Preliminary analysis of the Hayabusa2 samples returned from asteroid Ryugu

C-type asteroids¹ are considered to be primitive small Solar System bodies enriched in water and organics, providing clues to the origin and evolution of the Solar System and the building blocks of life. C-type asteroid 162173 Ryugu has been characterized by remote sensing^2,3,4,5,6,7 and on-asteroid measurements^8,9 with Hayabusa2 (ref. ¹⁰). However, the ground truth provided by laboratory analysis of returned samples is invaluable to determine the fine properties of asteroids and other planetary bodies. We report preliminary results of analyses on returned samples from Ryugu of the particle size distribution, density and porosity, spectral properties and textural properties, and the results of a search for Ca–Al-rich inclusions (CAIs) and chondrules. The bulk sample mainly consists of rugged and smooth particles of millimetre to submillimetre size, confirming that the physical and chemical properties were not altered during the return from the asteroid. The power index of its size distribution is shallower than that of the surface boulder observed on Ryugu¹¹, indicating differences in the returned Ryugu samples. The average of the estimated bulk densities of Ryugu sample particles is 1,282 ± 231 kg m⁻³, which is lower than that of meteorites¹², suggesting a high microporosity down to the millimetre scale, extending centimetre-scale estimates from thermal measurements^5,9. The extremely dark optical to near-infrared reflectance and spectral profile with weak absorptions at 2.7 and 3.4 μm imply a carbonaceous composition with indigenous aqueous alteration, matching the global average of Ryugu^3,4 and confirming that the sample is representative of the asteroid. Together with the absence of submillimetre CAIs and chondrules, these features indicate that Ryugu is most similar to CI chondrites but has lower albedo, higher porosity and more fragile characteristics.

On 6 December 2020, samples from the C-type asteroid 162173 Ryugu were returned to Earth by Hayabusa2 in a hermetically sealed container within the re-entry capsule (Tachibana, S. et al., manuscript in preparation), and transported from South Australia to the Extraterrestrial Sample Curation Center (ESCuC) in Sagamihara, Japan. Samples were recovered in a non-destructive manner and under a strict contamination-controlled conditions to perform initial descriptions before delivery for in-depth investigations by the nominated analytical teams and for future research worldwide, as detailed in the Methods and Extended Data Fig. 1. The asteroid Ryugu is the fourth extraterrestrial body of which samples have been returned to the Earth by spacecraft, following past sample return missions by Apollo¹³, Luna¹⁴ and Chang’e-5¹⁵ from the Moon, Stardust from comet 81 P/Wild2¹⁶ and Hayabusa from near-Earth S-type asteroid Itokawa^17,18. The Ryugu sample has sizes ranging from ~8 mm, the largest average diameter, down to fine submillimetre dusts, with millimetre-scale particles being the most common (Extended Data Fig. 2).

A total of 5.424 ± 0.217 g was collected from Ryugu (Extended Data Fig. 2), and has been kept as physically and chemically pristine as possible, handled only in a vacuum or in purified nitrogen without exposure to Earth’s atmosphere. From Chamber A, 3.237 ± 0.002 g of samples was recovered, collected during the first touch-down sampling (TD1) at the equatorial ridge region of Ryugu¹⁰. We assume that these samples represent the surface materials of Ryugu at the uppermost centimetre-scale layer, and that this layer is influenced by insolation, radiation, temperature cycling and micrometeoritic impacts. From Chamber C, 2.025 ± 0.003 g of samples was recovered, collected during the second touch-down sampling (TD2) at a site¹⁰ proximal to the artificial crater excavated by the Small Carry-on Impactor (SCI)^6,19. We assume that some of the samples in Chamber C represent subsurface materials excavated by the impact experiments, and that these samples have not experienced long-term exposure to space.

The size–frequency distributions for particles larger than 1 mm hand-picked from the bulk samples of chambers A and C were reconstructed from individual particle measurements (Fig. 1). The sample size distribution has a slope of −3.88 ± 0.25 in the power-index. This power index of Chamber A + C particles is steeper than the global average index (−2.65 ± 0.05) obtained for boulders (5–140 m in size) on Ryugu or the power-index (approximately −2) for gravels (0.02 m to several metres in size) at the local touch-down sites¹¹ observed by the telescopic Optical Navigation Camera (ONC-T)²⁰. The steeper power-index in the returned particles implies a higher relative abundance of the smaller particles but there are several possible interpretations for the steep power-index arise, including: the fragile nature of samples from Ryugu that may have undergone further fragmentations during impact sampling using a bullet and the cone-shaped collector²¹, the shock and vibration experienced during Earth entry in the sample container mounted inside the re-entry capsule²², possible artificial fractionation effects from the better transference of smaller particles through the sampler horn²¹ and/or a sampling bias caused by hand-picking of particles with vacuum tweezers by several personnel (as mentioned in the Methods). The power-index of Chamber A particles, −4.59 ± 0.44, is steeper than those of Chamber C, −3.15 ± 0.20, which shows a much shallower power-index in the size range larger than 3 mm. This larger size enrichment in Chamber C could indicate that such larger particles might have been excavated from regolith below Ryugu’s surface by the SCI close to site TD2^10,19.

A dashed red and blue line is a fitting line to the size distribution of Ryugu particles in the chamber A and C, respectively, and a solid black line is a fitting line to the size distribution of those in chambers A and C. The power-index of those in the chambers A and C (shown as Chamber A + C) is −3.88, which is much steeper than of the global average of Ryugu boulders of >5 m, −2.65 (ref. ¹¹). This might indicate that further fragmentation occurred for smaller Ryugu grains before and/or after their recovery.

Source data

From the micrographs of Ryugu particles and their weights measured using a balance, the bulk densities of Ryugu particles could be estimated on the basis of assumptions mentioned in the Methods. The average bulk density of Ryugu particles in both chambers A and C is 1,282 ± 231 kg m⁻³ (Fig. 2). This is lower than the average bulk density of CI chondrites²³ of 2,110 kg m⁻³, that of the Tagish Lake meteorite²⁴ (1,660 ± 80 kg m⁻³, the most porous meteorites ever found on Earth). Assuming that millimetre-sized sample grains have the same grain density as CI chondrites (Orgueil; 2,380 ± 80 kg m⁻³)²³, we estimate the microporosity of Ryugu samples to be 46%. Our value is consistent with the porosity determined by remote thermal imaging by the Thermal Infrared Imager (TIR)²⁵ and on-site thermal measurements⁹ with the radiometer (MARA) on the Mobile Asteroid Surface Scout (MASCOT)²⁶; this value is lower than that of meteorites, suggesting that thermal measurements made remotely at the centimetre scale can be confirmed by laboratory sample measurements made at the millimetre scale. Thus the microscopic observations and weight measurements for the Ryugu samples imply low density and/or high microporosity. The calculated bulk density of the Ryugu samples is comparable to that of Ryugu rock estimated from the bulk density of Ryugu and linear mixture packing theory: 1,380 ± 70 kg m⁻³ within the range of variation²⁷.

The average sample bulk density (1,282 ± 231 kg m⁻³) is slightly larger than that of Ryugu (1,190 kg m⁻³, vertical dashed purple line)² but much smaller than those of the Tagish Lake meteorite (vertical dashed green line)²⁴ and CI chondrites (vertical dashed orange line)²³, indicating the porous nature of Ryugu samples compared with known primitive chondrites.

Source data

Such high-microporosity materials have not been discovered in any meteorites found on Earth, probably due to break-up owing to their fragile nature during entry into the Earth’s atmosphere or a higher abundance of lower-density components such as carbonaceous materials (1,300–1,400 kg m⁻³)²⁸ compared with other carbonaceous chondrites (CCs). The global average density (bulk density) of Ryugu is 1,190 ± 20 kg m⁻³, indicating a macroporosity of 7%, which is inconsistent with the large macroporosities required for primitive asteroids when typical meteoritic density is assumed²³, provided that the returned samples collected from the two sampling sites on the surface of Ryugu are representative of bulk materials on Ryugu. The low macroporosity of Ryugu is probably consistent with the packing model using the size–frequency distribution of Ryugu²⁹. No substantial difference in density distribution was found between chambers A and C, consistent with the same thermal properties inside and outside the artificial crater³⁰. There are particles denser than 1,800 kg m⁻³ (>2σ) in Chamber A, which is within the density range of typical meteorites found on Earth¹² and indicates that Ryugu might consist of a mixture of particles from different origins³⁰ or varying degrees of alteration in the parent bodies^5,30.

Optical and near-infrared reflectance profiles of the samples measured using optical microscopy, Fourier transform infrared (FTIR) spectroscopy and the infrared hyperspectral microscope (MicrOmega)^31,32 show very dark features with an albedo of ~0.02 from 0.4 µm to 4 µm (Figs. 3 and 4), which is in good agreement with the global average of albedo^3,4 observed by ONC-T and the Near Infrared Spectrometer (NIRS3)³³. The surface compositions and inclusions of each sample show some variety but most of them are considered representative of the typical surface materials of Ryugu as they have spectroscopically homogeneous and featureless characteristics without apparent high-temperature components (such as chondrules or Ca–Al-rich inclusions (CAI)), but have many bright and patchy fine inclusions (Extended Data Fig. 2). Although full photometric measurements are needed to elucidate the optical properties of the Ryugu samples, the apparent rarity of chondrules in Ryugu samples is consistent with predictions by a previous study²⁷. The surface morphology of the samples is mainly classified into two patterns of rugged and smooth surfaces even at the millimetre to submillimetre scale, which is similar to the patterns found for centimetre- to metre-scale surfaces^3,8 observed by ONC-T and the imager on MASCOT (MasCAM)³⁴. The presence of different types of surface morphology may indicate past mixing processes of materials of different origin or different degrees of alteration^5,7,30. The shape distribution of the particles, which has been studied in a separate paper (Tachibana, S. et al., manuscript in preparation), shows variations in aspect ratios, including elongated and flattened particles that are consistent with the ejecta observed during the sampling operations (Tachibana, S. et al., manuscript in preparation).

a, Spectra are normalized to each of continua between 2.0 µm to 4.0 µm. Both spectra show features at 2.72 µm (a vertical dashed black line in the left), corresponding to hydroxyl (OH) absorption, and 3.4 µm (a vertical dashed black line in the right), corresponding to organic molecule or carbonate adsorption. A faint absorption at 3.1 µm (a vertical dashed black line in the centre) is also confirmed in spectra of bulk samples analysed by MicrOmega, indicating the presence of a nitrogen-rich phase³². b, The same raw spectra are compared with remote-sensing data for Ryugu taken by NIRS3 with its error bars ⁴. The absorption feature at 2.72 µm (a vertical dashed green line) observed with NIRS3 is confirmed by the Ryugu samples. The continuum of Ryugu samples is reddenned compared with that of NIRS3, which might reflect the space weathering effect being clearer in the samples than remote-sensing data.

Source data

The red lines represent typical types of CC from RELAB data⁵¹ and the blue lines are unusual types of CC from RELAB and Sugita et al.³. Note that the data for each of the CCs are from powder samples within sizes ranging from <63 µm to <155 µm. Ryugu particles obtained from chambers A and C show an albedo of ~0.02 (reflectance factor at 30°, 0°, 30°), which is comparable to remote-sensing data of Ryugu’s surface taken by ONC-T^3,39. Globally, Ryugu is confirmed to be much darker than most meteorites.

Source data

To conduct reconnaissance sample analyses during this curation phase, non-destructive and non-invasive characterization of the composition was performed by near-infrared spectroscopy through the two complementary instruments. Both FTIR and MicrOmega analyses for bulk samples from chambers A and C show spectral profiles. The FTIR can obtain reflectance spectrum from of 1 to 4 µm wavelength range with a footprint of ~6 mm diameter (Fig. 3), and the MicrOmega can analyze hyperspectral image-cubes of 256 × 256 pixels (22 µm pixel size), with up to 400 spectral channels covering the 0.99–3.65 µm spectral range. Both exhibit clear absorption features at 2.7 µm and 3.4 µm, for both samples. The narrow and relatively deep (~15%) absorption feature at 2.72 µm indicates the presence of hydroxyl (OH) in the samples, which is comparable to the 2.72 µm absorption feature detected across the surface of Ryugu by NIRS3⁴ but the position of the absorption peak is in better agreement with the materials excavated by the SCI impact experiment³⁵. MicrOmega high spatial resolution enabled us to identify a few submillimetre grains with distinct and highly diagnostic spectral features. As an example, an absorption centred at 3.4 µm, also present in FTIR spectra, corresponds to both carbonates and CH-rich phases. Similarly, an absorption centred at 3.1 µm is interpreted as relating to NH-rich compounds as it has been postulated to be similar to that observed on 1 Ceres³⁶. These detections are evidence of aqueous alteration of Ryugu’s parent body and consistent with the non-detection of high-temperature components like chondrules and CAIs. They point towards the Ryugu parent body being more similar to CI chondrites than to any other type of meteorite found on Earth (Table 1). Details of the MicrOmega findings are presented in a companion paper³².

High-resolution (5 µm per pixel) optical microscopic imaging through six filters, compatible with the ONC-T camera of Hayabusa2^3,737, was conducted on bulk samples from chambers A and C (Fig. 4). The disk-averaged spectra and reflectance of Earth-returned samples from 0.39 to 0.85 µm (ul to x bands on ONC-T) agree well with those of Ryugu³; very flat spectra consistent with Cb-type asteroids classified by ground-based observations³⁸ and low reflectance (0.02 at the v band) under the geometric condition with incidence, emission and phase angles of 30°, 0° and 30°, respectively. This agreement indicates that Earth-returned samples represent the Ryugu surface materials well. The visible and infrared reflectance of the samples from chambers A and C are both brighter than those of remote-sensing data taken by ONC-T^3,39 and NIRS3^4,35 beyond their observation and analytical errors (Figs. 3 and 4). This may be due to differences in surface conditions of regolith particles between the asteroid surface, on which they might be covered by fine powdery materials, and obtained samples, which might expose their surfaces when they experienced disturbances during the sampling process, and/or the possible contribution of reflected light from the bottom surface of the sapphire dishes. The infrared reflectance of the bulk samples from Chamber A is brighter than that of the samples from Chamber C in data acquired by both FTIR and MicrOmega, although some variations in wavelength exist in the MicrOmega results³². This tendency is inconsistent with results from the NIRS3 observation, which shows deeper absorption in 2.72 µm close to site TD2 site compared with other surface materials on Ryugu³⁵. Although optical and infrared microscopic images show that Ryugu sample particles exhibit many bright spots (Extended Data Fig. 2), most bright spots disappear in different viewing geometries and so are not intrinsic to compositional variation (for example, CAIs and chondrules) but caused by different photometric conditions³². Many bright spots are found on the surfaces of boulders in the on-asteroid images⁸, but most may be caused by photometric effects.

Our initial observations in the laboratory for the entire set of returned samples demonstrate that Hayabusa2 retrieved a representative and unprocessed (albeit slightly fragmented) sample from Ryugu. Our data further extends an idea based on the remote-sensing observations that suggested that Ryugu is dominated by hydrous CC-like materials, similar to CI chondrites, but with a darker, more porous and more fragile nature. This inference should be further corroborated by in-depth investigations hereafter by state-of-the-art analytical methods with higher resolution and precision. The initial descriptions by Hayabusa2 provide a good signpost for future sample returns missions and their curation.

Hayabusa2 sample recovery and transportation to the ESCuC

On 5 December 2020, the re-entry capsule was released from the spacecraft and it entered the Earth’s atmosphere on 6 December 2020, after a successful return cruise from Ryugu to the Earth. The re-entry capsule retrieval operation was carried out under strict compliance with Australian COVID-19 regulations. The landing area of the capsule was determined from a beacon signal transmitted by the capsule using five antennas installed at different locations. The Marine radar systems and two drones were also used for this operation to retrieve the capsule, heat shields and parachute. The re-entry capsule was located near the parachute, which was found by helicopter observation. A safety check of the capsule was first completed at the landing location because pyrotechnic devices were used for parachute deployment and separation. No damage to the capsule was observed, and the capsule was transported back to a quick look facility prepared in the Woomera Prohibited Area with permission from the Australian safety officer. The re-entry capsule was recovered from the landing site in the Woomera Prohibited Area, South Australia, 5 h after landing, and transported to the quick look facility. The capsule was placed in a clean booth in the quick look facility; the sample container was then extracted from the capsule and its outer surface cleaned after a safety check (see also Extended Data Fig. 1). The temperature monitor attached to the sample container indicated that the container was never heated up to 65 °C, which is much lower than the outgassing temperature of water, ~100 °C.

The container was installed on the Hayabusa2 GAs Extraction and Analysis system. After overnight evacuation of the vacuum line of the GAs Extraction and Analysis system, on 7 December the bottom of the sample was pierced with a tungsten carbide needle to release volatile components of the sample held inside the container²². The container was in a vacuum, indicating that the container seal held during re-entry and no terrestrial contamination took place. The gas extracted from the sample container was split into four gas tanks at room temperature, and the residual gas in the system was then trapped in two gas tanks cooled at the temperature of liquid nitrogen. A fraction of the gas was analysed by a quadrupole mass spectrometer (WATMASS, Tokyo Electronics). The sample container was put into a nitrogen-purged antivibration transportation box and was safely transported to the ESCuC in the Sagamihara Campus of JAXA on 8 December 2020 (~57 h after the capsule landed). A heat shield made of carbon-reinforced plastic was then removed from the outer lid of the container after drilling work with a milling machine to expose the heads of the bolts and remove them. The Hayabusa2 sample container was sealed with a metal-to-metal sealing system^21,22. The container lid was pressed against the container edge with a pressure load of ~2,700 N by pressure springs. To open the container in the clean chamber designed for Ryugu samples in a vacuum, the container was installed into the container opening system. The pressure springs and the outer lid with latches were then removed from the container while the pressure load was kept constant. The container with the opening system was then attached to the clean chamber, which was designed to keep the Ryugu samples in a vacuum, on 11 December (132 h after it landed) and was opened on 14 December 2020 after the chamber was evacuated.

As the outer surface of the container had been cleaned, the outer lid was first anchored to access the inner lid, then the inner lid was anchored with rods to remove the outer lid and the frame for the latches. Finally, the inner lid was anchored by the container opening system (Extended Data Fig. 1).

The clean room and clean chambers for Hayabusa2

The concept of Hayabusa2 curation was to initially make non-destructive measurements and to deliver samples for further detailed investigations without any contamination from terrestrial materials or exposure to the terrestrial atmosphere. The ESCuC was therefore equipped to the ISO 6 or Class 1000 clean room protocol (1,000 dust particles of ≥0.5 µm in diameter in cubic feet)⁴⁰. The clean chambers for Hayabusa2-returned samples were prepared to handle samples under a vacuum or ultra-purified nitrogen atmosphere without exposure to the terrestrial atmosphere⁴¹. They comprise five independent chambers: CC3-1 for opening the container in a vacuum, CC3-2 for opening Chamber A of the catcher and removing a few particles in a vacuum, CC3-3 for exchanging the environment from a vacuum to purified nitrogen, CC4-1 for dismantling the catcher to extract the samples from each chamber, and CC4-2 for observation and weighing of the samples. All of the sample containers, pick-up devices, handling tools and other jigs and tools used in the clean chambers were specially cleaned to avoid contamination and were made from materials that were highly controlled to minimize the possibility of chemical reactions with the samples⁴².

Retrieval of Hayabusa2 samples from the container

As the sample container opening system was connected to CC3-1 with dry air overflowing from the chamber, the chamber was evacuated to reach a high vacuum (10⁻⁶ Pa). The chamber was then in a static vacuum condition for the inner lid of the container to be opened. Soon after the container was opened, the chamber was evacuated again. The sample catcher (which is combined with the inner lid) was extracted from the container and the bottom of the container was left behind. The catcher was then turned upside down so the cover of Chamber A of the catcher faced upwards and it was transported from CC3-1 to CC3-2; a gate valve between them was then closed. In CC3-2 in vacuum conditions, the surface of the cover of the Chamber A was cleaned with a Teflon spatula. All of the screw bolts of the cover were then unscrewed and the cover was removed with an electrostatic chuck to expose the samples inside Chamber A of the catcher. A large numbers of black particles of millimetre size or larger were observed inside Chamber A.

A few particles of millimetre size were removed from the chamber with a sample handling tool equipped inside the CC3-2 and put into a quartz glass dish. A cover made of quartz glass was attached to the opening of Chamber A of the catcher; the catcher was then transported from CC3-2 to CC3-3 and the gate valve between them was closed. CC3-1 and CC3-2 continued to evacuate after that. CC3-3 was slowly purged with purified nitrogen to reach atmospheric pressure. After that, the catcher was handled with tools and jigs manipulated with Viton-coated butyl gloves equipped in the CC3-3, CC4-1 and CC4-2. First, a jig for handling was attached to the catcher and the screw bolts that connected the catcher with the inner lid were removed to separate the catcher from the lid.

The catcher was next transported to CC4-2 through CC4-1 to measure its weight with a balance equipped in the CC4-2. Given the design weight of the catcher and a tare weight of the attached jig, the total weight of samples inside the catcher was calculated to be 5.424 ± 0.217 g. The balance was a Mettler-Toledo XP404s, with an outer cover modified to one made of stainless steel 304 sealed with Viton, and with the power and signal cables modified from the originals to ones coated by Teflon.

An optical microscope Nikon SMZ1270i with an XYZ electric motors system was equipped above the CC4-2, and black particles inside Chamber A of the catcher were photographed with the microscope. The catcher was then transported to CC4-1 and it was dismantled with tools and jigs to transfer samples from each of the chambers (A, B and C) to containers made of sapphire glass (see supplement for its spectral feature) set underneath funnels made of stainless steel 304. After several large particles were hand-picked directly from the opening of the funnels with a vacuum tweezer, samples from chambers A and C were divided from the funnels into three sapphire containers with a spatula made of stainless steel. Samples inside Chamber B, which was exposed to the sampler horn after site TD1 and before site TD2¹⁰, were also recovered into a sapphire container and comprise only a small amount of powder (13 ± 0.5 mg). Only a limited number of samples enters into the chamber B, indicating that only a small amount of the samples should be mixed up between three chambers. The samples in the sapphire containers were weighed with a balance and spectrally characterized with FTIR, MicrOmega and visible spectrometers. Next, particles of >1 mm in size were individually hand-picked with a vacuum tweezer that had a nozzle made of stainless steel 304 and deposited into a sapphire dish; individual particles were then photographed, weighed and measured with FTIR and MicrOmega.

These obtained data are catalogued for further detailed research that started in the summer of 2021. The sample will be made available to the community and distributed through the Hayabusa2 Sample Allocation Committee in the summer of 2022.

Outline of measurements for sample description

Multiband optical images of the Ryugu samples were taken using a nadir-viewing camera system with a macro lens and a monochrome CMOS detector (Kiralux CS895MU) with illumination at 30° from the nadir⁴³. We used six filters (ul: 0.39 µm, b: 0.48 µm, v− 0.55 µm, Na: 0.59 µm, w− 0.70 µm, x: 0.85 µm) compatible with ONC-T of Hayabusa2^3,20,21 to illuminate the samples for macro-lens measurements.

Spectroscopy of Ryugu samples

The FTIR used for this study was a JASCO VIR-300, equipped to CC4-2. It can measure in the infrared spectrum between 1.0 µm and 4.0 µm wavelengths. Its minimum beam spot size in the focused position is 1 mm, and a nominal beam spot for bulk sample measurement size is 6 mm. The incident beam comes through a sapphire viewport to illuminate samples inside an FTIR chamber attached to CC4-2 (with a purified nitrogen condition). Before and after the sample measurement, the incident and emission angles of the infrared light were designed to be 16°, thus phase angle for the samples is 32°. The NIRS3 spectrum was created by averaging 128 spectra acquired on 15 May 2019 (see extended data table 2 of Kitazato et al.³⁵ for details). Its reflectance values have been corrected to the same viewing geometry (incidence,16°; emission, 16°, phase, 32°) using the latest photometric model⁴⁴. Error bars are 1σ. The instrument, which includes incident and reflected light paths, was purged with nitrogen to decrease the influences of absorption of atmospheric molecules such as H₂O and CO₂. Infragold was measured before sample measurement to compensate for the background. No obvious effect from the sapphire containers was detected in the bulk sample analyses.

The detailed method for MicrOmega analyses is detailed in another paper³². MicrOmega was mounted on a dedicated chamber attached to CC3-3. The samples are analysed on an XYZ and θ moving stage under the nitrogen-purged conditions, and observed with MicrOmega through the sapphire window.

Size distribution and density determination of Ryugu particles

The sizes of Ryugu particles were measured from optical microscope images taken after their separation into individual containers. Note that particles were separated using tweezers by various curatorial members of the ESCuC, which may have caused a sampling bias. For the analyses of their size distributions, the major and minor diameters were calculated on the basis of eclipses circumscribed from the binarized images of particles, and averages of the major and minor diameters were used as the sizes of the particles. A cumulative number of particles versus their average diameters are plotted as Fig. 1, and a power-index fitting to the distribution was calculated by maximum-likelihood fitting methods with goodness-of-fit tests based on the Kolmogorov–Smirnov statistic^45,46.

The volume of a given hand-picked particle, its size, D_p, was calculated as follows:

where a and b are the major and minor Fetet diameters, respectively, measured from its optical microscopic image and t is thickness, measured by focusing on the top and bottom of the particle using the optical microscope. Using D_p calculated from equation (1), the volume of a Ryugu particle was calculated using the following formula based on ref. ⁴⁷:

The densities of the particles were calculated from the volumes obtained with the formula and weights measured with the balance in CC4-2 (Fig. 2). Typical errors in the density calculations range from 30 to 500 kg m⁻³, mainly due to uncertainties in the estimation of their volumes. The estimated volumes should include all of the pores inside sample particles; thus the calculated densities correspond to bulk densities of the particles, not grain densities, which are calculated on the basis of volumes excluding pores inside the particles.

Here we note that all source data for the figures in this article is provided in the Supplement Items. Source data are provided with this paper.

The Hayabusa2 mission has been led by JAXA, in collaboration with DLR (German Space Center) and CNES (French Space Center), and was also supported by NASA, the ASA (Australian Space Agency) and other universities and institutes. We thank all of the members of the Hayabusa2 project team for their technical and scientific contributions to the successful return of the asteroid samples to Earth. This research is partly supported by the Japan Society for the Promotion of Science (JSPS) under KAKENHI grant numbers JP17H06459, JP18K03830, JP19K03958, JP19K23473, JP20K14548, JP19K23474, JP21K13986, JP20K14535, JP19H00725, JP19KK0094, JP20H00202, JP18K18795, JP18H04468, JP15H05695, JP16H06348 and JP19H01951, the Core-to-Core programme ‘International Network of Planetary Sciences’ and the Australian Research Council (grant number DP210101798). The activities of the Institut d’Astrophysique Spatiale are supported by the Centre National d’Etudes Spatiales, France.

1. Miwa Yoshitake

   Present address: Japan Patent Office, Tokyo, Japan

2. Ayako Iwamae

   Present address: Toyo University, Tokyo, Japan

Affiliations

1. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Sagamihara, Japan

   Toru Yada, Masanao Abe, Tatsuaki Okada, Aiko Nakato, Kasumi Yogata, Akiko Miyazaki, Kentaro Hatakeda, Kazuya Kumagai, Masahiro Nishimura, Yuya Hitomi, Hiromichi Soejima, Miwa Yoshitake, Ayako Iwamae, Shizuho Furuya, Masayuki Uesugi, Yuzuru Karouji, Tomohiro Usui, Tasuku Hayashi, Daiki Yamamoto, Ryota Fukai, Lucie Riu, Shogo Tachibana, Hirotaka Sawada, Kanako Sakamoto, Hajime Yano, Tetsuya Yamada, Masaki Fujimoto, Hisayoshi Yurimoto, Hiroshi Kikuchi, Rina Noguchi, Yuri Shimaki, Kei Shirai, Yukio Yamamoto, Yasuhiro Yokota, Moe Matsuoka, Akira Miura, Atsushi Fujii, Satoshi Hosoda, Takahiro Iwata, Shota Kikuchi, Yuya Mimasu, Osamu Mori, Naoko Ogawa, Takanobu Shimada, Stefania Soldini, Tadateru Takahashi, Yuto Takei, Hiroshi Takeuchi, Ryudo Tsukizaki, Fuyuto Terui, Satoru Nakazawa, Satoshi Tanaka, Takanao Saiki, Makoto Yoshikawa & Yuichi Tsuda

2. The Graduate University for Advanced Studies (SOKENDAI), Hayama, Japan

   Masanao Abe, Takahiro Iwata, Satoshi Tanaka, Makoto Yoshikawa & Yuichi Tsuda

3. University of Tokyo, Tokyo, Japan

   Tatsuaki Okada, Shizuho Furuya, Seiji Sugita, Yuichiro Cho, Koki Yumoto, Yuna Yabe, Shogo Tachibana, Yayoi N. Miura & Eri Tatsumi

4. Marine Works Japan, Ltd, Yokosuka, Japan

   Kentaro Hatakeda, Kazuya Kumagai, Yuya Hitomi, Hiromichi Soejima & Ayako Iwamae

5. Japan Synchrotron Radiation Research Institute, Hyogo, Japan

   Masayuki Uesugi & Kentaro Uesugi

6. JAXA Space Exploration Center, Japan Aerospace Exploration Agency, Sagamihara, Japan

   Yuzuru Karouji, Yoshiaki Ishihara, Kazunori Ogawa, Naoko Ogawa & Takanobu Shimada

7. Chiba Institute of Technology, Narashino, Japan

   Seiji Sugita, Koji Wada, Hiroki Senshu, Manabu Yamada & Shota Kikuchi

8. Institut d’Astrophysique Spatiale, Université Paris-Saclay, CNRS, Orsay, France

   Jean-Pierre Bibring, Cedric Pilorget, Vincent Hamm, Rosario Brunetto, Lucie Riu, Lionel Lourit, Damien Loizeau & Guillaume Lequertier

9. Centre National d’Etudes Spatiales, Toulouse, France

   Aurelie Moussi-Soffys

10. Kyushu University, Fukuoka, Japan

    Ryuji Okazaki & Hiroshi Naraoka

11. Japan Agency for Marine-Earth Science and Technology, Kanagawa, Japan

    Yoshinori Takano

12. The University of Queensland, St Lucia, Queensland, Australia

    Trevor R. Ireland

13. The University of Aizu, Aizu-Wakamatsu, Japan

    Kohei Kitazato, Naru Hirata & Chikatoshi Honda

14. National Astronomical Observatory of Japan, Mitaka, Japan

    Noriyuki Namiki, Koji Matsumoto & Hirotomo Noda

15. Kobe University, Kobe, Japan

    Masahiko Arakawa, Naoyuki Hirata & Kei Shirai

16. Hokkaido University, Sapporo, Japan

    Hisayoshi Yurimoto

17. Tohoku University, Sendai, Japan

    Tomoki Nakamura

18. Kyoto University, Kyoto, Japan

    Takaaki Noguchi

19. Hiroshima University, Higashi-Hiroshima, Japan

    Hikaru Yabuta

20. Kochi Institute for Core Sample Research, JAMSTEC, Nankoku, Kochi, Japan

    Motoo Ito

21. Institute for Planetary Materials, Okayama University, Misasa, Japan

    Eizo Nakamura & Katsura Kobayashi

22. Kindai University, Higashi-Hiroshima, Japan

    Tatsuhiro Michikami

23. Niigata University, Niigata, Japan

    Rina Noguchi

24. Nagoya University, Nagoya, Japan

    Tomokatsu Morota & Sei-ichiro Watanabe

25. Kochi University, Kochi, Japan

    Rie Honda

26. Observatoire de Paris, Meudon, France

    Moe Matsuoka

27. Rikkyo University, Tokyo, Japan

    Naoya Sakatani

28. Instituto de Astrofísica de Canarias, University of La Laguna, Tenerife, Spain

    Eri Tatsumi

29. Space Engineering Development Co., Ltd, Sagamihara, Japan

    Atsushi Fujii

30. Research and Development Directorate, JAXA, Sagamihara, Japan

    Chikako Hirose, Hitoshi Ikeda, Go Ono & Kent Yoshikawa

31. University of Liverpool, Liverpool, UK

    Stefania Soldini

32. NEC Corporation, Fuchu, Japan

    Tadateru Takahashi

33. Kanagawa Institute of Technology, Atsugi, Japan

    Fuyuto Terui

34. University of Tokyo, Kashiwa, Japan

    Satoshi Tanaka

Contributions

T. Yada and M.A. led the initial descriptions of the Hayabusa2-returned samples in the JAXA ESCuC, and T. Yada, T.O and T.U. coordinated co-author contributions and led the data analyses and interpretations. T. Yada, K. Yogata, M.N., A.N., A.M., K. Kumagai, K.H., Y.H., M.S., M. Yoshitake, S.F., A.I.S., D.Y., T.H., R.F., T.O., M.A., T.U., K.U., M.U., Y.K. and K. Kobayashi curated samples and contributed to planning. S. Tachibana, H. Sawada, R.O., Y.T., K. Sakamoto, Y.N.M., H. Yano, T.R.I., T. Yamada and M.F. contributed to sampling and sample recovery. T. Yada, A.N., A.M., K. Yogata, K.H., K. Kumagai, M.N., Y.H., M.Y., A.I.S., S.F. and M.A. performed the microscopy, size and weight measurements, and their data reductions. M.A., K.H., A.M., A.N., K. Yogata, T. Yada, K. Kumagai., M.N., Y.H. and K. Kitazato performed the FTIR data acquisitions and reductions. J.P.B., C.P., V.H., R.B., D.L., G.L., L.L., L.R., T.O., T. Yada, K. Yogata, A.N., A.M., K.H., K. Kumagai, M.N., Y.H., A.M.S. and M.F. conducted the MicrOmega data acquisitions and reductions. S. Sugita, Y.C., K. Yumoto, Y. Yabe, A.M., M.A., T. Yada, A.N., K.H., K. Yogata, K.K., M.N. and Y.H. acquired the multiband microscopy data and performed reductions. S. Tanaka, T.O., S.Sugita, N.N., K.Kitazato, H. Yabuta, T. Nakamura, Y.I., Naru Hirata, Naoyuki Hirata, K.M., T. Michikami, H.Noda, R.N., Y.S., K. Shirai, K.O., K.W., H. Senshu, Y. Yamamoto, T. Morota, R.H., Y. Yokota, C. Honda, M.M., N.S., E.T., A. Miura, M. Yamada, M.A., T.I., H. Yano, A.F., C.Hirose, S.H., H.I., S.K., Y.M., O.M., N.O., G.O., H.Sawada, T.Shimada, S.Soldini, T.T., Y.Takei, H.T., R.T., K. Yoshikawa, F.T., T. Saiki, S.N., M.Y., S.W. and Y. Tsuda contributed to science operations of the spacecraft and selected sampling sites. Y. Tsuda, S.W., M. Yoshikawa, T. Saiki, S. Tanaka, F.T., S.N., S. Sugita, N.N., K. Kitazato, T.O., S. Tachibana, Naru Hirata, H. Yurimoto, T. Nakamura, T. Noguchi, H.Yabuta, H.N., M.I. and E.N. administered the project and acted as principal investigators. T. Yada, T.O., T.U., S. Sugita, Y.C., K.Yumoto, S.W., S. Tachibana, J.P.B., R.B., K. Kitazato, T. Michikam and H.K. contributed to the interpretation and writing. All authors discussed the results anded on the manuscript.

Competing interests

The authors declare no competing interests.

Peer review information Nature Astronomy thanks Beth Clark and Hannah Kaplan for their contribution to the peer review of this work.

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/.

Reprints and Permissions

• • Beth Ellen Clark

  Nature Astronomy (2021)

• • C. Pilorget
  • T. Okada
  • J.-P. Bibring

  Nature Astronomy (2021)