What to Expect When Hayabusa2 Blows a Hole in Asteroid Ryugu
If you enjoyed the drama of Hayabusa2's sample collection touchdown, get ready for an even bigger fireworks display. The spacecraft is about to deploy an explosives-filled box that will detonate in space, fire a copper plate into Ryugu, and create a crater up to 10 meters wide. The moment of crater generation is set for 5 April at 02:36 UTC. Here's what to expect.
Hayabusa2 SCI artist's concept
This artist's concept shows Hayabusa2 deploying the Small Carry-on Impactor, SCI (left), and then hiding behind Ryugu (right) as the device explodes, shooting a copper plate into the surface. The DCAM3 camera system watches in the foreground.
Hayabusa2 is a Japanese mission to collect a sample from asteroid Ryugu and return it to Earth in 2020.
Why is JAXA doing this?
The goal of the Small Carry-on Impactor experiment—SCI for short—is to learn more about how asteroids like Ryugu change over time. More specifically, JAXA scientists are hoping to learn:
How big a crater will form on Ryugu from an impactor of known mass and speed, by comparing before and after pictures at the crater site
What the materials beneath Ryugu's surface that haven't been exposed to space weathering look like
Whether or not the surface moves easily when struck by an impactor
How easily boulders shatter due to impacts, if the impactor happens to hit a boulder
There's a lot of uncertainty involved with SCI, which makes it a really interesting experiment. Scientists aren't quite sure how big the crater will be. They can only aim SCI to a certain degree; the target spot has a margin of error of 200 meters. The width of the crater will depend on the type of material the impactor hits. Most models estimate a crater up to 10 meters wide, but there are a few surface types that could result in either a very small crater (if the impactor hits a particularly porous spot) or a crater even larger than 10 meters (if it hits a bunch of tiny, coarse pebbles). The crater depth is expected to be about a tenth of its diameter, which is actually a rule of thumb for simple, bowl-shaped craters anywhere in the solar system!
The target area is near Ryugu's equator, about a quarter of the way around the asteroid east of the first sample collection site. That’s roughly 300 meters from MASCOT’s final resting place, so it’s not impossible that SCI could hit quite close to the now-dead lander. Since the Hayabusa2 team might also collect a sample from this artificial crater, they chose a spot geologically similar to the first touchdown site, allowing for an above-and-beneath-the-surface comparison. The location is also relatively free of hazards, which should help for a future touchdown.
Ryugu surface map
Ryugu's surface with labeled major features and locations, as of early March 2019.
Here’s an image of Ryugu with the SCI target spot just a bit left of center:
JAXA, University of Tokyo, Kochi University, Rikkyo University, Nagoya University, Chiba Institute of Technology, Meiji University, University of Aizu, AIST
Kolobok crater and environs, Ryugu
At 240 meters in diameter, Kolobok is one of Ryugu's largest craters. It is located on the equator at 1.5°S and 333.5°E. Several other smaller craters are located on or near its rim. Above and slightly to the right of it, most of it in deep shadow, is another large crater, Cendrillon.
How are they making the crater?
Rather than drop a bomb directly on Ryugu's surface and heavily contaminate the area with plastic explosives, the plan is to lessen contamination by turning a bomb into a space gun that fires a copper plate into the surface. You wouldn't expect to find copper on Ryugu, so this will help scientists distinguish between native and non-native Ryugu materials later. This is also the reason the sample collection process involves a bullet made of tantalum.
The SCI experiment is a small cylinder 30 centimeters in diameter and about 22 centimeters long. It sticks out from the bottom of Hayabusa2, near the meter-long sample horn:
Hayabusa2 components, bottom view
Here's SCI before integration. SCI itself is on the right; the left piece is a cover with a white, reflective wrap that makes it easier for SCI to be imaged from a distance after deployment. The gold cap is standard spacecraft insulation that the copper projectile will blow right through.
Hayabusa2 SCI experiment
Hayabusa2's SCI experiment. SCI itself is on the right; the copper projectile comes from the bottom. On the left is a thermal cover that was added before launch.
Inside the SCI cylinder is a funnel filled with plastic explosives, capped on the wide end with a 2-kilogram curved copper plate. Delightfully, in both an academic paper and JAXA press materials, this funnel is simply referred to as the "explosive part."
Saiki et. al (2017) / JAXA
Hayabusa2 SCI "explosive part"
These diagrams show the "explosive part," a plastic explosive-packed funnel capped with a copper plate installed inside Hayabusa2's deployable SCI experiment.
Hayabusa2 will deploy SCI from a height of 500 meters and start a 40-minute timer before detonation. The cylinder has no means of attitude control, so Hayabusa2 will give it a slight spin to stabilize it as it gently falls toward Ryugu.
And then, Hayabusa2 will run. It will first make a "horizontal retreat," sliding sideways for about a kilometer. Then, it will drop off a camera system called DCAM3 to watch the fireworks (more on that in a moment) before making a "vertical retreat" until it is safely shielded from the SCI explosion by Ryugu.
Hayabusa2 SCI sequence
This chart shows the sequence of events for Hayabusa2's SCI operation.
Here are the key SCI event times. All are in Earth-received time; to calculate the time the event occurred aboard the spacecraft, subtract 17 minutes.
19:13 4 April
22:13 4 April
02:13 5 April
11:13 5 April
19:31 4 April
22:31 4 April
02:31 5 April
11:31 5 April
SCI detonation and crater formation
19:53 4 April
22:53 4 April
02:53 5 April
11:53 5 April
JAXA hasn't listed an exact height at which SCI will detonate. Full-scale tests on Earth were conducted at 100 meters, and a 2017 paper said the cylinder would fall to at least 200 meters while Hayabusa2 escaped, so it's safe to say somewhere between 100 and 200 meters. When detonation occurs, it will take just milliseconds for the "explosive part" to accelerate the copper plate to a speed of about 2 kilometers per second, much faster than the sample collection bullet that travels at 300 meters per second. The curved copper plate will actually turn inside out and become helmet-shaped before it slams into Ryugu.
Hayabusa2 SCI copper plate deformation
The copper plate from Hayabusa2's SCI experiment deforms as it flies toward the surface.
If all goes well, Hayabusa2 will stay in direct line-of-sight with DCAM3 while being shielded from high-speed SCI debris and crater ejecta.
What will we see?
Before answering what we'll see from SCI, let's look at what we won't see. Here's a video made from 2011 full-scale tests of SCI on Earth. WARNING: IT'S VERY LOUD. I jumped the first time I watched the test, but was so awestruck I left the audio levels intact, and used the track from the microphone closest to the experiment for both camera angles.
WARNING: LOUD. This video shows two camera angles from a test of Hayabusa2's SCI experiment on Earth in 2011. The copper projectile fires from a concrete bunker, penetrates several gridded targets, and hits a mound of dirt simulating asteroid Ryugu 100 meters away.
It would be incredible to see that video recreated in microgravity, but sadly, DCAM3 will be a kilometer away. Here's an approximation of what we might actually see:
Saiki et. al (2017)
Hayabusa2 simulated DCAM3 view
A simulated view of what DCAM3 might see during the Hayabusa2 SCI experiment.
That's still pretty cool! DCAM3, or Deployable Camera 3, is an evolution of the DCAM1 and DCAM2 systems that were used during JAXA's IKAROS mission in 2010. IKAROS, you might recall, was the world's first steerable solar sail that hitched a ride to interplanetary space on the rocket that sent Akatsuki to Venus.
IKAROS sail from DCAM2
One of the deployable cameras on IKAROS shows the IKAROS solar sail fully deployed.
DCAM3 has two cameras: one low-resolution color analog camera that will transmit to Hayabusa2 in real-time, and a higher-resolution monochrome digital camera that will send images later. DCAM3's battery will only last 3 hours, but its signal is strong enough to reach Hayabusa2 10 kilometers away. There's also a camera called MCAM that will image DCAM3 as it pops loose from Hayabusa2.
To avoid any slow-speed crater ejecta that briefly enters orbit around Ryugu before either falling back to the surface or getting pushed into space due to solar radiation pressure, Hayabusa2 will wait 2 weeks before returning to its 20-kilometer home position. Eventually, the spacecraft will return to the scene of the crime to see what happened. The team already collected pre-SCI imagery of the crater formation area from a height of about 1.7 kilometers. These images will help the team locate the new, artificial crater.
Then, they will decide whether to perform a second touchdown, either in the artificial crater they just created, or at a nearby location called S01, which they observed in detail from 6 to 8 March at a height of 22 meters. A second touchdown wouldn't happen until June at the earliest.
One final note: The mission has updated their spacecraft renderings based on what they now know about Ryugu (don't miss Emily's new article that discusses this in detail!). Here are before-and-after shots of Hayabusa2 touching down. The surface certainly turned out to be a lot rockier than expected!
Akihiro Ikeshita / JAXA
Hayabusa2 render before and after arrival
Before and after renders of Hayabusa2 touching down on Ryugu highlight the difference between the expected and actual terrain on the asteroid.