OSIRIS-REx

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Animation of OSIRIS-REx
Animation of OSIRIS-REx trajectory.gif
Around the Sun
Animation of OSIRIS-Rex trajectory around 101955 Bennu.gif
Around 101955 Bennu
Animation of OSIRIS-REx around Bennu - touch down on Bennu.gif
Touchdown on Bennu
Animation of Osiris-REx SRC around Earth - Landing on Earth.gif
Landing on Earth
  OSIRIS-REx ·   101955 Bennu  ·  Earth ·  Sun

Sample acquisition

Artist's concept of TAGSAM instrument in operation Artist's concept of OSIRIS-REx TAGSAM in operation.jpg
Artist's concept of TAGSAM instrument in operation

Procedure

Rehearsals were performed before sampling, during which the solar arrays were raised into a Y-shaped configuration to minimize the chance of dust accumulation during contact and provide more ground clearance in case the spacecraft tipped over (up to 45°) during contact. [29] The descent was very slow, minimizing thruster firings prior to contact to reduce the likelihood of asteroid surface contamination by unreacted hydrazine propellant. Contact with the surface of Bennu was detected using accelerometers, and the impact force was dissipated by a spring in the TAGSAM arm. [47]

Upon surface contact by the TAGSAM instrument, a burst of nitrogen gas was released, to blow regolith particles smaller than 2 cm (0.8 in) into the sampler head at the end of the robotic arm. A five-second timer limited the collection time to mitigate the chance of a collision, and the probe then executed a back-away maneuver to depart safely. [29]

The plan was then for OSIRIS-REx to perform a braking maneuver a few days later to halt the drift away from the asteroid in case it was necessary to return for another sampling attempt. It would then take images of the TAGSAM head to verify a sample had been acquired. If a sample was acquired, the spacecraft would rotate about the short axis of the sample arm to determine sample mass by measuring momentum of inertia and determine if it was in excess of the required 60 g (2.1 oz).

Both the braking and rotation maneuvers were canceled when images of the sample container clearly showed a large excess of material was collected, some of which was able to escape through the container's seal because some material had jammed the mechanism open. The collected material was scheduled for immediate storage in the Sample-Return Capsule. [48] [29] On 28 October 2020, the sample collector head was secured in the return capsule. Following the separation of the head from the collector arm, the arm was retracted into its launch configuration, and the Sample-Return Capsule lid was closed and latched preparing to return to Earth. [49] [50]

In addition to the bulk sampling mechanism, contact pads on the end of the sampling head made of tiny stainless steel loops (Velcro) [51] passively collected dust grains smaller than 1 mm.

Operations

The final four candidate sample sites OSIRIS-REx candidate sample sites on Bennu.png
The final four candidate sample sites
The successful October 2020 sample collection, showing OSIRIS-REx touching down on the Nightingale sample site OSIRIS-REX SamCam TAGSAM Event 2020-10-20 small.gif
The successful October 2020 sample collection, showing OSIRIS-REx touching down on the Nightingale sample site
Sample collection as seen by the navigation camera (00:47; October 20, 2020)
Images of the TAGSAM head showing that it is full of rocks and dust collected from Bennu and that it is leaking material into space OSIRIS-REx TAGSAM head during sample imaging 2020-10-22.gif
Images of the TAGSAM head showing that it is full of rocks and dust collected from Bennu and that it is leaking material into space
OSIRIS-REx successfully stows its sample of asteroid Bennu in October 2020. OSIRIS-RExStowsAsteroidBennuSample-20201029.png
OSIRIS-REx successfully stows its sample of asteroid Bennu in October 2020.
The sample container closes.

NASA selected the final four candidate sample sites in August 2019, named Nightingale, Kingfisher, Osprey, and Sandpiper. [52] On 12 December 2019, they announced that Nightingale had been selected as the primary sample site and Osprey was selected as the backup site. [53] Both were within craters, with Nightingale near Bennu's north pole while Osprey was near the equator. [54]

NASA planned to perform the first sampling in late August 2020; [55] NASA's originally planned Touch-and-Go (TAG) sample collection was scheduled for 25 August 2020, but was rescheduled for 20 October 2020, at 22:13 UTC. [56] [57] On 15 April 2020, the first sample collection rehearsal was successfully performed at the Nightingale sample site. The exercise took OSIRIS-REx as close as 65 m (213 ft) from the surface before performing a back-away burn. [58] [59] A second rehearsal was successfully completed on 11 August 2020, bringing OSIRIS-REx down to 40 m (130 ft) from the surface. This was the final rehearsal before the sample collection scheduled for 20 October 2020, at 22:13 UTC. [60] [61]

At 22:13 UTC, on 20 October 2020, OSIRIS-REx successfully touched down on Bennu at a distance of 200 million miles (320 million kilometers) from Earth. [62] [63] NASA confirmed via images taken during sampling that the sampler had made contact. The spacecraft touched down within 92 cm (36 in) of the target location. [64] [65] A sample of the asteroid which was estimated to weigh at least 2 ounces (57 grams) was collected by OSIRIS-REx following the touch down. [18] After imaging the TAGSAM head, NASA concluded that there were rocks wedged in the mylar flap meant to keep the sample inside, causing the sample to slowly escape into space. [66] In order to prevent further loss of the sample through the flaps, NASA canceled the previously planned spinning maneuver meant to determine the mass of the sample as well as a navigational braking maneuver, and decided to stow the sample on 27 October 2020 rather than 2 November 2020 as originally planned, which was completed successfully. The collector head was observed hovering over the Sample Return Capsule (SRC) after the TAGSAM arm moved it into the proper position for capture, and the collector head was later secured onto the capture ring in the SRC. [66]

When the head was seated into the Sample-Return Capsule's capture ring on 28 October 2020, the spacecraft performed a "backout check", which commanded the TAGSAM arm to back out of the capsule. This maneuver is designed to tug on the collector head and ensure that the latches – which keep the collector head in place – are well secured. Following the test, the mission team received telemetry confirming that the head was properly secured in the Sample-Return Capsule. Thereafter, on 28 October 2020, two mechanical parts on the TAGSAM arm were disconnected – these are the tube that carried the nitrogen gas to the TAGSAM head during sample collection and the TAGSAM arm itself. Over the next several hours, the mission team commanded the spacecraft to cut the tube that stirred up the sample through the TAGSAM head during sample collection, and separate the collector head from the TAGSAM arm. Once the team confirmed these activities were done, it commanded the spacecraft on 28 October 2020, to close and seal the Sample-Return Capsule, the final step of the sample stowage process of Bennu's samples. [67] To seal the SRC, the spacecraft closed the lid and then secured two internal latches. On inspecting images, it was observed that a few particles had escaped from the collector head during the stowage procedure, but it was confirmed that no particles would hinder the stowage process, since the team was confident that a plentiful amount of material remained inside of the head, more than the 60 g (2.1 oz) needed, that is, 121.6 g (4.29 oz). [11] The sample of Bennu was safely stored and ready for its journey to Earth. With the collector head secure inside the SRC, pieces of the sample would no longer be lost. [68]

Sample return

OSIRIS-REx Sample Return (NHQ202309240005).jpg
Two members of the recovery team examine the return capsule after landing
OSIRIS-REx Sample Return (NHQ202309240002).jpg
Close-up photo of the return capsule upon landing
OSIRIS-REx expected landing area map.jpg
Expected landing area of return capsule in Utah

On 7 April 2021, OSIRIS-REx completed its final flyover of Bennu and began drifting away from the asteroid. [69] On 10 May 2021, the spacecraft departed the vicinity of Bennu and began its two-year journey to Earth with the asteroid sample. [70] [71] [72]

On 24 September 2023, at 4:42 a.m. MDT (UTC-06:00), at a distance of 63,000 miles (101,000 kilometers) from Earth, it ejected the sample return capsule, which re-entered the atmosphere at 27,650 miles per hour (44,500 km/h). [73] Due to a mistake in wiring, the drogue parachute did not deploy as planned at 100,000 feet (30,400 meters). [74] However, the main parachute was released when the spacecraft reached about 9,000 feet (2,700 meters), and it survived deployment despite higher than anticipated speeds. [74] About 8:52 a.m. MDT the capsule landed at 11 mph (18 km/h) at the Utah Test and Training Range, one minute earlier than predicted. [74] [75] [76] The main spacecraft maneuvered to a trajectory away from Earth for its extended mission to Apophis in 2029 called OSIRIS-APEX. [77]

At 10:15 a.m. MDT (UTC-06:00), the capsule was taken from the landing site by helicopter. The sample will be analyzed at NASA's Astromaterials Research and Exploration Science Directorate (ARES) and at Japan's Extraterrestrial Sample Curation Center. [76] [78] Asteroid sample material requests will be considered and distributed to organizations worldwide by ARES. [23]

On 11 October 2023, the recovered capsule was opened to reveal a "first look" at the asteroid sample contents. [12] Further looks were reported on 13 December 2023 and revealed organic molecules and unknown materials that require study to determine their composition. [79] [80]

Some damaged fasteners prevented immediate opening, but, after three months, on 13 January 2024, NASA reported fully opening the recovered container. [81] [82] In total, 121.6 g (4.29 oz) of asteroidal material was recovered from the sample container. [11] [83]

Extended mission

On 25 April 2022, NASA confirmed that the mission would be extended. After dropping off its sample to Earth on 24 September 2023, the mission became OSIRIS-APEX ('APophis EXplorer'). [77] As its new name suggests, its next target will be the near-Earth asteroid (and potentially hazardous object) 99942 Apophis. Apophis will make an extremely close pass to the Earth on 13 April 2029. Observations of Apophis will commence on 8 April 2029, and a few days later, on 21 April, OSIRIS-APEX is planned to rendezvous with the asteroid. [84] OSIRIS-APEX will orbit Apophis for around 18 months in a regime similar to that at Bennu. The spacecraft will perform a maneuver, similar to sample collection at Bennu, by using its thrusters to disturb Apophis's surface, in order to expose and spectrally study the subsurface and the material beneath it. [16]

Animation of OSIRIS-APEX
Animation of OSIRIS-REx around Sun - Extended mission.gif
Around the Sun
Animation of OSIRIS-APEX around 99942 Apophis.gif
Around 99942 Apophis
  OSIRIS-APEX ·   99942 Apophis ·  Earth ·  Sun

Name

OSIRIS-REx and OSIRIS-APEX are acronyms, and each letter or combination of letters relates to part of the respective projects: [85]

  • O – Origins
  • SI – Spectral Interpretation
  • RI – Resource Identification
  • S – Security
  • REx – Regolith Explorer
  • APEX – Apophis Explorer

Each of these words was chosen to represent an aspect of this mission. [85] For example, the S, for security means the security of Earth from impact by hazardous near-Earth objects (NEOs). [85] Specifically it refers to better understanding the Yarkovsky effect, which can alter the trajectories of orbiting bodies. [85] Regolith Explorer means that the mission will study the texture, morphology, geochemistry, and spectral properties of the regolith of asteroid Bennu while Apophis Explorer corresponds to the study of Apophis asteroid. [85]

When its heritage concept was proposed in the Discovery Program in 2004, it was called only OSIRIS, with REx for "Regolith Explorer" used descriptively rather than as part of the name. [86]

The asteroid for the second mission is named after the ancient Egyptian god Apophis, who was associated with chaos and destruction. [87] The mission name itself was a reference to the god Osiris. Dante Lauretta, deputy PI of the mission, was called "a mythology buff" by the mission PI Michael Drake: "he was doodling on a pad and trying to capture the principal themes of what we are trying to do with this mission study life origins, identify resources, planetary security in the form of asteroid deflection and he realized he got the name of Osiris out of that, an ancient god of Egypt who may have been one of the first pharaohs." [88] [89]

Science objectives

Sample Return Capsule infographic OSIRIS-REx Sample Return Capsule (Schematic).png
Sample Return Capsule infographic

The science objectives of the mission are: [90]

  • Return and analyze a sample of pristine carbonaceous asteroid regolith in an amount sufficient to study the nature, history, and distribution of its constituent minerals and organic compounds
  • Map the global properties, chemistry, and mineralogy of a primitive carbonaceous asteroid to characterize its geologic and dynamic history and provide context for the returned samples
  • Document the texture, morphology, geochemistry, and spectral properties of the regolith at the sampling site in situ at scales down to millimeters
  • Measure the Yarkovsky effect (a thermal force on the object) on a potentially hazardous asteroid and constrain the asteroid properties that contribute to this effect
  • Characterize the integrated global properties of a primitive carbonaceous asteroid to allow for direct comparison with ground-based telescopic data of the entire asteroid population

Telescopic observations have helped define the orbit of 101955 Bennu, a near-Earth object (NEO) with a mean diameter in the range of 480 to 511 m (1,575 to 1,677 ft). [91] It completes an orbit of the Sun every 436.604 days (1.2 years). This orbit takes it close to the Earth every six years. Although the orbit is reasonably well known, scientists continue to refine it. It is critical to know the orbit of Bennu because recent calculations produced a cumulative probability of 1 in 1410 (or 0.071%) of impact with Earth from 2169 to 2199. [92] One of the mission objectives is to refine understanding of non-gravitational effects (such as the Yarkovsky effect) on this orbit, and the implications of those effects for Bennu's collision probability. Knowing Bennu's physical properties will be critical for future scientists to understand when developing an asteroid impact avoidance mission. [93]

Specifications

OSIRIS-REx.stl
3D model of OSIRIS-REx
OSIRIS-REx instrument deck.png
OSIRIS-REx instrument deck
  • Dimensions: Length 2.4 m (7 ft 10 in), width 2.4 m (7 ft 10 in), height 3.15 m (10.3 ft) [2]
  • Width with solar arrays deployed: 6.17 m (20.2 ft) [2]
  • Power: Two solar arrays generate 1226 to 3000 Watts, depending on the spacecraft's distance from the Sun. Energy is stored in Li-ion batteries. [2]
  • Propulsion system: Based on a hydrazine monopropellant system developed for the Mars Reconnaissance Orbiter , carrying 1,230 kg (2,710 lb) of propellant and helium. [94]
  • The sample-return capsule reentered the Earth's atmosphere with a parachute assisted landing. The capsule with encased samples was retrieved from Earth's surface and is being studied, as was done with the Stardust mission.

Instruments

In addition to its telecommunication equipment, the spacecraft carries a suite of instruments to image and analyze the asteroid on many wavelengths, [95] and retrieve a physical sample to return to Earth. The Planetary Society coordinated a campaign to invite interested persons to have their names or artwork on the mission's spirit of exploration saved on a microchip now carried in the spacecraft. [96]

OCAMS

Imaging camera suite Osiris-Rex Ocams 007.jpg
Imaging camera suite

The OSIRIS-REx Camera Suite (OCAMS) consists of the PolyCam, the MapCam, and the SamCam. [95] Together, they acquire information on asteroid Bennu by providing global mapping, sample site reconnaissance and characterization, high-resolution imaging, and records of the sample acquisition. [97]

  • PolyCam, an 20 cm (7.9 in) telescope, acquired visible-light images with increasingly higher resolution on approach the asteroid and high-resolution surface images from orbit
  • MapCam searches for satellites and outgassing plumes. It maps the asteroid in four blue, green, red and near infrared channels, and informs the model of Bennu's shape and provides high resolution imaging of the potential sample sites
  • SamCam continuously documents the sample acquisitions

OVIRS

OVIRS Osiris-Rex Ovirs gsfc 20150619 2015-12655 019-023.jpg
OVIRS

The OSIRIS-REx Visible and IR Spectrometer (OVIRS) is a spectrometer which maps minerals and organic substances on the asteroid's surface. [95] It provides full-disc asteroid spectral data at 20 m resolution. It maps blue to near-infrared, 400–4300 nm, with a spectral resolution of 7.5–22 nm. [98] This data will be used in concert with OTES spectra to guide sample-site selection. The spectral ranges and resolving powers are sufficient to provide surface maps of carbonates, silicates, sulfates, oxides, adsorbed water and a wide range of organic compounds.[ citation needed ]

OTES

OTES Osiris-Rex Otes-3.jpg
OTES

The OSIRIS-REx Thermal Emission Spectrometer (OTES) provides thermal emission spectral maps and local spectral information of candidate sample sites in the thermal infrared channel covering 4–50 µm, again to map mineral and organic substances. [95] The wavelength range, spectral resolution, and radiometric performance are sufficient to resolve and identify silicates, carbonates, sulfates, phosphates, oxides, and hydroxide minerals. OTES is also used to measure the total thermal emission from Bennu in support of the requirement to measure emitted radiation globally.[ citation needed ]

Based on the performance of Mini-TES in the dusty surface environment of Mars, OTES was designed to be resilient to extreme dust contamination on the optical elements.[ citation needed ]

REXIS

The Regolith X-ray Imaging Spectrometer (REXIS) will provide an X-ray spectroscopy map of Bennu to map element abundances. [95] REXIS is a collaborative development by four groups within Massachusetts Institute of Technology (MIT) and Harvard University, with the potential to involve more than 100 students throughout the process. REXIS is based on flight heritage hardware, thereby minimizing elements of technical risk, schedule risk, and cost risk. [99]

REXIS is a coded aperture soft X-ray (0.3–7.5 keV) telescope that images X-ray fluorescence line emission produced by the absorption of solar X-rays and the solar wind with elements in the regolith of Bennu leading to local X-ray emissions. Images are formed with 21  arcminute resolution (4.3 m spatial resolution at a distance of 700 m). Imaging is achieved by correlating the detected X-ray image with a 64×64 element random mask (1.536 mm pixels). REXIS will store each X-ray event data in order to maximize the data storage usage and to minimize the risk. The pixels will be addressed in 64×64 bins and the 0.3–7.5 keV range will be covered by five broad bands and 11 narrow line bands. A 24-second resolution time tag will be interleaved with the event data to account for Bennu rotation. Images will be reconstructed on the ground after downlink of the event list. Images are formed simultaneously in 16 energy bands centered on the dominant lines of abundant surface elements from O-K (0.5 keV) to Fe-Kß (7 keV) as well the representative continuum. During orbital phase 5B, a 21-day orbit 700 m from the surface of Bennu, a total of at least 133 events/asteroid pixel/energy band are expected under 2 keV; enough to obtain significant constraints on element abundances at scales larger than 10 m.[ citation needed ]

On 11 November 2019, while observing the asteroid with REXIS, university students and researchers involved in the mission unexpectedly discovered an X-ray burst from a black hole named MAXI J0637-430 located 30,000 light-years away. [100]

OLA

The OSIRIS-REx Laser Altimeter (OLA) is a scanning and lidar instrument that will provide high resolution topographical information throughout the mission. [95] The information received by OLA creates global topographic maps of Bennu, local maps of candidate sample sites, ranging in support of other instruments, and support navigation and gravity analyses.[ citation needed ]

OLA scans the surface of Bennu at specific intervals to rapidly map the entire surface of the asteroid to achieve its primary objective of producing local and global topographic maps. The data collected by OLA will also be used to develop a control network relative to the center of mass of the asteroid and to enhance and refine gravitational studies of Bennu.[ citation needed ]

OLA has a single common receiver and two complementary transmitter assemblies that enhance the resolution of the information brought back. OLA's high-energy laser transmitter is used for ranging and mapping from 1 to 7.5 km (0.62 to 4.66 mi). The low-energy transmitter is used for ranging and imaging from 0.5 to 1 km (0.31 to 0.62 mi). The repetition rate of these transmitters sets the data acquisition rate of OLA. Laser pulses from both the low and high energy transmitters are directed onto a movable scanning mirror, which is co-aligned with the field of view of the receiver telescope limiting the effects of background solar radiation. Each pulse provides target range, azimuth, elevation, received intensity and a time-tag.[ citation needed ]

OLA was funded by the Canadian Space Agency (CSA) and was built by MDA at Brampton, Ontario, Canada. [101] OLA was delivered for integration with the spacecraft on 17 November 2015. [102] The lead instrument scientist of OLA is Michael Daly from York University. [103]

TAGSAM

TAGSAM arm test before launch Osiris-Rex Sample-return-arm-test-167.jpg
TAGSAM arm test before launch

The sample-return system, called Touch-And-Go Sample Acquisition Mechanism (TAGSAM), consists of a sampler head with an articulated 3.35 m (11.0 ft) arm. [2] [95] An on-board nitrogen source supports up to three separate sampling attempts to acquire at least 60 g (2.1 oz) of sample in all. The surface contact pads also collect fine-grained material.[ citation needed ]

Highlights of the TAGSAM instrument and technique include:

  • Relative approach velocity of 10 cm/s (3.9 in/s) [104]
  • Contact within 25 m (82 ft) of selected location
  • OCAMS documents sampling at 1 Hz
  • Collect samples in less than five seconds, direct nitrogen (N2) annular jet fluidizes regolith, surface-contact pad captures surface sample
  • Verify bulk sample collection via spacecraft inertia change; surface sample by imaging sampler head
  • Sampler head stored in sample-return capsule and returned to Earth

Cooperation with JAXA

Hayabusa2 is a similar mission from JAXA to collect samples from near-Earth asteroid 162173 Ryugu. It arrived at the asteroid in June 2018, left in November 2019 after two successful sample collections, and returned to Earth in December 2020. The recovery capsule of Hayabusa2 re-entered Earth atmosphere and landed in Australia, as planned, on 5 December 2020. The sample contents were to be extensively analyzed, including water content, to provide clues on the initial formation of the asteroid. The main module of Hayabusa2 is performing a swing-by procedure to "push" it onward to its next destination, asteroid 1998KY26, by 2031. Because the two missions were similar and had overlapping timelines (OSIRIS-REx was still in the return phase), NASA and JAXA signed an agreement to collaborate on sample exchange and research. [105] [106] The two teams visited each other, with representatives from JAXA visiting the OSIRIS-REx Science Operations Center at the University of Arizona, and members of the OSIRIS-REx team traveling to Japan to meet with the Hayabusa2 team. [107] [108] The teams are sharing software, data, and techniques for analysis, and will eventually exchange portions of the samples that are returned to Earth. [109] [110]

OSIRIS-REx II

OSIRIS-REx II was a 2012 mission concept to replicate the original spacecraft for a double mission, with the second vehicle collecting samples from the two moons of Mars, Phobos and Deimos. It was stated that this mission would be both the quickest and least expensive way to get samples from the moons. Mars I and II are now the aims of another mission, led by JAXA, called MMX, to be launched in 2024. [111] [112] [113]

See also

Notes

  1. Origins, Spectral Interpretation, Resource Identification, Security, Regolith Explorer

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Daniella ("Dani") Mendoza DellaGiustina is a Mexican American planetary scientist and academic. She is the principal investigator for NASA's OSIRIS-APEX Mission to asteroid (99942) Apophis, Deputy Principal Investigator of NASA's OSIRIS-REx Asteroid Sample Return Mission, and assistant professor at the University of Arizona's Lunar and Planetary Laboratory.

References

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OSIRIS-REx
OSIRIS-APEX
OSIRIS-REx spacecraft model.png
Artist's rendering of the OSIRIS-REx spacecraft
NamesOSIRIS-REx
OSIRIS-APEX
Mission typeAsteroid sample return [1]
Operator NASA / Lockheed Martin
COSPAR ID 2016-055A OOjs UI icon edit-ltr-progressive.svg
SATCAT no. 41757
Website www.asteroidmission.org
Mission duration7 years (planned)
889 days at asteroid (actual)
7 years, 6 months, 23 days (elapsed)
Spacecraft properties
ManufacturerLockheed Martin
Launch mass2,110 kg (4,650 lb) [2]
Dry mass880 kg (1,940 lb)
Dimensions2.44 × 2.44 × 3.15 m (8 ft 0 in × 8 ft 0 in × 10 ft 4 in)
Power1226 to 3000 watts
Start of mission
Launch date8 September 2016, 23:05 UTC [3]
Rocket Atlas V 411 (AV-067)
Launch site Cape Canaveral SLC-41
Contractor United Launch Alliance (ULA)
End of mission
DisposalSample Return Capsule: Recovered
Landing dateSample Return Capsule: 24 September 2023, 14:52 UTC [4]
Landing site Utah Test and Training Range [4]
Orbital parameters
Reference system Bennu-centric
Altitude0.68–2.1 km (0.42–1.30 mi) [5] [6]
Period 22–62 hours [7] [6]
Flyby of Earth
Closest approach22 September 2017 [2] [8]
Distance17,237 km (10,711 mi)