Double Asteroid Redirection Test (DART) is a NASA space mission aimed at testing a method of planetary defense against near-Earth objects (NEOs).[3][4] It was designed to assess how much a spacecraft impact deflects an asteroid through its transfer of momentum when hitting the asteroid head-on.[5] The asteroid selected for the test poses no actual threat to Earth and was selected for the convenience of the test. The probe was launched from Earth on 24 November 2021, and on 26 September 2022 intentionally crashed into Dimorphos, the minor-planet moon of the asteroid Didymos.[6] On 11 October, NASA declared DART a success, confirming it had shortened Dimorphos' orbital period around Didymos by about 32 minutes, surpassing the pre-defined success threshold of 73 seconds.[7][8]
2021 NASA space mission
This article is about the impactor mission. For the Earth orbiter, see DART (satellite).
Double Asteroid Redirection Test
Diagram of the DART spacecraft striking Dimorphos.
Didymos Reconnaissance and Asteroid Camera for Optical navigation (DRACO)
DART mission patch
Solar System Exploration program
Europa Clipper→
DART is a joint project between NASA and the Johns Hopkins Applied Physics Laboratory (APL). The project was funded through NASA's Planetary Defense Coordination Office, managed by NASA's Planetary Missions Program Office at the Marshall Space Flight Center, and several NASA laboratories and offices provided technical support. International partners, such as the European Space Agency (ESA), Italian Space Agency (ASI), and Japan Aerospace Exploration Agency (JAXA), are contributing to related or subsequent projects.[9]
Mission history
NASA and the European Space Agency (ESA) started with individual plans for missions to test asteroid deflection strategies, but by 2015, they struck a collaboration called AIDA (Asteroid Impact and Deflection Assessment) involving two separate spacecraft launches that would work in synergy.[10][11][12] Under that proposal, the European spacecraft, AIM, would have launched in December 2020, and DART in July 2021. AIM would have orbited the larger asteroid to study its composition and that of its moon. DART would then kinetically impact the asteroid's moon on 26 September 2022, during a close approach to Earth.[11]
The AIM orbiter was however canceled, then replaced by Hera which plans to start observing the asteroid four years after the DART impact. Live monitoring of the DART impact thus had to be obtained from ground-based telescopes and radar.[13][12]
In June 2017, NASA approved a move from concept development to the preliminary design phase,[14] and in August 2018 the start of the final design and assembly phase of the mission.[15] On 11 April 2019, NASA announced that a SpaceX Falcon 9 would be used to launch DART.[16]
Satellite impact on an asteroid had already been implemented once, by NASA's 372kg (820lb)Deep Impact space probe's impactor spacecraft and for a completely different purpose (analysis of the structure and composition of a comet). On impact, Deep Impact released 19 gigajoules of energy (the equivalent of 4.8 tons of TNT),[17] and excavated a crater up to 150m (490ft) wide.[18]
Description
Spacecraft
The DART spacecraft was an impactor with a mass of 610kg (1,340lb)[19] that hosted no scientific payload and had only sensors for navigation.
Camera
DRACO camera
DART's navigation sensors included a sun sensor, a star tracker called SMART Nav software (Small-body Maneuvering Autonomous Real Time Navigation),[20] and a 20cm (7.9in) aperture camera called Didymos Reconnaissance and Asteroid Camera for Optical navigation (DRACO). DRACO was based on the Long Range Reconnaissance Imager (LORRI) onboard New Horizons spacecraft, and supported autonomous navigation to impact the asteroid's moon at its center. The optical part of DRACO was a Ritchey-Chrétien telescope equipped with telephoto lens with a field of view of 0.29° and a focal length of 2.6208 m (f/12.60). The spatial resolution of the images taken immediately before the impact are expected to be around 20 centimeters per pixel. The instrument had a mass of 8.66kg (19.1lb).[21]
The detector used in the camera was a CMOS image sensor measuring 2,560 × 2,160 pixels. The detector records the wavelength range from 0.4 to 1 micron (visible and near infrared). A commercial off-the-shelf CMOS detector was used instead of a custom charge-coupled device in LORRI, as DRACO did not require the extreme low-light performance demanded of LORRI during New Horizons' Pluto flyby. DRACO's detector performance actually met or exceeded that of LORRI because of the improvements in sensor technology in the decade separating the design of LORRI and DRACO.[22] Fed into an onboard computer with software descended from anti-missile technology, the DRACO images helped DART autonomously guide itself to its crash.[23]
Solar arrays
The spacecraft's solar arrays used a Roll Out Solar Array (ROSA) design, that was tested on the International Space Station (ISS) in June 2017 as part of Expedition 52.[24]
Using ROSA as the structure, a small portion of the DART solar array was configured to demonstrate Transformational Solar Array technology, which has very-high-efficiency SolAero Inverted Metamorphic (IMM) solar cells and reflective concentrators providing three times more power than current other solar array technology.[25]
Antenna
The DART spacecraft was the first spacecraft to use a new type of high-gain communication antenna, a Spiral Radial Line Slot Array (RLSA). The circularly-polarized antenna operates at the X-band NASA Deep Space Network (NASA DSN) frequencies of 7.2 and 8.4 GHz, and has a gain of 29.8 dBi on downlink and 23.6 dBi on uplink. The fabricated antenna in a flat and compact shape exceeds the given requirements and has been tested through environments resulting in a TRL-6 design.[26]
NASA's Evolutionary Xenon Thruster (NEXT)
Ion thruster
DART spacecraft used the NEXT gridded ion thruster, a type of solar electric propulsion.[13][27] It was powered by 22m2 (240sqft) solar arrays to generate the ~3.5kW needed to power the NASA Evolutionary Xenon Thruster–Commercial (NEXT-C) engine.[28] Early tests of the ion thruster revealed a reset mode that induced higher current (100 A) in the spacecraft structure than expected (25 A). It was decided not to use the ion thruster further as the mission could be accomplished without it, using conventional thrusters. However, the ion thrusters remained available if needed to deal with contingencies, and had DART missed its target, the ion system could have returned DART to Dimorphos two years later.[29]
Secondary spacecraft
LICIACube CubeSat, a companion satellite of the DART spacecraft
The Italian Space Agency (ASI) contributed a secondary spacecraft called LICIACube (Light Italian CubeSat for Imaging of Asteroids), a small CubeSat that piggybacked with DART and separated on 11 September 2022, 15 days before impact. It acquired images of the impact and ejecta as it drifted past the asteroid.[30][31] LICIACube communicated directly with Earth, sending back images of the ejecta after the Dimorphos flyby.[32][33] LICIACube is equipped with two optical cameras, dubbed LUKE and LEIA.[34]
Effect of the impact on Dimorphos and Didymos
The spacecraft hit Dimorphos in the direction opposite to the asteroid's motion. Following the impact, the orbital speed of Dimorphos therefore dropped slightly, which reduced the radius of its orbit around Didymos. The trajectory of Didymos was also modified, but in inverse proportion to the ratio of its mass to the much lower mass of Dimorphos. The actual velocity change and orbital shift depended on the topography and composition of the surface, among other things. The contribution of the recoil momentum from the impact ejecta produces a poorly predictable "momentum enhancement" effect.[35] Before the impact, the momentum transferred by DART to the largest remaining fragment of the asteroid was estimated as up to 3–5 times the incident momentum, depending on how much and how fast material would be ejected from the impact crater. Obtaining accurate measurements of that effect was one of the mission's main goals and will help refine models of future impacts on asteroids.[36]
The DART impact excavated surface/subsurface materials of Dimorphos, leading to the formation of a crater and/or some magnitude of reshaping (i.e., shape change without significant mass loss). Some of the ejecta may eventually hit Didymos's surface. If the kinetic energy delivered to its surface is high enough, reshaping may also occur in Didymos, given its near-rotational-breakup spin rate. Reshaping on either body will modify their mutual gravitational field, leading to a reshaping-induced orbital period change, in addition to the impact-induced orbital period change. If left unaccounted for, this could lead to an erroneous interpretation of the effect of the kinetic deflection technique.[37]
Observations of the impact
Telescopes observing DART's impactAstronomers using the NSF’s NOIRLab’s SOAR telescope in Chile captured the vast plume of dust and debris blasted from the surface of the asteroid Dimorphos by NASA’s DART spacecraft when it impacted on 26 September 2022. In this image, the more than 10,000 kilometer long dust trail — the ejecta that has been pushed away by the Sun’s radiation pressure, not unlike the tail of a comet — can be seen stretching from the center to the right-hand edge of the field of view.
DART's companion LICIACube,[38][32]Hubble Space Telescope, James Webb Space Telescope and the Earth-based ATLAS observatory all detected the ejecta plume from the DART impact.[39][40] On September 26, SOAR observed the visible impact trail to be over 10,000 km long.[41] Initial estimates of the change in binary orbit period were expected within a week and with the data released by LICIACube.[42] DART's mission science depends on careful Earth-based monitoring of the orbit of Dimorphos over the subsequent days and months. Dimorphos was too small and too close to Didymos for almost any observer to see directly, but its orbital geometry is such that it transits Didymos once each orbit and then passes behind it half an orbit later. Any observer that can detect the Didymos system therefore sees the system dim and brighten again as the two bodies cross. The impact was planned for a moment when the distance between Didymos and Earth is at a minimum, permitting many telescopes to make observations from many locations. The asteroid will be near opposition and visible high in the night sky into 2023.[43] The change in Dimorphos's orbit around Didymos was detected by optical telescopes watching mutual eclipses of the two bodies through photometry on the Dimorphos-Didymos pair. In addition to radar observations, they confirmed that the impact shortened Dimorphos' orbital period by 32 minutes.[44]
Follow-up mission
In a collaborating project, the European Space Agency is developing Hera, a spacecraft that will be launched to Didymos in 2024[30][45][46] and arrive in 2026.[47][48] (5 years after DART's impact), to do a detailed reconnaissance and assessment.[46]Hera would carry two CubeSats, Milani and Juventas.[46]
Shape model of Didymos and its satellite Dimorphos, based on photometric light curve and radar data
The mission's target was Dimorphos in 65803 Didymos system, a binary asteroid system in which one asteroid is orbited by a smaller one. The primary asteroid (Didymos A) is about 780m (2,560ft) in diameter; the asteroid moon Dimorphos (Didymos B) is about 160m (520ft) in diameter in an orbit about 1km (0.62mi) from the primary.[13] The mass of the Didymos system is estimated at 528billion kg, with Dimorphos comprising 4.8billion kg of that total.[19] Choosing a binary asteroid system is advantageous because changes to Dimorphos's velocity can be measured by observing when Dimorphos subsequently passes in front of its companion, causing a dip in light that can be seen by Earth telescopes. Dimorphos was also chosen due to its appropriate size; it is in the size range of asteroids that one would want to deflect, were it on a collision course with Earth. In addition, the binary system was relatively close, about 11millionkm (7millionmi), to the Earth in 2022.[57] The Didymos system is not an Earth-crossing asteroid, and there is no possibility that the deflection experiment could create an impact hazard.[58] On 4October 2022, Didymos made an Earth approach of 10.6millionkm (6.6millionmi).[59]
Preflight preparations
DART being encapsulated in the Falcon 9 payload fairing on 16 November 2021
Launch preparations for DART began on 20 October 2021, as the spacecraft began fueling at Vandenberg Space Force Base (VSFB) in California.[60] The spacecraftarrived at Vandenberg in early October2021 after a cross-country drive. DART team members prepared the spacecraft for flight, testing the spacecraft's mechanisms and electrical system, wrapping the final parts in multilayer insulation blankets and practicing the launch sequence from both the launch site and the mission operations center at APL.DART headed to the SpaceX Payload Processing Facility on VSFB on 26 October 2021. Two days later, the team received the green light to fill DART's fuel tank with roughly 50kg (110lb) of hydrazine propellant for spacecraft maneuvers and attitude control. DART also carried about 60kg (130lb) of xenon for the NEXT-C ion engine. Engineers loaded the xenon before the spacecraft left APL in early October 2021.[61]
Starting on 10 November 2021, engineers mated the spacecraft to the adapter that stacks on top of the SpaceX Falcon 9 launch vehicle. The Falcon 9 rocket without the payload fairing rolled for a static fire and later came back to the processing facility again where technicians with SpaceX installed the two halves of the fairing around the spacecraft over the course of two days, 16 and 17 November, inside the SpaceX Payload Processing Facility at Vandenberg Space Force Base and the ground teams completed a successful Flight Readiness Review later that week with the fairing then attached to the rocket.[62]
A daybefore launch, the launch vehicle rolled out of the hangar and onto the launch pad at Vandenberg Space Launch Complex 4 (SLC-4E); from there, it lifted off to begin DART's journey to the Didymos system and it propelled the spacecraft into space.[61]
Launch
DART separation from second stage
The DART spacecraft was launched on 24 November 2021, at 06:21:02 UTC.
Early planning suggested that DART was to be deployed into a high-altitude, high-eccentricity Earth orbit designed to avoid the Moon. In such a scenario, DART would use its low-thrust, high-efficiency NEXT ion engine to slowly escape from its high Earth orbit to a slightly inclined near-Earth solar orbit, from which it would maneuver onto a collision trajectory with its target. But because DART was launched as a dedicated Falcon 9 mission, the payload along with Falcon 9's second stage was placed directly on an Earth escape trajectory and into heliocentric orbit when the second stage reignited for a second engine startup or escape burn. Thus, although DART carries a first-of-its-kind electric thruster and plenty of xenon fuel, Falcon 9 did almost all of the work, leaving the spacecraft to perform only a few trajectory-correction burns with simple chemical thrusters as it homed in on Didymos's moon Dimorphos.[63]
The transit phase before impact lasted about 9 months. During its interplanetary travel, the DART spacecraft made a distant flyby of the 578-meter-diameter near-Earth asteroid (138971) 2001 CB21 in March 2022.[64] DART passed 0.117AU (17.5millionkm; 10.9millionmi) from 2001 CB21 in its closest approach on 2 March 2022.[65]
DART's DRACO camera opened its aperture door and took its first light image of some stars on 7 December 2021, when it was 3millionkm (2millionmi) away from Earth.[66] The stars in DRACO's first light image were used as calibration for the camera's pointing before it could be used to image other targets.[66] On 10 December 2021, DRACO imaged the open clusterMessier 38 for further optical and photometric calibration.[66]
On 27 May 2022, DART observed the bright star Vega with DRACO to test the camera's optics with scattered light.[67] On 1 July and 2 August 2022, DART's DRACO imager observed Jupiter and its moon Europa emerging from behind the planet, as a performance test for the SMART Nav tracking system to prepare for the Dimorphos impact.[68]
Course of the impact
Two months before the impact, on 27 July 2022, the DRACO camera detected the Didymos system from approximately 32millionkm (20millionmi) away and started refining its trajectory. The LICIACube nanosatellite was released on 11 September 2022, 15 days before the impact.[69] Four hours before impact, some 90,000km (56,000mi) away, DART began to operate in complete autonomy under control of its SMART Nav guidance system. Three hours before impact, DART performed an inventory of objects near the target. Ninety minutes before the collision, when DART was 38,000km (24,000mi) away from Dimorphos, the final trajectory was established.[70] When DART was 24,000km (15,000mi) away Dimorphos became discernible (1.4 pixels) through the DRACO camera which then continued to capture images of the asteroid's surface and transmit them in real-time.[71]
DRACO was the only instrument able to provide a detailed view of Dimorphos' surface. The use of DART's thrusters caused vibrations throughout the spacecraft and solar panels, resulting in blurred images. To ensure sharp images, the last trajectory correction was executed 4 minutes before impact and the thrusters were deactivated afterwards.[71]
Compiled timelapse of DART's final 5.5 minutes until impact
The last full image, transmitted two seconds before impact, has a spatial resolution of about 3 centimeters per pixel. The impact took place on 26 September 2022, at 23:14 UTC.[2]
The head-on impact of the 500kg (1,100lb)[72] DART spacecraft at 6.6km/s (4.1mi/s)[73] likely imparted an energy of about 11 gigajoules, the equivalent of about three tonnes of TNT,[74] and was expected to reduce the orbital velocity of Dimorphos between 1.75cm/s and 2.54cm/s, depending on numerous factors such as material porosity.[75] The reduction in Dimorphos's orbital velocity brings it closer to Didymos, resulting in the moon experiencing greater gravitational acceleration and thus a shorter orbital period. Although the change in Dimorphos's orbit is small, the offset in its orbital position will accumulate and become more noticeable over time.[11][58][76] The orbital period reduction from the head-on impact serves to facilitate ground-based observations of Dimorphos. An impact to the asteroid's trailing side would increase its orbital period to 12 hours and coincide with Earth's day and night cycle, which would limit ground-based telescopes from observing all orbital phases of Dimorphos nightly.[43]
The impact targeted the center of Dimorphos and decreased the orbital period, previously 11.92 hours, by roughly 32 minutes.[19]
While the orbital change in this case was small, the change is in the velocity and over the course of years will accumulate to a large change in position.[77] For a hypothetical Earth-threatening body, even such a tiny change, if applied early enough, could be sufficient to mitigate or prevent an impact. As the diameter of Earth is only around 13,000 kilometers, a hypothetical asteroid impact could be avoided with as little of a shift as half of that (6,500 kilometers). A 2cm/s velocity change accumulates to that distance in approximately 10 years.
Ejection of LICIACube, which maneuvers to avoid crashing into the asteroid.[69]
26 September 2022 19:14 UTC (T-4 hours)
89,000km (55,000mi)
Terminal phase—start of autonomous navigation with SMART Nav. DRACO locks onto Didymos since Dimorphos is not visible yet.[2]
22:14 UTC (T-60 minutes)
22,000km (14,000mi)
The DRACO camera detects Dimorphos.
22:54 UTC (T-20 minutes)
7,500km (4,700mi)
SMART Nav enters precision lock onto Dimorphos and DART begins thrusting toward Dimorphos.[2]
23:10 UTC (T-4 minutes)
1,500km (930mi)
Start of final course correction
23:11 UTC (T-2 minutes 30 seconds)
920km (570mi)
Last image with both Didymos (lower-left) and Dimorphos entirely in frame is taken
23:12 UTC (T-2 minutes)
740km (460mi)
End of final course correction
23:14 UTC (T-20 seconds)
130km (81mi)
The photos taken reach the expected spatial resolution.
23:14 UTC (T-11 seconds)
68km (42mi)
Last image showing all of Dimorphos by DART
23:14 UTC (T-3 seconds)
18km (11mi)
23:14 UTC (T-2 seconds)
12km (7.5mi)
Final complete image of Dimorphos transmitted. Resolution roughly 3 cm per pixel (~ 30m across).
23:14 UTC (T-1 second)
6km (3.7mi)
Last partial image taken by DART before impact, transmission of the image was interrupted by the destruction of the spacecraft and all of its transmitting hardware. Resolution per pixel to be determined at a later date by analysis of image and timing.
DART Mission animated video from launch to impact along with separation of LICIACube
Size of DART and the two Didymos asteroids
Infographic showing the effect of DART's impact on the orbit of Didymos B and the deployment of LICIACube
Views of the Didymos and Dimorphos binary asteroid system obtained from radar facilities at NASA Jet Propulsion Laboratory’s Goldstone planetary radar in California and the National Science Foundation’s Green Bank Observatory
The images show a series of radar images captured at different times on Oct. 9, 2022, of the Didymos and Dimorphos binary asteroid system obtained from radar facilities at NASA JPL
This chart offers insight into data the DART team used to determine the orbit of Dimorphos after impact
This animation showing a highly magnified view of how Dimorphos’ orbit around Didymos is seen from Earth
See also
Asteroid impact avoidance– Methods to prevent destructive asteroid hits
"Double Asteroid Redirection Test (DART)". NASA. 28 October 2021. Retrieved 5 November 2021. This article incorporates text from this source, which is in the public domain.
Bray, Matthew (2020). "A Spiral Radial Line Slot Array Antenna for NASA's Double Asteroid Redirection Test (DART)". 2020 IEEE International Symposium on Antennas and Propagation and North American Radio Science Meeting. pp.379–380. doi:10.1109/IEEECONF35879.2020.9330400. ISBN978-1-7281-6670-4. S2CID231975847.
Kantsiper, Brian (2017). "The Double Asteroid Redirection Test (DART) mission electric propulsion trade". 2017 IEEE Aerospace Conference. pp.1–7. doi:10.1109/AERO.2017.7943736. ISBN978-1-5090-1613-6. S2CID43072949.
Launches are separated by dots (•), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ). CubeSats are smaller. Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in brackets).
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