

npFe0

nanophase Fe metal

STEM: 

scanning-transmission electron microscope

TEM: 

transmission electron microscope.

Declarations

Acknowledgements

This research was supported by a grant to LPK from the NASA Laboratory Analysis of Returned Samples (LARS) program. We gratefully acknowledge the samples allocated for this study from JAXA and the Hayabusa Curation Facility.

Authors’ Affiliations

(1)
Robert M Walker Laboratory for Space Science, Code KR, Astromaterials Research and Exploration Science, NASA Johnson Space Center
(2)
GeoControl Systems, Inc. - Jacobs JETS contract - NASA Johnson Space Center

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Copyright

© Keller and Berger; licensee Springer. 2014

This article is published under license to BioMed Central Ltd. This is an Open Access article distributed under the terms of the Creative Commons Attribution License (http://creativecommons.org/licenses/by/4.0), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly credited.