# A dehydrated space-weathered skin cloaking the hydrated interior of Ryugu

Takaaki Noguchi, Toru Matsumoto, Akira Miyake, Yohei Igami, Mitsutaka Haruta, Hikaru Saito, Satoshi Hata, Yusuke Seto, Masaaki Miyahara, Naotaka Tomioka, et al.

► To cite this version:

Takaaki Noguchi, Toru Matsumoto, Akira Miyake, Yohei Igami, Mitsutaka Haruta, et al. A dehydrated space-weathered skin cloaking the hydrated interior of Ryugu. Nature Astronomy, 2022, Nature Astronomy, 7, pp.170-181. 10.1038/s41550-022-01841-6. hal-04138464

HAL Id: hal-04138464

https://hal.univ-lille.fr/hal-04138464

Submitted on 23 Jun 2023

HAL is a multi-disciplinary open access
archive for the deposit and dissemination of sci-
entific research documents, whether they are pub-
lished or not. The documents may come from
teaching and research institutions in France or
abroad, or from public or private research centers.

L'archive ouverte pluridisciplinaire HAL, est
destinée au dépôt et à la diffusion de documents
scientifiques de niveau recherche, publiés ou non,
émanant des établissements d'enseignement et de
recherche français ou étrangers, des laboratoires
publics ou privés.

<figure><img src="image_1.png" /></figure>

Distributed under a Creative Commons Attribution 4.0 International License
<figure><img src="image_2.png" /></figure>

# A dehydrated space-weathered skin cloaking the hydrated interior of Ryugu

Received: 26 April 2022

Accepted: 24 October 2022

Published online: 19 December 2022

<figure><img src="image_3.png" /></figure>

Check for updates

A list of authors and their affiliations appears at the end of the paper

Without a protective atmosphere, space-exposed surfaces of airless Solar System bodies gradually experience an alteration in composition, structure and optical properties through a collective process called space weathering. The return of samples from near-Earth asteroid (162173) Ryugu by Hayabusa2 provides the first opportunity for laboratory study of space-weathering signatures on the most abundant type of inner solar system body: a C-type asteroid, composed of materials largely unchanged since the formation of the Solar System. Weathered Ryugu grains show areas of surface amorphization and partial melting of phyllosilicates, in which reduction from $Fe^{3+}$ to $Fe^{2+}$ and dehydration developed. Space weathering probably contributed to dehydration by dehydroxylation of Ryugu surface phyllosilicates that had already lost interlayer water molecules and to weakening of the 2.7 µm hydroxyl (–OH) band in reflectance spectra. For C-type asteroids in general, this indicates that a weak 2.7 µm band can signify space-weathering-induced surface dehydration, rather than bulk volatile loss.

Solar wind irradiation and high-velocity micrometeoroid bombardment dominate space weathering¹,² for all airless bodies. However, the effects of these processes vary substantially, depending on the specific class of body. The solar wind is a plasma composed mainly of low-energy protons and electrons streaming from our Sun¹⁻³, which induces radiation damage, including amorphization of silicates and formation of nanophase metallic iron particles (npFe⁰). In contrast, micrometeoroids are interplanetary dust particles that impact airless surfaces at hypervelocities⁴, resulting in cratering, melting and vapour deposits, and sometimes also amorphous silicates and npFe⁰. Space-weathering products of two anhydrous bodies, the Moon and the S-type asteroid Itokawa, have been investigated extensively⁵⁻¹⁴. These studies revealed that nanometre-sized metallic Fe particles (npFe⁰), formed via space weathering, resulted in weakened absorption features in visible to near-infrared reflectance. In contrast, it has been unclear what role npFe⁰ plays in the reflectance properties of dark (C- and D-type) asteroids¹,².

Space-weathering modification of reflectance spectra features from airless bodies makes identifying a direct link between asteroids and specific meteorite classes based on composition and mineralogy difficult. The Hayabusa mission of the Japan Aerospace

Exploration Agency (JAXA) revealed the connection between visible to near-infrared reflectance spectra from S-type asteroids and ordinary chondrite meteorites⁵, with the difference largely attributable to the role of nanophase particles. However, laboratory experiments that mimic solar wind irradiation and micrometeoroid impact on C-type asteroids show a lack of detectable production of npFe⁰, with some spectra reddening (a positive change in spectral slope) and others bluing (just the opposite)¹⁵⁻²⁰. Thus, the observed change of spectral slope and absorption band in reflectance spectra of C-type asteroids compared with carbonaceous chondrites meteorites is difficult to interpret¹⁵⁻²⁰. JAXA's Hayabusa2 spacecraft observed spectral variation on asteroid Ryugu²¹⁻²⁴ thought to be related to space weathering. Our studies of Ryugu samples offer the first opportunity to directly link the spectral variation to the space-weathering-induced physical and chemical alteration of regolith on C-type asteroids.

## Results

### Surface modifications found on Ryugu grains

The mineralogy of most Ryugu grains investigated by (scanning) transmission electron microscopy is similar to that of CI chondrites²⁵, which are the most chemically primitive materials in the Solar System²⁶,

<figure><img src="image_4.png" /></figure>

e-mail: noguchi.takaaki.2i@kyoto-u.ac.jp
<figure><img src="image_5.png" /><figcaption>**Fig. 1** | **Secondary electron images of Ryugu grains showing surface modifications related to space weathering.** *a*, The grain C0105-03004800 was collected at the second touchdown site. It is composed of two parts showing different types of space weathering: a frothy layer and a smooth layer. Enlarged images of the two boxed areas on this grain are shown in the insets at the upper right (frothy layer) and the lower left (smooth layer) corners of *a*.</figcaption></figure>

*b*, The grain A0104-02203700 was collected at the first touchdown site. The frothy layer partially covers the smooth layer on the left-hand side of the image. The boundary between two types of layers is indicated by a dashed curve. The frothy layer has many burst vesicles. A melt splash, located at the lower centre of the image, is attached to the surface of the frothy layer.

consistent with other recent studies²⁷⁻³¹. Therefore, to understand the space weathering of Ryugu grains is to understand the weathering of the most chemically primitive Solar System material.

More than 500 grains (average diameter ~71 µm) collected at the first touchdown (landing) site (TD1) and >300 grains (average diameter ~57 µm) collected at the second touchdown site (TD2) were investigated for surface modifications potentially related to space weathering. Recognizable surface modifications of the phyllosilicate-rich matrix were found in ~6% of the observed grains from TD1 and ~7% from TD2 (Extended Data Fig. 1). The surface modifications of grains differ considerably from those from the Moon and Itokawa because the most abundant phases in Ryugu grains are hydrated sheet silicates (phyllosilicates), not anhydrous silicates (for example, olivine). Several distinct surface modifications are observed, including smooth layers, frothy layers, melt splashes and their combinations (Fig. 1 and Extended Figs. 2 and 3). We also examined three millimetre-sized grains (A0067, A0094 and A0058) that have surface modifications related to space weathering.

## Smooth layers on Ryugu grains

Approximately 5% of the observed grains from TD1 and ~3% from TD2 have a smooth layer, evident as a thin (<100 nm) continuous smooth sheet covering the surface. Some of these layers contain vesicles of <50 nm diameter that intersect the surface (Fig. 2a and Extended Data Fig. 2a). Partial detachment of the smooth layers is observed in some grains (Extended Data Fig. 4). Electron diffraction reveals that smooth layers are almost completely amorphous (Extended Data Fig. 2d). Atomic ratios among major cations of the smooth layers are indistinguishable from those of the phyllosilicate-rich matrix (Fig. 3a). Most Fe in the smooth layer is Fe²⁺, but most Fe in the underlying phyllosilicates is Fe³⁺ based on the Fe L₃-edge electron energy-loss spectroscopy (EELS), and Fe L₃ and Fe K X-ray absorption near-edge spectroscopy (XANES) (Fig. 3b and Supplementary Table 1), indicating that the smooth layer is more reduced than the matrix.

An unweathered Ryugu grain that was irradiated with 4 keV He⁺ at a fluence of 1.3 × 10¹⁸ ions cm⁻² to simulate space weathering shows a surface morphology and an internal structure that are very similar to those of the smooth layers (Figs. 1a and 2a, and Extended Data Fig. 2) of the bonafide space-weathered grains. On lunar and Itokawa grains, smooth surfaces were formed by micrometeoroid impacts and subsequent redeposition. On Ryugu grains, in contrast, we found a ~10-nm-thick

vapour deposit on top of a smooth layer of only one grain (Extended Data Fig. 5), suggesting that 'vapour deposition' does not play an important role in forming smooth layers. Instead, the laboratory-irradiated Ryugu grain indicates that solar wind irradiation probably played an important role in modifying the surface of the phyllosilicate-rich matrix, and the smooth layers represent space weathering induced by solar wind irradiation.

## Frothy layers and melt splashes on Ryugu grains

Frothy layers are found on ~1% of the observed grains from TD1 and ~2% of grains from TD2, which are composed of silicate glass containing abundant embedded vesicles ~0.1- to ~1 µm wide and numerous submicroscopic (<200 nm) rounded Fe-Ni sulfide beads (Fig. 2b and Extended Data Fig. 3). The internal structure suggests that silicate and Fe-Ni sulfides were melted and immiscibly separated into silicate and sulfide melts and that vesiculation occurred during melting. The frothy layers have higher Fe and lower Si+Al and Mg than the interior phyllosilicate-rich matrix (Fig. 3c,d), irrespective of the size of the grain on which they reside. The frothy layer is also more reduced in Fe than the underlying phyllosilicates (Fig. 3e-h). The Fe-Ni sulfide beads, composed of pyrrhotite and pentlandite with diameters from ~200 to <10 nm, are ubiquitous within frothy layers (Extended Data Fig. 6a-d). While most microphase sulfides are probably immiscibly separated as droplets during melting, the ~10-nm-sized nanophase sulfide shown in Extended Data Fig. 6d may be a vapour deposit, consistent with previous laser irradiation experiments¹⁵,¹⁶. We identified no npFe⁰ within the frothy layers investigated. However, on the surface of a frothy layer, we found an aggregate composed of npFe⁰ and troilite (stoichiometric FeS) (Extended Data Fig. 6e-h). Porous apatite, dolomite and magnetite occur in some frothy layers and are believed to be relict minerals that survived melting. In addition, a frothy layer is observed with abundant blisters (vesicles just below the surface) (Fig. 2c). Melt splashes (<10 µm across) are found on <1% of the observed grains from TD1 and ~1% of grains from TD2, and are attached to Ryugu grains with and without detectable surface modifications (Fig. 1b).

## Exceptionally rare npFe⁰ on Ryugu

The exceptionally low abundance of npFe⁰ in Ryugu grains is in stark contrast to lunar and Itokawa surface samples, which contain abundant npFe⁰ in both radiation-damaged layers on ferromagnesian
<figure><img src="image_6.png" /><figcaption>**Fig. 2 | Cross-sections of three Ryugu grains showing typical surface modifications on the phyllosilicate-rich matrix.** *a*, The cross-section A0104-02306901 was prepared from the grain A0104-02306900 collected at the first touchdown site. It has a smooth layer that forms a ~100-nm-thick continuous layer covering the surface of the grain. The phyllosilicate-rich matrix is present below the smooth layer. A yellow dashed curve indicates the cross-section of the sample surface. The boundary between the smooth layer and the phyllosilicate-rich interior is indicated by an orange dashed curve. *b*, The cross-section C0105-03003701 was prepared from the grain C0105-03003700 collected at the second touchdown site. A frothy layer containing abundant vesicles (darker</figcaption></figure>

circles) and <50-nm-size brighter spots (Fe-Ni sulfide beads) covers the surface of this grain. The thickness of the frothy layer varies considerably locally from <100 nm to >500 nm. A yellow dashed curve indicates the cross-section of the sample surface. C-depo denotes carbon depositions to protect the surface of the samples during FIB processing. *c*, An enlarged image of a frothy layer in a cross-section A0104-02802202. The frothy layer contains many tiny (<20 nm across) blisters (vesicles just below the surface) on its surface. These are high-angular dark-field scanning transmission electron microscope images, in which materials with higher average atomic numbers are brighter than those with lower average atomic numbers.

silicates<sup>7–9,11,13,14</sup> and in vapour deposit layers produced by micrometeoroid impacts<sup>32,33</sup>. While nano- to microphase Fe-bearing sulfides are ubiquitous in all the frothy layers on the Ryugu grains investigated, no interior $npFe^0$ was found. The reduction effect of space weathering might be insufficient to form $npFe^0$ from abundant Fe<sup>3+</sup> contained in phyllosilicates in Ryugu grains (Supplementary Table 1). In addition, the -OH in phyllosilicates may hinder the reduction of Fe. These results are similar to laboratory experiments where in situ X-ray photoelectron spectroscopic analyses of H<sup>+</sup> and He<sup>+</sup> irradiated Murchison CM2 chondrite showed that partial reduction of surface Fe to lower oxidation states occurred with simulated solar wind exposure<sup>19</sup>. Nano- to microphase Fe sulfide is also common in both H<sup>+</sup> and He<sup>+</sup> irradiated Murchison CM2 chondrite and laser-irradiated Murchison. These results are consistent with our observations, although Murchison is a CM chondrite with significantly different mineralogy and Fe content than Ryugu. We suggest that it is unlikely that $npFe^0$ contributes significantly to the observed spectral variability on Ryugu, but submicroscopic Fe-Ni sulfides may contribute to this variability.

## More abundant impact melts on Ryugu than on Itokawa

Among Itokawa grains, only 2 out of 590 grains (0.3%) show melted structures<sup>34</sup> that resemble the frothy layers found on ~1% to 2% of Ryugu grains. The calculated dry and wet solidus temperatures of Ryugu material<sup>28</sup> are approximately the same (862 and 867 °C) under $-10^5$ Pa because of the low $H_2O$ solubility in the melt at low ambient pressures<sup>35,36</sup>, which indicates that high porosity may explain the higher abundance of impact melts among Ryugu grains relative to Itokawa grains. Ryugu grains have high average microporosity (~28%, measured by synchrotron radiation nanotomography) and may have experienced higher post-shock temperature than low-porosity (1.5–1.9%)<sup>37</sup> Itokawa grains since porosity collapse by shock compression causes a large temperature increase<sup>38</sup>. Both the surface morphology and internal structure of laser irradiation products<sup>15,17</sup> that simulate shock heating by micrometeoroid impacts are similar to those of the frothy layers (Figs. 1 and 2b, and Extended Data Fig. 3). Thus, one of the major formation mechanisms of the frothy layers might be frictional heating among loose regolith grains by meteoroid impact. In addition, in situ formation of melt by micrometeoroid impact onto the grains and deposition of melt formed by a neighbouring impact event would also contribute to the formation of the

frothy layers. The observed small melt splashes might be ejecta formed during micrometeoroid cratering.

## Discussion

We estimated the timescale of formation of the smooth layer on Ryugu grain surfaces. The fluence of the ion irradiation experiment (Extended Data Fig. 2c) is equivalent to $-3 \times 10^3$ years at 1.2 au (the semimajor axis of Ryugu’s orbit) by considering the solar wind flux density at 1 au, $3-5 \times 10^8$ ions cm$^{-2}$ s$^{-1}$ (ref. 39), and the average He/H ratio in the solar wind, 0.045 (ref. 40). We found an olivine crystal exhibiting a radiation-damaged rim and containing solar flare tracks with a number density of $-2 \times 10^8$ cm$^{-2}$ (Extended Data Fig. 7), which corresponds to an $-6 \times 10^3$ year dwell time for the grain within ~1 mm from the surface, based on lunar sample studies<sup>41</sup>. A thin (~20 nm) smooth layer on the phyllosilicate matrix was found near the olivine grain in the same sample. These independent results suggest that it may take $>3 \times 10^3$ years to form a detectable smooth layer on phyllosilicates. The exposure age of the smooth layer-covered surface of Ryugu grain A0067 is estimated to be $3 \times 10^4$ years, calculated by its crater population assuming they formed by interplanetary meteoroid impacts<sup>4</sup> (Extended Data Fig. 8). In comparison, studies of craters on Itokawa grains<sup>42,43</sup> showed that most submicrometre-scale craters were probably formed by secondary impacts of ejecta excavated from larger craters. If such impacts occurred on Ryugu, then the formation of the smooth layer would require less time. In either scenario, the upper limit on time required to develop the smooth layer is $3 \times 10^4$ years, which is consistent with the above estimate.

A frothy layer with abundant blisters (Fig. 2c) suggests that, after irradiation by the solar wind, blisters formed during subsequent heating, probably related to micrometeoroid impact, which induced the release of trapped solar wind gas species. This is consistent with steady and continual solar wind irradiation through time, while micrometeoroid bombardment occurs sporadically.

Some grains have partially exfoliated smooth layers (Extended Data Fig. 4), which suggests that smooth layers can detach. Detachment of smooth layers may explain the low abundance (~7%) of investigated grains with space-weathered features. In addition, the fragility of Ryugu grains may be another important factor that reduces the abundance of grains with observable space weathering. Among 6 large (millimetre-sized) grains collected at TD1,
~66% (4 of 6) show evidence of space weathering based on the field emission scanning electron microscope (FE–SEM) observation at Kyoto and Tohoku Universities, which is much higher than 6–7% for <100-µm-sized grains (Extended Data Fig. 1). The difference can be interpreted as indicating that most fine-grained samples are fragments of larger grains. Exfoliation and destruction could occur by thermal fatigue and meteoroid impacts on Ryugu. In addition, they could also occur during sampling and transportation to Earth, or even during handling processes.

To quantify the amount of —OH in the Ryugu grain surfaces, we used energy dispersive X-ray spectroscope (EDS) measurements of focused ion beam (FIB) cross-sections of weathered and pristine grains (Fig. 4) to determine oxygen to cation ratios, correcting for S-bonded Fe and Ni. The ratio of oxygen to cations bonded with oxygen shows that, in pristine grains, interlayer H₂O molecules in saponite are largely absent from a mixture of saponite and serpentine, but structural —OH groups in the phyllosilicates are retained (Fig. 4a). This estimation of —OH abundance is consistent with the thermogravimetric analysis of Ryugu grains²⁸.

Space weathering over the length of Ryugu's residence time at near-Earth orbits after its orbital shift from the main belt, which is thought to be several megayears based on noble gas data¹⁴, may also play an important role in the removal of interlayer H₂O from saponite. During the prolonged exposure to interplanetary space, even structural —OH groups might be removed from a mixture of serpentine and saponite that has lost its interlayer H₂O. This may occur by decomposition of saponite and serpentine by dehydroxylation, that is, a decomposition to anhydrous compounds and liberated H₂O molecules. However, we note that the solar wind would probably penetrate grains very heterogeneously owing to the high microporosity of the phyllosilicate-rich matrix of Ryugu grains.

A substantial amount of structural —OH has been lost in smooth layers (Fig. 4b). Almost all the structural —OH has been lost in frothy layers and also in the phyllosilicates just below frothy layers (Fig. 4c,d). These data suggest that more structural —OH in phyllosilicates is removed through dehydroxylation as space weathering proceeds (Fig. 5). A portion of structural —OH in phyllosilicates just below the smooth layer also appears to be absent (Fig. 4b), and sporadic amorphization of phyllosilicates is observed. Solar wind particles could penetrate to such depths, in regions of highest porosity of the phyllosilicate-rich matrix (Fig. 2a), and potentially promote dehydroxylation reactions. In addition, phyllosilicates just below the frothy layer lost most of their structural —OH (Fig. 4c, d). Frictional heating induced by meteoroid impacts and the formation of new surfaces by thermal stress⁴⁵ could promote dehydration by dehydroxylation.

A conceptual illustration (Fig. 5) shows the development of solar wind implantation, dehydration by dehydroxylation of phyllosilicates and progressive coverage of anhydrous silicate-rich melt on a Ryugu grain. Once a surface of a Ryugu grain is exposed to interplanetary space, the effects of solar wind irradiation start to accumulate at and near the surface. As time passes, the gradual accumulation of solar wind radiation damage and phyllosilicate dehydroxylation form the

smooth layer on its surface, which means that partial dehydration occurs in the smooth layer as shown in Fig. 4b. Because the effects of solar wind are constrained by the limited kinetic energy of solar wind particles³, the thickness of the smooth layer seldom exceeds ~100 nm. Sometimes, a very thin (~10 nm) vapour deposition may be formed on its surface as shown in Extended Data Fig. 5, although it is not illustrated in Fig. 5.

In contrast, formation of impact melts (frothy layers and melt splashes) is an intermittent process. The impact melt can be formed in several ways: in situ formation of melt by micrometeoroid impact melt onto the grain, deposition of melt formed by a neighbour impact event and in situ melting by frictional heating among porous regolith. In this conceptual illustration, partial coverage by impact melt occurred twice, at times I and II. After the coverage by a frothy layer, the effects of solar wind irradiation start to accumulate in the frothy layer. If another subsequent heating event or impact occurs, resulting in the deposition of another melt deposit, the implanted solar wind gases in the frothy layer may form blisters (Fig. 2c). The frothy layers (impact melts) are almost anhydrous because they were formed by high-temperature processing, which is indicated in Fig. 4c,d.

In Fig. 5, the change of colour from light blue via orange to yellow represents the progress of dehydration. The surface material of asteroid Ryugu becomes covered by nearly anhydrous material over time. After a long period of space exposure, dehydration by dehydroxylation of the phyllosilicates proceeds below both the smooth layers and the frothy ones, as shown in Fig. 4. We measured the chemical compositions of the frothy and smooth layers and the underlying phyllosilicate-rich matrix from the surface of grains to ~1.5 µm below the surface, demonstrating that the effects of dehydration by dehydroxylation extend to at least that depth in space-weathered Ryugu grains. Note that the natural overturn, or gardening, of regolith grains on the asteroid parent body interrupt the schematic history of space weathering so that the space-weathering processes on any one grain do not necessarily progress as shown in Fig. 5.

Strong absorption in the 3 µm region of the reflectance spectra¹,² is attributed to phyllosilicates and other —OH-rich minerals as well as H₂O ice. Among these materials, the 2.7 µm band is ascribed to —OH¹,². Dehydroxylation from phyllosilicates may weaken the band. Spacecraft-based measurements of the reflectance spectra obtained at the artificial crater at TD2 on Ryugu normalized to a surface standard spectrum show a 2.7 µm band depth inside the crater that is ~5% stronger than that of the standard spectrum and those from outside the crater¹⁶. These observations suggest that more —OH is preserved in the subsurface material that was exposed by the formation of the artificial crater. Additional factors such as grain size, porosity and viewing geometry can also affect reflectance spectra¹⁷⁻¹⁹. Considering all these factors together, we hypothesize that the 2.7 µm band features are potential indicators of the degree of space weathering for C-type asteroids.

In addition to the band depth, band shift could be an important indicator of the degree of space weathering, but a definitive interpretation of shift is so far elusive, with different experiments indicating

**Fig. 3 |** *Elemental compositions and redox states of Fe in a smooth layer, frothy layers and the interior phyllosilicates.* *a*, The ternary [Si+Al]-Mg-Fe atomic-ratio diagram shows that elemental compositions of a smooth layer are indistinguishable from those of the interior phyllosilicates in the cross-section sample A0104–02306901. *b*, However, a Fe L₃-edge peak in EELS spectra shows that Fe²⁺ is enriched in the smooth layer, which means that Fe³⁺ in the smooth layer is reduced to Fe²⁺. The EELS spectra were obtained from the upper (U) and lower (L) parts of the smooth layers, the upper (U) and lower (L) areas around the boundary between the smooth layer and the interior phyllosilicates, and the interior phyllosilicates. *c*, By contrast, the frothy layer in the cross-section sample C105–03003700 is more enriched in Fe relative to [Si+Al] and Mg than the interior phyllosilicates. *d*, The same compositional relationship is shown

between the frothy layer in the cross-section sample A0058–C2001 and the interior phyllosilicates. The whole grain sizes of these samples are quite different. C105–03003700 and A0058–C2001 are ~30 µm and ~3 mm across, respectively. *e–h*, Fe³⁺ in the frothy layers is also reduced to Fe²⁺, *e*, Fe L₃-edge peak spectra obtained by EELS. The spectra were obtained from the frothy layer, the boundary area between the frothy layer and the interior phyllosilicates, and the upper and lower areas of the interior phyllosilicates. *f*, Fe L₃-edge peak spectra obtained by STXM–XANES. *g, h*, Fe K-edge spectra (*g*) and background-subtracted pre-edge peak spectra (*h*) obtained by XANES. Int. phyllosilicates, phyllosilicates in the interior of a sample. Serp and Sap in *a, c*, and *d* are the abbreviations for serpentine and saponite, respectively.
different shift directions. Measurements of the Ryugu artificial crater showed a small shift, but it is difficult to link this to measurements at the scale of individual particles. Several experiments have tried to simulate space weathering induced by solar wind irradiation or micrometeoroid impact to assess impact on spectral features¹⁵⁻²⁰,⁴⁸⁻⁵⁰.

However, none yet fully satisfy realistic space-weathering conditions and include coordinated near-infrared spectroscopy, scanning electron microscopy and transmission electron microscopy on the irradiated samples. Further studies are greatly needed to accurately reproduce the features of space weathering of Ryugu samples.

<figure><img src="image_7.png" /></figure>

<figure><img src="image_8.png" /></figure>

<figure><img src="image_9.png" /></figure>

<figure><img src="image_10.png" /></figure>

<figure><img src="image_11.png" /></figure>

<figure><img src="image_12.png" /></figure>

<figure><img src="image_13.png" /></figure>

<figure><img src="image_14.png" /></figure>
<figure><img src="image_15.png" /></figure>

**Fig. 4 | Histograms of atomic ratios of oxygen to the cations bonded to oxygen in phyllosilicates, a smooth layer and frothy layers.** A mixture of saponite without interlayer H₂O molecules and serpentine has a range of ratios represented by green bands. If a mixture of saponite and serpentine is decomposed into an anhydrous compound, it has a range of ratios represented by red bands. In order to calculate the atomic ratios of oxygens to the cations bonded to oxygen in phyllosilicates, we subtracted the cations bonded to sulfur (S), which were calculated based on the assumption that the ratio of the S-bonded Fe and Ni ions to S is unity for simplicity. **a**, Phyllosilicates in a non-space-weathered grain contain almost no interlayer H₂O but preserve structural –OH groups. **b**, A smooth layer lost a considerable amount of structural –OH groups and phyllosilicates just below the smooth layers partially lost structural –OH groups. **c**, Phyllosilicates just below the frothy layer have lost the structural –OH groups considerably. **d**, Phyllosilicates just below the frothy layer have

lost almost all the structural –OH groups. Because the frothy layers have even lower ratios than the red bands, they are also anhydrous. Their very low ratios may be related to their high abundance of embedded Fe-Ni sulfide. The ratio at the right end of the green belts is 1.8, which is calculated from the generalized chemical formula of serpentine Y₆Z₄O₁₀(OH)₈. O/(Y + Z) = 18/10 = 1.8. The ratio at the left end of the green belts is 1.64, which is calculated from the generalized chemical formula of saponite with no interlayer H₂O molecules X₀.₆Y₀Z₈O₂₀(OH)₄. O/(X + Y + Z) = 24/14.6 = 1.64. The ratio at the right end of the red belts is 1.5, which is calculated from the generalized chemical formula of the dehydrated decomposition product of saponite X₀.₆Y₀Z₈O₂₂. O/(X + Y + Z) = 22/14.6 = 1.5. The ratio at the left end of the red belts is 1.4, which is calculated from the generalized chemical formula of the dehydrated decomposition product of serpentine Y₆Z₄O₁₄. O/(Y + Z) = 14/10 = 1.4.

In the case of Ryugu, strong thermal alteration on the parent body²³,⁴⁶ can be excluded as the cause for surface dehydration because phyllosilicates in nearly all Ryugu samples preserve their structural –OH²⁷,²⁸. Therefore, either space weathering, solar radiative heating or both could have caused these differences²². If the surface material of Ryugu was heated by solar radiation²³, all the grains and boulders from the surface to 10 to 100 cm deep must have experienced heating and dehydration throughout their interiors²³. However, no heavily heated grains were found in this and other studies²⁸⁻³¹,⁴⁴. Therefore, solar radiation heating is unlikely to have caused the decrease of the 2.7 µm feature. As described previously, space-weathered Ryugu grains have an almost completely dehydrated surface and an interior with no evidence of thermal metamorphism. If the surface material contains a higher number of space-weathered grains than the subsurface material, as expected based on regolith gardening processes, the spectral differences before and after crater formation can be explained by different amounts of space-weathered grains in the surface and subsurface material of Ryugu. Therefore, it is likely that space weathering played an important role in the dehydration of Ryugu's surface.

We note that ~40% of C-type asteroids do not show the 2.7 µm band features (sometimes generally referred to as the 3 µm band) and several interpretations were proposed for their origins⁵¹⁻⁵³. Based on our data from Ryugu grains, we propose that the absence of the 2.7 µm absorption band can be at least partly explained by surface dehydration due to space weathering. Gradual covering by anhydrous amorphous silicate with longer exposure to space weathering was proposed by a radiative transfer study of Bennu²⁰. The clear 2.7 µm feature on carbonaceous asteroid Bennu⁵⁴ explored by NASA's OSIRIS-REx spacecraft may be related to weaker space weathering experienced by Bennu than Ryugu or due to differences in phyllosilicate species and their chemical compositions. Suppression of the 'water band' by space weathering of C-type asteroid surfaces has implications for interpreting remote spectra, the first and least expensive tool for identifying water resources for eventual in situ resource utilization in space. Asteroids that appear dry on the surface may be water-rich, potentially requiring revision of our understanding of the abundances of asteroid types and the formation history of the asteroid belt.
<figure><img src="image_16.png" /></figure>

**Fig. 5 | A conceptual illustration showing the development of two types of space weathering with dehydration by dehydroxylation observed on a Ryugu grain.** Once a surface of a Ryugu grain is exposed to interplanetary space, the effects of solar wind irradiation start to accumulate at and near the surface, which is shown as hatched areas labelled as the 'Solar wind implanted zone' in the figure. As time passes, the gradual accumulation of solar wind radiation damage and phyllosilicate dehydroxylation form the smooth layer on its surface with a thickness that seldom exceeds -100 nm. In contrast, the formation of impact melts (frothy layer, cratering and melt splash) is an intermittent process. In this conceptual illustration, partial coverage by impact melt occurred twice at times I and II. The change of colour from light blue via orange to yellow represents

the progress of dehydration. As shown in Fig. 4, the impact melts are almost anhydrous. Therefore, the surface of the model grain is covered by both nearly anhydrous impact melts and dehydroxylated amorphized phyllosilicates. As a result, the surface of the asteroid Ryugu becomes covered by anhydrous material over time. After a long period of space exposure, dehydration by dehydroxylation of the phyllosilicates proceeds below both the smooth layers and the frothy ones. Note that the natural overturn, or gardening, of regolith grains on the asteroid parent body interrupt the schematic history of space weathering so that the space-weathering processes on any one grain do not necessarily progress as shown in Fig. 5.

# Methods

## Sample transfer and preparation for analyses

To preserve the pristine nature of the returned samples, the samples were prepared and analysed without cleaning, washing or other procedures that could introduce terrestrial contamination. The sample catcher has three separate chambers to store samples collected in the different locations on Ryugu. Chambers A and C contain samples collected from the first and second touchdown sites (TD1 and TD2), respectively. Air-tight sample transfer holders³⁵ were used to bring samples from JAXA to Kyoto University. The allocated grains were handled in an N₂-filled glove box at Kyoto University. Ryugu grains from both chambers were attached to Au plates on pin stubs with small amounts of epoxy glue. About 250 grains and about 40 thin foil sections prepared by FIB were investigated at the 21 hub universities and laboratories.

## FIB-scanning electron microscopy

Observation and sample preparation at Kyoto University are as follows. Surface morphology of about 300 grains was observed by a JEOL JSM-7001F FE-SEM. We observed them 15 pA current and 2 kV acceleration voltage. FIB sections were prepared using a Thermo Fisher Helios FIB-SEM. Selected areas were cut out with a 30 kV Ga⁺ ion beam. Before the extraction, the target areas were Pt-C coated by a 2 kV electron beam. Then, Pt-C was deposited on the target areas by 16 or 30 kV Ga⁺ ion beams. The sections mounted on the TEM grids were thinned

to a thickness of 50 to 200 nm on the 12 or 16 kV Ga⁺ ion beams. The damaged layers were removed using a 2 kV Ga⁺ ion beam. About 70 FIB sections were prepared and investigated by the team. In parallel with the above work, we also performed FIB and (scanning) transmission electron microscopy under air-free conditions using an air-tight FIB-SEM sample transfer holder and a double tilt LN₂ Atmos Defend Holder (Mel-Build Corporation) at Kyushu University. Another air-tight sample holder was used to transfer the samples. An Ar-filled glove box was used for sample handling. A Thermo Fisher Scios FIB-SEM was used for the observation of about 500 grains and for FIB processing of space-weathered grains. The conditions of the FIB processing are similar to those at Kyoto University.

## (Scanning) transmission electron microscopy

At Kyoto University, a JEOL JEM 2100 F (scanning) transmission electron microscope (SEM) operating at 200 kV equipped with a JEOL JED-2300T EDS was used. The ζ-factor method³⁶ was used for quantitative analysis. Electron diffraction maps with quasi-parallel illumination were acquired using a Gatan Orius200D camera. At Kyushu University, a monochromatized and Cs aberration-corrected Thermo Fisher Titan Cubed G2 operating at 300 kV, equipped with four-quadrant windowless super-X silicon drift detector EDS and Gatan Quantum 965 image filter (GIF) for EELS was used. The probe current was less than 200 pA for TEM observation and ~60 pA for STEM observation as well as energy
dispersive X-ray spectroscopy and EELS. The typical energy resolution of this EELS analysis was 0.4 eV. The energy dispersion was 0.1 eV per channel at the camera for EELS, which was calibrated by using standard samples of fayalite (Fe₂SiO₄) and synthetic Co olivine (Co₂SiO₄). EELS mapping was conducted using ~6 nm × ~6 nm square pixels and the acquisition time per pixel was 100 ms. The obtained EELS spectra were averaged over several hundred pixels (~10,000 nm²) to improve the signal-to-noise ratio. The Fe³⁺/ΣFe ratio was quantified by the Fe L₃ peak as follows. The background was first subtracted using a power-law fit over an energy range of 20 eV, then the spectrum was decomposed to Fe²⁺ and Fe³⁺ components by multiple linear least-squares fitting based on two standard spectra obtained from fayalite (Fe₂SiO₄) and Fe₂O₃ in the energy range corresponding to the Fe L₃ peak (705–715 eV). The Fe³⁺/ΣFe ratio was calculated from the ratio of the integrated spectral intensity of the Fe³⁺ component to the sum of the integrated spectral intensity of both components. The EDS acquisition time per pixel was 10 µs. For quantitative analysis, Cliff–Lorimer correction was used. K-factors were determined using many mineral standards. At Tohoku University, a JEOL JEM-2100F (S)TEM operating at 200 kV was used. K-factor correction was based on several mineral standards. At the University of Hawai'i at Mānoa, a monochromatized and Cs aberration-corrected Thermo Fisher Titan G2 (S)TEM operating at 300 kV, equipped with EDAX® thin-window EDS and Gatan Tridium EELS was used. A 'TitanX' ChemiSTEM and a Thermo Fisher Titan G2 STEM were also used for additional analysis at the Molecular Foundry, Lawrence Berkeley National Laboratory. At Université de Lille, a monochromatized and Cs aberration-corrected Thermo Fisher Titan Themis (S)TEM operating at 300 kV, equipped with four-quadrant windowless super-X SDD and Gatan Quantum 966 ERS GIF for EELS was used. For quantitative analysis, Cliff–Lorimer correction was used. K-factor correction was based on several mineral standards. At the University of Arizona, a Cs aberration-corrected Hitachi HF5000 (S)TEM, equipped with an Oxford Instruments X-Max 100 TLE EDS system and a Gatan GIF Quantum ER (model 965) electron energy-loss spectroscope was used. The microscope was operated at 200 kV using a 100 pm probe. The energy dispersion was set to 0.25 eV per channel. Maps were acquired by averaging three frames with a relatively large pixel time of 0.2 s for core loss and 0.001 s for the low loss. To quantify the Fe³⁺/Fe²⁺ ratio, FeO, Fe₂O₃ and Fe₃O₄ were used as standards. The samples were measured with a dispersion of 0.25 eV per channel. The background was subtracted using a power-law fit over an energy range of 100 eV. Then, a linear fit was applied in the pre-edge region for the removal of any residuals to ensure a null background intensity. After the background removal, the continuum intensity beneath the edge was subtracted, using a double arctan function⁵⁷. The Fe L₃a and Fe L₃b peak maxima of FeO and Fe₂O₃ were shifted to 708.7 eV and 710.25 eV, respectively, by systematically applying an offset of 3.19 eV to match the energies described in the literature⁵⁸. The spectrum images were acquired over an area measuring 76 × 20 pixels and 2.83 × 0.75 µm. The Fe L₂,₃-edge was quantified using the methods described in the literature⁵⁸,⁵⁹. The obtained calibration curve was applied to each pixel of the spectrum image to determine the Fe³⁺/ΣFe. At the Naval Research Laboratory, the Nion UltraSTEM200-X equipped with a Gatan Enfinium ER electron energy-loss spectroscope and a windowless Bruker SDD EDS was used. Bright-field TEM images were collected on a JEOL2200FS TEM, equipped with a Gatan OneView camera. Quantification of STEM-EDS data was performed with the Cliff–Lorimer method. The EELS measurements have a typical energy resolution of 0.5 eV.

## Scanning transmission X-ray microscopy

The HERMES scanning transmission X-ray microscopy (STXM) beamline at the synchrotron SOLEIL was used. Analytical conditions for X-ray absorption near-edge structure (XANES) analysis using STXM is as follows. Energy calibration was done using the 3p Rydberg peak of gaseous CO₂ at 294.96 eV as well as an internal haematite standard. The microscope

operates under a high vacuum at 10⁻⁵ mbar. Stacks of images are collected at the Fe L₂,₃-edge in the energy range 680–720 eV, with an energy increment of 0.15 eV in the spectral range of the two main peaks associated with Fe³⁺ and Fe²⁺ absorption. The dwell time per pixel was fixed to 1 ms. The beam is focused onto the sample using a Fresnel zone plate of 25 nm. We selected pixel sizes of ~40 nm. The hyperspectral dataset was extracted and processed using the Hyperspy Python-based package⁶⁰. The Fe³⁺/ΣFe ratio was quantified at each pixel⁵⁸,⁵⁹. The background is first subtracted, then a double arctangent is fitted and subtracted to take into account the iron content variation. Then the spectrum is integrated over the energy range corresponding to the Fe³⁺ absorption (708.8–712 eV) and the retrieved value is divided by the spectrum integrated over the full energy range (705–712 eV). This ratio is converted into the Fe³⁺/ΣFe ratio using calibration curves obtained on silicate standards. Ultimately, the component map was created by a linear least-squares fitting of the hyperspectral dataset, using component end-member spectra as inputs (oxidized silicates, melted silicate and sulfides).

## Synchrotron Fe K X-ray absorption spectroscopy

The I 14 X-ray Nanoprobe Beamline at Diamond Light Source, UK was used to achieve X-ray absorption spectroscopy mapping and X-ray fluorescence maps were obtained, each map measured at varied energies ranging from 7,050 to 7,350 eV with a higher energy resolution range over the XANES features (~7,100–7,150 eV). The XANES maps were processed using Mantis v.2.3.02 (ref. ⁶¹) and isolated spectra normalized in Athena v.0.8.056 (ref. ⁶²).

## Microcrater measurement

Forty impact craters ranging from 0.5 to 8.5 µm in average diameters on a millimetre-sized grain (A0067) were measured using a FIB-SEM at Kyoto University. The surface area of 3.6 × 10⁵ µm² was observed. The cumulative impactor flux $F(m)$ was calculated as $F(m) = N(m)/ST$, where *m* is the mass of the impactor, *N(m)* is the cumulative distribution of the impactor, *S* = 3.6 × 10⁵ µm² is the total investigated area of the Ryugu grain and *T* is the exposure time needed for craters to accumulate in the space environment. The mass of the impactor (*m*) is calculated from the diameter of the craters, assuming that an impactor is a spherical object having a density of 3 g cm⁻³ and that the ratio of the crater diameter *D* to the impactor diameter *d* (*D/d*) is assumed to be 1.60 based on laboratory impact experiments⁶³,⁶⁴. For comparison, interplanetary meteoroid flux is calculated using the models in the literature⁴,⁶⁴,⁶⁵.

## Microporosity measurements using X-ray nanotomography

Microporosity was estimated from the results of scanning imaging X-ray microscopy⁶⁶ performed at SPRing-8 BL47XU on Ryugu regolith samples (~15–80 µm; 27 particles). The samples were mounted on Ti needles using a FIB-SEM at Kyoto University, and differential phase images were obtained by scanning X-rays at 8 keV. Then 180° images were obtained every 0.4–1.2°, followed by phase recovery and tomographic reconstruction to obtain three-dimensional images of phase contrast with refractive index decrements (RIDs). The pixel size was ~100 × 100 × 100–200 nm. The grain surfaces were defined by automatic segmentation⁶⁷ and manual modification from the three-dimensional images, and their average RIDs were obtained. The RIDs (δ) are approximately proportional to the material density (ρ), as expressed by the following equation⁶⁸: $δ = ap^b$, where *a* = 3.7174, *b* = 0.87132. In this manner, the average RIDs were converted to the material density. Microporosity is the ratio of bulk density to particle density subtracted from 1. Since the particle density of the Ryugu has not been measured, the grain density of the Orgueil meteorite (2.42 × 10³ kg m⁻³)⁶⁹ was used to estimate the microporosity.

## Helium irradiation experiments

The irradiation experiments were performed at ISAS/JAXA. Irradiation experiments of 4 keV He ions onto a Ryugu grain CO107–HE01
(-300 × -200 µm) were performed in a vacuum. The grains were fixed on a gold substrate with a small amount of epoxy glue. The ion flux was kept at -1.5 × 10¹³ ions cm⁻² s and the total dose of the irradiated ions was 1.3 × 10¹⁸ ions cm⁻². The surface textures before and after irradiation were observed with a JEOL JSM-7000F FE-SEM at the University of Tokyo without carbon deposition under low acceleration voltage and low current conditions (2 kV and 50 pA). FIB thin foil preparation and (S)TEM observation were performed at Kyoto University.

## Data availability

All data needed to evaluate the conclusions in the paper are present in the paper and the Supplementary Information. All data are also available through the DARTS archive (https://data.darts.isas.jaxa.jp/pub/hayabusa2/paper/sample/.Noguchi_2022/). Source data are provided with this paper.

## References

1. Pieters, C. M. & Noble, S. K. Space weathering on airless bodies. *J. Geophys. Res. Planets* **121**, 1865–1884 (2016).

2. Grier, J. A. & Rivkin, A. S. *Airless Bodies of The Inner Solar System* (Elsevier, 2019).

3. Reams, D. V. *Solar Energetic Particles* 2nd edn (Springer, 2021).

4. Grün, E., Zook, H. A., Fechtig, H. & Giese, R. H. Collisional balance of the meteoritic complex. *Icarus* **62**, 244–272 (1985).

5. Nakamura, T. et al. Itokawa dust particles: a direct link between S-type asteroids and ordinary chondrites. *Science* **333**, 1113–1116 (2011).

6. Noguchi, T. et al. Incipient space weathering observed on the surface of Itokawa dust particles. *Science* **333**, 1121–1125 (2011).

7. Noguchi, T. et al. Space weathered rim found on the surfaces of the Itokawa dust particles. *Meteorit. Planet. Sci.* **49**, 188–214 (2014).

8. Matsumoto, T. et al. Surface and internal structures of a space-weathered rim of an Itokawa regolith particle. *Icarus* **257**, 230–238 (2015).

9. Matsumoto, T. et al. Iron whiskers on asteroid Itokawa indicate sulfide destruction by space weathering. *Nat. Commun.* **11**, 1117 (2020).

10. Matsumoto, T. et al. Space weathering of iron sulfides in the lunar surface environment. *Geochim. Cosmochim. Acta* **299**, 69–84 (2021).

11. Thompson, M. S. et al. Microchemical and structural evidence for space weathering in soils from asteroid Itokawa. *Earth Planet. Space* **66**, 89–99 (2014).

12. Langenhorst, F. et al. Mineralogy and defect microstructure of olivine dominated Itokawa dust particle: evidence for shock metamorphism, collisional fragmentation, and LL chondrite origin. *Earth Planet. Space* **66**, 118 (2014).

13. Burgess, K. D. & Stroud, R. Coordinated nanoscale compositional and oxidation state measurements of lunar space-weathered material. *J. Geophys. Res. Planets* **123**, 2022–2037 (2018).

14. Hicks, L. et al. Fe-redox changes in Itokawa space-weathered rims. *Meteorit. Planet. Sci.* **55**, 2599–2618 (2020).

15. Thompson, M. S. et al. Spectral and chemical effects of simulated space weathering of the Murchison CM2 carbonaceous chondrite. *Icarus* **319**, 499–511 (2019).

16. Thompson, M. S. et al. The effect of progressive space weathering on the organic and inorganic components of a carbonaceous chondrite. *Icarus* **346**, 113775 (2020).

17. Matsuoka, M., Nakamura, T., Hiroi, T., Okumura, S. & Sasaki, S. Space weathering simulation with low-energy laser irradiation of Murchison CM chondrite for reproducing micrometeoroid bombardments on C-type asteroids. *Astrophys. J.* **890**, L23 (2020).

18. Lantz, C. et al. Ion irradiation of carbonaceous chondrites: a new view of space weathering on primitive asteroids. *Icarus* **285**, 43–57 (2017).

19. Laczniak, D. L. et al. Characterizing the spectral, microstructural, and chemical effects of solar wind irradiation on the Murchison carbonaceous chondrite through coordinated analyses. *Icarus* **364**, 114479 (2021).

20. Trang, D. et al. The role of hydrated minerals and space weathering products in the bluing of carbonaceous chondrites. *Planet. Sci. J.* **3**, 68 (2021).

21. Kitazato, K. et al. The surface composition of asteroid 162173 Ryugu from Hayabusa2 near-infrared spectroscopy. *Science* **364**, 272–275 (2019).

22. Sugita, S. et al. The geomorphology, color, and thermal properties of Ryugu: implications for parent-body processes. *Science* **364**, eaaw0422 (2019).

23. Morota, T. et al. Sample collection from asteroid (162173) Ryugu by Hayabusa2: implications for surface evolution. *Science* **368**, 654–659 (2020).

24. Tatsumi, E. et al. Spectrally blue hydrated parent body of asteroid (162173) Ryugu. *Nat. Commun.* **12**, 5837 (2021).

25. Brearley, A. J. & Jones, R. H. in *Planetary Materials* Reviews in Mineralogy Vol. 36 (ed. Papike, J. J.) C1 (Mineralogical Society of America, 1998).

26. Weisberg, M. E., McCoy, T. J. & Krot, A. N. in *Meteorites and the Early Solar System II* (eds. Lauretta, D. S. & McSween, H. Y. Jr) 19–52 (University of Arizona Press, 2006).

27. Yada, T. et al. Preliminary analysis of the Hayabusa2 samples returned from C-type asteroid Ryugu. *Nat. Astron.* **6**, 214–220 (2021).

28. Yokoyama, T. et al. The first returned samples from a C-type asteroid show kinship to the chemically most primitive meteorites. *Science* https://doi.org/10.1126/science.abn7850 (2022).

29. Nakamura, E. et al. On the origin and evolution of the asteroid Ryugu: a comprehensive geochemical perspective. *Proc. Jpn. Acad. Ser. B* **98**, 227–282 (2022).

30. Nakamura, T. et al. Formation and evolution of carbonaceous asteroid Ryugu: direct evidence from returned samples. *Science* https://doi.org/10.1126/science.abn8671 (2022).

31. Ito, M. et al. Hayabusa2 returned samples: a unique and pristine record of outer Solar System materials from asteroid Ryugu. *Nat. Astron.* https://doi.org/10.1038/s41550-022-01745-5 (2022).

32. Keller, L. P. & McKay, D. S. The nature and origin of rims on lunar soil grains. *Geochim. Cosmochim. Acta* **61**, 2331–2341 (1997).

33. Noble, S., Pieters, C. M. & Keller, L. P. An experimental approach to understanding the optical effects of space weathering. *Icarus* **192**, 629–642 (2007).

34. *Hayabusa Sample Library* (Astromaterials Science Research Group, JAXA/ISAS, accessed 25th November, 2022) https://curation.isas.jaxa.jp/curation/hayabusa/index.html

35. Gualda, G. A. R., Ghiorso, M. S., Lemons, R. V. & Carley, T. L. Rhyolite-MELTS: a modified calibration of MELTS optimized for silica-rich, fluid-bearing magmatic systems. *J. Petrol.* **53**, 875–890 (2012).

36. Ghiorso, M. S. & Gualda, G. A. R. An H₂O-CO₂ mixed fluid saturation model compatible with rhyolite-MELTS. *Contrib. Mineral. Petrol.* **169**, 53 (2015).

37. Tanbakouei, S. et al. Mechanical properties of particles from the surface of asteroid 25143 Itokawa. *Astron. Astrophys.* **629**, A119 (2019).

38. Bland, P. A. et al. Pressure-temperature evolution of primordial solar system solids during impact-induced compaction. *Nat. Commun.* **5**, 5451 (2014).
39. Rucinski, D. et al. Ionization processes in the heliosphere - Rates and methods of their determination. *Space Sci. Rev.* **78**, 73-84 (1996).

40. Bürgi, A. Proton and alpha particle fluxes in the solar wind: results of a three-fluid model. *J. Geophys. Res.* **97**, 3137v3150 (1992).

41. Keller, L. P. et al. Solar energetic particle tracks in lunar samples: a transmission electron microscope calibration and implications for lunar space weathering. *Meteorit. Planet. Sci.* **56**, 1685-1707 (2021).

42. Matsumoto, T., Hasegawa, S., Nakao, S., Sakai, M. & Yurimoto, H. Population characteristics of submicrometer-sized craters on regolith particles from asteroid Itokawa. *Icarus* **303**, 22–33 (2018).

43. Harries, D. et al. Secondary submicrometer impact cratering on the surface of asteroid 25143 Itokawa. *Earth Planet. Sci. Lett.* **450**, 337–345 (2016).

44. Okazaki, R. et al. Noble gases and nitrogen in samples of asteroid Ryugu record its volatile sources and recent surface evolution. *Science* https://doi.org/10.1126/science.abo0431 (2022).

45. Lauretta, D. et al. Episodes of particle ejection from the surface of the active asteroid (101955) Bennu. *Science* **366**, 1217 (2019).

46. Rubino, S. et al. Space weathering affects the remote near-IR identification of phyllosilicates. *Planet. Sci. Jour.* **1**, 61 (2020).

47. Kitazato, K. et al. Thermally altered subsurface material of asteroid (162173) Ryugu. *Nat. Astron.* **5**, 246–250 (2021).

48. Cloutis, E. A. et al. Spectral reflectance 'deconstruction' of the Murchison CM2 carbonaceous chondrite and implications for spectroscopic investigations of dark asteroids. *Icarus* **305**, 203–224 (2018).

49. Rubino, S. et al. Geometry induced bias in the remote near-IR identification of phyllosilicates on space weathered bodies. *Icarus* **376**, 114887 (2022).

50. Prince, B. S. & Loeffler, M. J. Space weathering of the 3-µm phyllosilicate feature induced by pulsed laser irradiation. *Icarus* **372**, 114736 (2022).

51. Hiroi, T., Pieters, C. M., Zolensky, M. E. & Lipschutz, M. E. Evidence of thermal metamorphism on the C, G, B, and F asteroids. *Science* **261**, 1016–1018 (1993).

52. Vernazza, P. et al. Interplanetary dust particles as samples of icy asteroids. *Astrophys. J.* **806**, 204 (2015). (10pp).

53. Vernazza, P. et al. Different origins or different evolution? Decoding the spectral diversity among C-type asteroids. *Astron. J.* **153**, 72 (2017). (10pp).

54. Hamilton, V. E. et al. Evidence for widespread hydrated minerals on asteroid (101955) Bennu. *Nat. Astron.* **3**, 332–340 (2019).

55. Ito, M. et al. The universal sample holders of microanalytical instruments of FIB, TEM, NanoSIMS, and STXM-NEXAFS for the coordinated analysis of extraterrestrial materials. *Earth, Planet Space* **72**, 133 (2020).

56. Watanabe, M. & Williams, D. B. The quantitative analysis of thin specimens: a review of progress from the Cliff-Lorimer to the new ζ-factor methods. *J. Microsc.* **221**, 89–109 (2006).

57. van Aken, P. A. & Liebscher, B. Quantification of ferrous/ferric ratios in minerals: new evaluation schemes of Fe L₂₃ electron energy-loss near-edge spectra. *Phys. Chem. Mineral.* **29**, 188–200 (2002).

58. Bourdelle, F. et al. Quantification of the ferric/ferrous iron ratio in silicates by scanning transmission X-ray microscopy at the Fe L₂₃ edges. *Contrib. Mineral. Petrol.* **166**, 423–434 (2013).

59. Le Guillou, C., Changela, H. G. & Brearley, A. J. Widespread oxidized and hydrated amorphous silicates in CR chondrites matrices: implications for alteration conditions and H₂ degassing of asteroids. *Earth Planet. Sci. Lett.* **420**, 162–173 (2015).

60. de la Pena, F. et al. Electron microscopy (Big and Small) data analysis with the open-source software package HyperSpy. *Microsc. Microanal.* **23**, 214–215 (2017).

61. Lerotic, M., Mak, R., Wirick, S., Meirer, F. & Jacobsen, C. MANTIS: a program for the analysis of X-ray spectromicroscopy data. *J. Synchrotron Radiat.* **21**, 1206–1212 (2014).

62. Ravel, B. & Newville, M. ATHENA, ARTEMIS, HEPHAESTUS: data analysis for X-ray absorption spectroscopy using IFEFFIT. *J. Synchrotron Radiat.* **12**, 537–541 (2005).

63. Price, M. et al. Comet 81P/Wild 2: the size distribution of finer (sub-10 µm) dust collected by the Stardust spacecraft. *Meteorit. Planet. Sci.* **45**, 1409–1428 (2010).

64. Shu, A. et al. Cratering studies in polyvinylidene fluoride (PVDF) thin films. *Planet. Space Sci.* **89**, 29–35 (2013).

65. Jehn, R. An analytical model to predict the particle flux on spacecraft in the solar system. *Planet. Space Sci.* **48**, 1429–1435 (2000).

66. Takeuchi, A., Uesugi, K. & Suzuki, Y. Three-dimensional phase-contrast X-ray microtomography with scanning-imaging X-ray microscope optics. *J. Synch. Rad.* **20**, 793–800 (2013).

67. Matsumoto, M. et al. Discovery of fossil asteroidal ice in primitive meteorite Acfer 094. *Sci. Adv.* **5**, eaax5078 (2019).

68. Chan, T. & Vese, L. An active contour model without edges. In *Proc. International Conference on Scale-Space Theories in Computer Vision* (eds Nielsen, M. et al.) 141–151 (Springer, 1999).

69. Macke, R. J., Consolmagno, G. J. & Britt, D. T. Density, porosity, and magnetic susceptibility of carbonaceous chondrites. *Meteorit. Planet. Sci.* **45**, 1231–1241 (2011).

## Acknowledgements

The Hayabusa2 project has been developed and led by JAXA in collaboration with the Deutsches Zentrum für Luft- und Raumfahrt (DLR) and the Centre national d'études spatiales (CNES), and supported by NASA and the Australian Space Agency (ASA). We thank all of the members of the Hayabusa2 project for their technical and scientific contributions. TEM works at Kyushu University were supported by the Advanced Characterization Platform of the Nanotechnology Platform Japan (grant no. JPMXP09A21KU0393) sponsored by the Ministry of Education, Culture, Sports, Science and Technology (MEXT), Japan. P.B., T.H.V.P. and R.R. acknowledge the Centre National d'Etude Spatiale (CNES). H.L., C.L.G., D.J., F.D.L.P. and M. Marinova acknowledge the advanced characterization platform, University of Lille - CNRS. Work at the Molecular Foundry was supported by the Office of Science, Office of Basic Energy Sciences, of the US Department of Energy under contract no. DE-AC02-05CH11231. This work was funded by the following funds: JSPS KAKENHI grant nos. 19H00725, 19KK0094, 21H05424, 20H01965, 20H00198, 20H00205, 16H06348 and 20H00188; JSPS Core-to-core program 'International Network of Planetary Sciences'; UK Science and Technology Facilities Council (STFC) grant no. ST/S000429/1; Start-up funds from Purdue University; ISITE ULNE, Métropole Européenne de Lille, the region 'Hauts-de-France' and the ERDF program of the European Union; and European Research Council (ERC) under grant agreement no. 771691 (Solarys).

## Author contributions

T. Noguchi, T. Matsumoto, A. Miyake, Y. Igami, M. Haruta, H. Saito, S. Hata, Y.S., M. Miyahara, N.T., H.A.I., J.P.B., K.O., E.D., H.L., C.L.G., D.J., M. Marinova, F.D.L.P., F.L., D.H., P.B., T.H.V.P., R.R., N.M.A., T.Z., P.-M.Z., M.S.T., R.S., K.B., B.A.C., J.C.B., L.H., L.D., M.R.L., P.A.B., M.E.Z., D.R.F., J. Martinez, A. Tsuchiyama, M. Yasutake, J. Matsuno, S.O., I.M., K.U., M.U., A. Takeuchi, M.S., S.E., A. Takigawa, T. Michikami, T. Nakamura, M. Matsumoto, Y.N., H. Yurimoto, K.N., N.K., N. Sakamoto and S. Tachibana engaged in the following analyses: (scanning) transmission electron microscopy, XANES, nanotomography and He irradiation experiments. T. Noguchi, T. Matsumoto, N.T., R.O., H.A.I., M.S.T., N.M.A. and T.Z. wrote the first draft. The draft was revised and edited by T. Noguchi, T. Matsumoto, N. Tomioka, H.A.I., R.S., P.B., M.S.T., T.Z., T. Nakamura,
S. Tachibana, D.S.L., H.Y., A. Miyake, Y. Igami, S.H., M. Miyahara, H.C.C., E.D., H.S., A. Tsuchiyama, M.E.Z., A. Takigawa, J.C.B., H.L., L.D., D.H., M.R.L., C.L.G., and S.S. All the other authors also commented on the manuscript. The whole analytical project was directed by T. Noguchi.

**Competing interests**

The authors declare no competing interests.

**Additional information**

Extended data is available for this paper at
https://doi.org/10.1038/s41550-022-01841-6.

**Supplementary information** The online version
contains supplementary material available at
https://doi.org/10.1038/s41550-022-01841-6.

**Correspondence and requests for materials** should be addressed
to Takaaki Noguchi.

**Peer review information** *Nature Astronomy* thanks Cateline Lantz, David Trang and the other, anonymous, reviewer(s) for their contribution to the peer review of this work.

**Reprints and permissions information** is available at
www.nature.com/reprints.

**Publisher's note** Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.

**Open Access** This article is licensed under a Creative Commons Attribution 4.0 International License, which permits use, sharing, adaptation, distribution and reproduction in any medium or format, as long as you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons license, and indicate if changes were made. The images or other third party material in this article are included in the article's Creative Commons license, unless indicated otherwise in a credit line to the material. If material is not included in the article's Creative Commons license and your intended use is not permitted by statutory regulation or exceeds the permitted use, you will need to obtain permission directly from the copyright holder. To view a copy of this license, visit http://creativecommons.org/licenses/by/4.0/.

© The Author(s) 2022

Takaaki Noguchi<sup>1,2</sup>, Toru Matsumoto<sup>1,2</sup>, Akira Miyake<sup>1</sup>, Yohei Igami<sup>1</sup>, Mitsutaka Haruta<sup>3</sup>, Hikaru Saito<sup>4,5</sup>, Satoshi Hata<sup>6,7</sup>, Yusuke Seto<sup>8</sup>, Masaaki Miyahara<sup>9</sup>, Naotaka Tomioka<sup>10</sup>, Hope A. Ishii<sup>11</sup>, John P. Bradley<sup>11</sup>, Kenta K. Ohtaki<sup>11</sup>, Elena Dobrică<sup>11</sup>, Hugues Leroux<sup>12</sup>, Corentin Le Guillou<sup>12</sup>, Damien Jacob<sup>12</sup>, Francisco de la Peña<sup>12</sup>, Sylvain Laforet<sup>12</sup>, Maya Marinova<sup>13</sup>, Falko Langenhorst<sup>14</sup>, Dennis Harries<sup>15</sup>, Pierre Beck<sup>16</sup>, Thi H. V. Phan<sup>16</sup>, Rolando Rebois<sup>16</sup>, Neyda M. Abreu<sup>17</sup>, Jennifer Gray<sup>18</sup>, Thomas Zega<sup>19</sup>, Pierre-M. Zanetta<sup>19</sup>, Michelle S. Thompson<sup>20</sup>, Rhonda Stroud<sup>21</sup>, Kate Burgess<sup>22</sup>, Brittany A. Cymes<sup>23</sup>, John C. Bridges<sup>24</sup>, Leon Hicks<sup>24,25</sup>, Martin R. Lee<sup>26</sup>, Luke Daly<sup>26,27,28</sup>, Phil A. Bland<sup>29</sup>, Michael E. Zolensky<sup>30</sup>, David R. Frank<sup>11</sup>, James Martinez<sup>31</sup>, Akira Tsuchiyama<sup>32,33,34</sup>, Masahiro Yasutake<sup>35</sup>, Junya Matsuno<sup>32</sup>, Shota Okumura<sup>1</sup>, Itaru Mitsukawa<sup>1</sup>, Kentaro Uesugi<sup>35</sup>, Masayuki Uesugi<sup>35</sup>, Akihisa Takeuchi<sup>35</sup>, Mingqi Sun<sup>33,34,36</sup>, Satomi Enju<sup>37</sup>, Aki Takigawa<sup>38</sup>, Tatsuhiro Michikami<sup>39</sup>, Tomoki Nakamura<sup>40</sup>, Megumi Matsumoto<sup>40</sup>, Yusuke Nakauchi<sup>41</sup>, Masanao Abe<sup>41,42</sup>, Masahiko Arakawa<sup>43</sup>, Atsushi Fujii<sup>41</sup>, Masahiko Hayakawa<sup>41</sup>, Naru Hirata<sup>44</sup>, Naoyuki Hirata<sup>43</sup>, Rie Honda<sup>45</sup>, Chikatoshi Honda<sup>44</sup>, Satoshi Hosoda<sup>40</sup>, Yu-ichi Iijima<sup>41,60</sup>, Hitoshi Ikeda<sup>41</sup>, Masateru Ishiguro<sup>46</sup>, Yoshiaki Ishihara<sup>41</sup>, Takahiro Iwata<sup>41,42</sup>, Kousuke Kawahara<sup>41</sup>, Shota Kikuchi<sup>47</sup>, Kohei Kitazato<sup>44</sup>, Koji Matsumoto<sup>48,42</sup>, Moe Matsuoka<sup>41</sup>, Yuya Mimasu<sup>41</sup>, Akira Miura<sup>41</sup>, Tomokatsu Morota<sup>38</sup>, Satoru Nakazawa<sup>41</sup>, Noriyuki Namiki<sup>48,42</sup>, Hirotomo Noda<sup>48,42</sup>, Rina Noguchi<sup>49</sup>, Naoko Ogawa<sup>41</sup>, Kazunori Ogawa<sup>41</sup>, Tatsuaki Okada<sup>41,42</sup>, Chisato Okamoto<sup>43,61</sup>, Go Ono<sup>41</sup>, Masanobu Ozaki<sup>41,42</sup>, Takanao Saiki<sup>41</sup>, Naoya Sakatani<sup>50</sup>, Hirotaka Sawada<sup>41</sup>, Hiroki Senshu<sup>47</sup>, Yuri Shimaki<sup>41</sup>, Kei Shirai<sup>43</sup>, Seiji Sugita<sup>38,47</sup>, Yuto Takei<sup>41</sup>, Hiroshi Takeuchi<sup>41,42</sup>, Satoshi Tanaka<sup>41,42</sup>, Eri Tatsumi<sup>51,38</sup>, Fuyuto Terui<sup>52</sup>, Ryudo Tsukizaki<sup>41</sup>, Koji Wada<sup>47</sup>, Manabu Yamada<sup>47</sup>, Tetsuya Yamada<sup>41</sup>, Yukio Yamamoto<sup>41</sup>, Hajime Yano<sup>41,42</sup>, Yasuhiro Yokota<sup>41</sup>, Keisuke Yoshihara<sup>41</sup>, Makoto Yoshikawa<sup>41,42</sup>, Kent Yoshikawa<sup>41</sup>, Ryohta Fukai<sup>41</sup>, Shizuho Furuya<sup>41</sup>, Kentaro Hataakeda<sup>53</sup>, Tasuku Hayashi<sup>41</sup>, Yuya Hitomi<sup>53</sup>, Kazuya Kumagai<sup>53</sup>, Akiko Miyazaki<sup>41</sup>, Aiko Nakato<sup>41</sup>, Masahiro Nishimura<sup>41</sup>, Hiromichi Soejima<sup>53</sup>, Ayako I. Suzuki<sup>53</sup>, Tomohiro Usui<sup>41</sup>, Toru Yada<sup>41</sup>, Daiki Yamamoto<sup>41</sup>, Kasumi Yogata<sup>41</sup>, Miwa Yoshitake<sup>41</sup>, Harold C. Connolly Jr<sup>19,54</sup>, Dante S. Lauretta<sup>19</sup>, Hisayoshi Yurimoto<sup>55</sup>, Kazuhide Nagashima<sup>11</sup>, Noriyuki Kawasaki<sup>55</sup>, Naoya Sakamoto<sup>56</sup>, Ryuji Okazaki<sup>57</sup>, Hikaru Yabuta<sup>9</sup>, Hiroshi Naraoka<sup>57</sup>, Kanako Sakamoto<sup>41</sup>, Shogo Tachibana<sup>58</sup>, Sei-ichiro Watanabe<sup>59</sup> & Yuichi Tsuda<sup>41</sup>

<footnote n="1">¹Division of Earth and Planetary Sciences, Kyoto University, Kyoto, Japan. ²The Hakubi Center for Advanced Research, Kyoto University, Kyoto, Japan.</footnote>

<footnote n="3">³Institute for Chemical Research, Kyoto University, Kyoto, Japan. ⁴Institute for Materials Chemistry and Engineering, Kyushu University, Fukuoka, Japan.</footnote>

<footnote n="5">⁵Pan-Omics Data-Driven Research Innovation Center, Kyushu University, Fukuoka, Japan. ⁶Interdisciplinary Graduate School of Engineering Sciences, Kyushu University, Fukuoka, Japan. ⁷The Ultramicroscopy Research Center, Kyushu University, Fukuoka, Japan. ⁸Department of Geosciences, Osaka Metropolitan University, Osaka, Japan. ⁹Department of Earth and Planetary Systems Science, Hiroshima University, Hiroshima, Japan. ¹⁰Kochi Institute for Core Sample Research, X-Star, JAMSTEC, Nankoku, Japan. ¹¹Hawaiʻi Institute of Geophysics and Planetology, The University of Hawaiʻi at Mānoa, Honolulu, HI, USA. ¹²Unité Matériaux et Transformations UMR 8207, Université de Lille, CNRS, INRAE, Centrale Lille, Lille, France. ¹³Institut Michel-Eugène Chevreul FR 2638, Université de Lille, CNRS, INRAE, Centrale Lille, Université Artois, Lille, France. ¹⁴Institut für Geowissenschaften, Friedrich-Schiller-Universität Jena, Jena, Germany. ¹⁵European Space Resources Innovation Centre, Luxembourg Institute of Science and Technology, Belvaux, Luxembourg. ¹⁶Institut de Planétologie et d'Astrophysique de Grenoble (IPAG), Université Grenoble Alpes, CNRS, Grenoble, France. ¹⁷NASA Langley Research Center, Hampton,</footnote>
VA, USA. ¹⁸Materials Characterization Lab, The Pennsylvania State University Materials Research Institute, University Park, USA. ¹⁹Lunar and Planetary Laboratory, The University of Arizona, Tucson, AZ, USA. ²⁰Department of Earth, Atmospheric and Planetary Sciences, Purdue University, West Lafayette, IN, USA. ²¹Buseck Center for Meteorite Studies, Arizona State University, Tempe, AZ, USA. ²²Materials Science and Technology Division, US Naval Research Laboratory, Washington, DC, USA. ²³NRC Postdoctoral Research Associate, US Naval Research Laboratory, Washington, DC, USA. ²⁴Space Park Leichester, The University of Leicester, Leicester, UK. ²⁵School of Geology, Geography and the Environment, The University of Leicester, Leicester, UK. ²⁶School of Geographical and Earth Sciences, The University of Glasgow, Glasgow, UK. ²⁷Australian Centre for Microscopy and Microanalysis, The University of Sydney, Sydney, New South Wales, Australia. ²⁸Department of Materials, The University of Oxford, Oxford, UK. ²⁹School of Earth and Planetary Sciences, Curtin University, Perth, Western Australia, Australia. ³⁰ARES, NASA Johnson Space Center, Houston, TX, USA. ³¹Jacobs Engineering, Dallas, TX, USA. ³²Research Organization of Science and Technology, Ritsumeikan University, Kusatsu, Japan. ³³CAS Key Laboratory of Mineralogy and Metallogeny, Guangdong Provincial Key Laboratory of Mineral Physics and Materials, Guangzhou Institute of Geochemistry, Chinese Academy of Sciences (CAS), Guangzhou, China. ³⁴CAS Center for Excellence in Deep Earth Science, Guangzhou, China. ³⁵Japan Synchrotron Radiation Research Institute (JASRI/SPing-8), Sayo, Japan. ³⁶University of Chinese Academy of Sciences, Beijing, China. ³⁷Department of Mathematics, Physics, and Earth Science, Ehime University, Matsuyama, Japan. ³⁸Department of Earth and Planetary Science, The University of Tokyo, Tokyo, Japan. ³⁹Faculty of Engineering, Kindai University, Higashi-Hiroshima, Japan. ⁴⁰Department of Earth Science, Tohoku University, Sendai, Japan. ⁴¹Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Sagamihara, Japan. ⁴²The Graduate University for Advanced Studies (SOKENDAI), Hayama, Japan. ⁴³Department of Planetology, Kobe University, Kobe, Japan. ⁴⁴Aizu Research Center for Space Informatics, The University of Aizu, Fukushima, Japan. ⁴⁵Department of Information Science, Kochi University, Kochi, Japan. ⁴⁶Department of Physics and Astronomy, Seoul National University, Seoul, Korea. ⁴⁷Planetary Exploration Research Center, Chiba Institute of Technology, Chiba, Japan. ⁴⁸National Astronomical Observatory of Japan, Tokyo, Japan. ⁴⁹Faculty of Science, Niigata University, Niigata, Japan. ⁵⁰Department of Physics, Rikkyo University, Tokyo, Japan. ⁵¹Instituto de Astrofísica de Canarias, University of La Laguna, Tenerife, Spain. ⁵²Department of Mechanical Engineering, Kanagawa Institute of Technology, Atsugi, Japan. ⁵³Marine Works Japan Ltd, Yokosuka, Japan. ⁵⁴Department of Geology, Rowan University, Glassboro, NJ, USA. ⁵⁵Department of Earth and Planetary Sciences, Hokkaido University, Sapporo, Japan. ⁵⁶Creative Research Institution Sousei, Hokkaido University, Sapporo, Japan. ⁵⁷Department of Earth and Planetary Sciences, Kyushu University, Fukuoka, Japan. ⁵⁸UTokyo Organization for Planetary and Space Science, The University of Tokyo, Tokyo, Japan. ⁵⁹Department of Earth and Environmental Sciences, Nagoya University, Nagoya, Japan. ⁶⁰Deceased: Yu-ichi Iijima. ⁶¹Deceased: Chisato Okamoto. e-mail: noguchi.takaaki.2i@kyoto-u.ac.jp
<figure><img src="image_17.png" /></figure>

**Extended Data Fig. 1** | Histograms of average diameters of fine-grained Ryugu samples investigated in this study. Grains recovered from both (a) 1st and (b) 2nd touchdown (landing) sites (TD1 and TD2) have a skewed size distribution. No clear differences are observed between size distributions of non-space

<figure><img src="image_18.png" /></figure>

weathered (blue bins) and space weathered (red bins) grains in both touchdown sites. The proportions of grains with smooth layers, frothy layers, and melt splashes on non-space weathered surfaces are expressed as percentages in both (a) and (b). Bin ranges are 10 µm.
<figure><img src="image_19.png" /></figure>

**Extended Data Fig. 2** | Textural comparison between smooth surfaces and a He+ ion irradiated sample. Secondary electron (SE) images of (a) a smooth layer on the Ryugu grain A0104–02909600. (b, c) A surface of the non-space weathered Ryugu grain C0107–HE01 (b) before and (c) after a 4 keV He+ irradiation experiment. (d, e) Bright-field (BF) TEM images, diffraction maps,

and electron diffraction patterns of (d) natural and (e) artificial smooth layers on Ryugu grains, which are described in (a) and (b), respectively. In both cases, the smooth layers in the cross-section samples A0104–02809802 and C0107–HE01 are amorphized as shown in the insets of electron diffraction patterns #1 in (d) and (e).
<figure><img src="image_20.png" /></figure>

<figure><img src="image_21.png" /></figure>

**Extended Data Fig. 3** | **Textural Comparison between frothy layers and laser irradiated samples.** (a) SE image of a frothy layer on the Ryugu grain A0104-0223700. (b) Backscattered electron image of the surface of the Murchison CM chondrite after laser irradiation experiment. In both (a) and (b), there are many burst vesicles on grain surfaces. (c) HAADF-STEM image of a frothy layer

<figure><img src="image_22.png" /></figure>

in a cross-section sample A0058-C2001-02 on the large Ryugu grain A0058-C2001. (d) BF TEM image of the Murchison meteorite cross-section sample after laser irradiation experiment. One of the run products of the laser irradiation experiments performed by Thompson et al. (2019) was used for comparison.
<figure><img src="image_23.png" /></figure>

**Extended Data Fig. 4** | Partially exfoliated smooth layers on phyllosilicate-rich matrix. (a) Secondary electron image of a smooth layer on the grain A104-02700600. Partial exfoliation of the smooth surface is indicated by yellow arrows. (b-c) BF-TEM image of an exfoliated smooth layer containing vesicles in the cross-section sample A104-02100203. (c) An enlarged image of the area is

indicated by a square in (b). The arrows in (c) indicate vesicles in the exfoliated smooth layer. The interstice between the exfoliated layer and the phyllosilicate base is filled by epoxy resin, and Pt-C was deposited by FIB-SEM, both from sample preparation.
<figure><img src="image_24.png" /><figcaption>a</figcaption></figure>

<figure><img src="image_25.png" /></figure>

**Extended Data Fig. 5** | 10-nm thick vapor deposit on a smooth layer found in a cross-section sample A104-02809801. A very thin (-10 nm) layer covers the ~60-nm thick smooth layer. EDS maps show that the upper part of the very thin layer is enriched in Mg, Si, Fe, and O, and the lower part is depleted in Mg, Si, and Fe. There are no detectable differences in concentrations in S and Ni.

Because similarly thin top surface layers with such element distribution patterns were reported from Itokawa grains6,7, this top surface layer is considered a vapor deposit on the smooth layer. The estimated boundary between the vapor deposition and the smooth layer is indicated by green or red arrows. This is the only vapor deposit found on the surface of smooth layers investigated.
<figure><img src="image_26.png" /></figure>

**Extended Data Fig. 6** | **High-resolution images of sulfide and metal in a frothy layer on the large grain A0058–C2001.** (a) A BF-TEM image of a spherical Fe–Ni sulfide bead in the frothy layer in the cross-section sample A0058-C2001-03. (b, c) Enlarged BF-TEM images of the red and green boxed areas are shown in (b) and (c), respectively. The lattice fringes shown in (b) are 0.30 nm, which suggests (2 0 2̄) of pyrrhotite (Po). The fringes shown in (c) are 0.18 nm, suggestive of (4 4 0) of pentlandite (Pn). (d) HAADF-STEM image of the cross-section sample A0058-C2001-07 shows a chain of nanophase (np) (Fe, Ni)S in the thin (~100 nm)

smooth layer. (e-h) An aggregate composed of nanophases (<100 nm) on the frothy layer of the cross-section sample A0058-C2001-7. HAADF-STEM image of the aggregate is shown in (e). Enlarged BF-TEM images of the red and green boxed areas in (e) are shown in (f) and (g), respectively. The lattice fringes shown in (b) are 0.30 nm, which suggests (2 0 2̄) of pyrrhotite (Po). The fringes shown in (f) is 0.20 nm, suggestive of (110) of kamacite (FeO) and those in (g) are 0.22 and 0.30 nm, suggestive of (1 2 4), and (110) of troilite (Tr). (h) EELS map of the same area shown in (e) shows that the aggregate lacks oxygen and contains iron.
<figure><img src="image_27.png" /></figure>

**Extended Data Fig. 7** | An olivine crystal and the surrounding phyllosilicate-rich matrix in the rare olivine-bearing grain A0104-02403200. (a) BF-TEM image of radiation-damaged olivine and highly porous hydrated matrix in the cross-section sample A0104-02403206, which was prepared from A0104-02403200. (b) Low-angle annular dark-field

(LAADF)-STEM image shows that the olivine contains solar flare tracks indicated by arrows as well as dislocations (Disloc) and a radiation damage layer. (c) BF-TEM image shows that a thin (-20 nm) continuous smooth layer covers the phyllosilicate-rich matrix of the cross-section sample A0104-02303204, which was prepared from A0104-02403200.
a

<figure><img src="image_28.png" /></figure>

b

<figure><img src="image_29.png" /></figure>

**Extended Data Fig. 8** | Exposure age of the surface of a millimeter-sized Ryugu grain A0067 estimated from the impact crater population. Forty craters with average diameters ranging from 300 nm up to 8.5 µm were examined to estimate the exposure age (see Methods). (a) Secondary electron image of one of the investigated craters. (b) The cumulative impactor flux versus the mass of the impactor, assuming exposure time from $10^2$ years to $10^5$ years (solid lines). Broken

lines indicate interplanetary meteoroid flux models at Ryugu's perihelion (0.96 au [astronomical unit]), average orbit (1.2 au), and aphelion (1.4 au). This diagram shows that the exposure age of the smooth layer-covered surface of A0067 is estimated to be $3 \times 10^4$ years, calculated by its crater population and assuming craters formed by interplanetary meteoroid impacts, even if the average semimajor axis of the orbit of Ryugu had changed from 0.96 to 1.4 au.