In October 2017, the interstellar object 'Oumuamua passed through our solar
system, leaving many questions in its wake. Not only was it the first object
of its kind ever observed, but the limited data astronomers obtained as it
shot out of our solar system left them all scratching their heads. Even
today, almost five years after this interstellar visitor made its flyby,
scientists are still uncertain about its true nature and origins. In the
end, the only way to get real answers from 'Oumuamua is to catch up with it.
Interestingly enough, there are many proposals on the table for missions
that could do just that. Consider Project Lyra, a proposal by the Institute
for Interstellar Studies (i4is), which would rely on advanced propulsions
technology to rendezvous with interstellar objects (ISOs) and study them.
According to their latest study, if their mission concept launched in 2028
and performed a complex Jupiter Oberth maneuver (JOM), it would be able to
catch up to 'Oumuamua in 26 years.
On October 30th, 2017, less than two weeks after 'Oumuamua was detected, the
Initiative for Interstellar Studies (i4is) inaugurated Project Lyra. The
purpose of this concept study was to determine if a mission to rendezvous
with 'Oumuamua was feasible using current or near-term technologies. Since
then, the i4is team has conducted studies that considered catching up with
the ISO using nuclear-thermal propulsion (NTP) and a laser sailcraft,
similar to Breakthrough Starshot—an interstellar mission concept for
reaching Alpha Centauri in 20 years.
As they describe in their study, most of the previously proposed methods for
reaching 1I/'Oumuamua using near-term technologies call for a solar Oberth
maneuver (SOM). A perfect example is the Sundiver, a proposal by researcher
Coryn Bailer-Jones of the Max Planck Institute for Astronomy (MPIA). As he
described to Universe Today in a previous article, this concept relies on
the sun's radiation pressure to obtain a very high velocity with a light
sail.
"The principle of the Oberth effect is to apply your boost when you are
moving fastest relative to the body you are orbiting, which is the sun, in
the case of the Sundiver," he said. "The closer you are to the sun in your
orbit, the faster you will be. So to take advantage of the Oberth effect,
you need to get as close to the sun as possible."
At the heart of the SOM and other Oberth maneuvers is a technique known as a
gravity assist, which has been used to explore the solar system since the
early 1970s. This technique involves using the gravitational force of three
bodies, including the spacecraft, a second body that provides the "assist"
(typically a large planet), and the central body about which the
spacecraft's path is being controlled.
Adam Hibberd, a researcher with the i4is, was the lead author of this latest
Lyra study, titled "Project Lyra: A Mission to 1I/'Oumuamua without solar
Oberth maneuver." Before joining i4is, Hibberd was an aerospace engineer who
developed the Optimum Interplanetary Trajectory Software (OITS). When
'Oumuamua was detected, he decided to use OITS with this ISO as the intended
destination. After finding out about Project Lyra, he joined them and their
research efforts shortly afterward.
As he explained to Universe Today via email, the solar Oberth maneuver (SOM)
relies on three discrete changes in velocity (aka. impulses) to exit the
solar system. These include:
- At Earth, to increase the spacecraft's farthest distance from the sun (aphelion),
- At aphelion, to slow down and fall in close to the sun,
- At the closest point to the sun (perihelion), when the spacecraft is traveling at it fastest, to get an extra boost
"This three-impulse scenario was discovered by Theodore Edelbaum in 1959,
although the term SOM seems to have stuck. It is fuel-optimal for generating
high speeds out of the solar system. This is precisely what is needed to
catch an ISO when the ISO has passed perihelion and is receding quickly from
the sun.
"However, this theoretical setup disregards Jupiter. Thus, as a slight
modification to this, if we slow down in step 2 with the help of a reverse
Jupiter gravitational assist, then we can achieve escape with even less
fuel. It is because the SOM is so efficient at generating high speeds that
it has been used to research missions to ISOs."
Looking for alternatives to a SOM, Hibbert and his colleagues considered
using a time-tested route that would incorporate Jupiter's powerful
gravitational pull. Part of their motivation for this was the inherent
challenges a solar gravity assist maneuver presents. While this maneuver
looks great on paper, it has never been executed before, and therefore has a
low technology readiness level (TRL) rating.
What's more, there's the issue of how much heating will take place as the
spacecraft achieves perihelion during step 3 (between 3 and 10 solar radii).
These issues were addressed in a recent NASA Solar and Space Physics concept
study titled "Interstellar Probe: Humanity's Journey to Interstellar Space."
This study was conducted for the Solar and Space Physics 2023–2032 Decadal
Survey, which included (among others) concepts for an interstellar probe. In
Appendix D2.2., the study addresses thermal protection in the context of a
solar Oberth maneuver:
"Unlike earlier missions, where a shield design was needed for a given sun
distance, the Interstellar Probe challenge is to see how close to the sun a
spacecraft can realistically get. As the solar distance decreases, the umbra
angle increases, and the size of the shield, relative to the spacecraft,
grows significantly.
"Because a conceptual design effort cannot include all the material design,
fabrication and testing limitations of the full design, the final
recommendation of allowable sun distance is made based on where the design
seems to be moving from very difficult to impossible."
As the Parker Solar Probe amply demonstrates, getting close to the sun
requires a heat shield that can handle extreme heat and radiation. In the
case of Parker, that shield measures about 2.44 meters (8 ft) in diameter
and weighs almost 72.5 kg (160 lbs). While the size and mass of a heat
shield for Lyra would not be identical, it's a fair bet that a solar heat
shield would result in a lot of additional mass for the lightsail.
As an alternative, Hibberd and his team recommended a Jupiter Oberth
maneuver (JOM), which would launch from Earth, swing around Venus and Earth,
conduct a deep space maneuver (DSM), swing by Earth again, then receive a
gravity assist using Jupiter's gravitational pull. This is summarized by the
acronym V-E-DSM-E-J, or the more commonly used V-E-E-GA—Venus, Earth, Earth,
Gravity Assist. As Hibberd indicated, this maneuver would have several
advantages over a SOM, among them:
"[It] would not require a heavy heat shield and also would not need: a) An
extra travel distance from Jupiter to the solar Oberth of around 5.2
astronomical units (au), [and] b) A further travel back to around Jupiter's
orbit of an additional 5.2 au. Both (a) & (b) would take time for a SOM
which would not be required for a Jupiter Oberth maneuver."
"JOM is a discovery which is key to the remit of Project Lyra to find
options using current or near-term technology, as essentially, it does not
require any hardware or maneuvers which have not been tried before, unlike
the SOM. Nevertheless, despite the saving in time from not requiring (a) and
(b) above—the lower escape speeds generated by the JOM mean the mission
duration must be longer."
Another advantage Hibberd and his team identified was the arrival speed of
the spacecraft, which would be much slower than one relying on a SOM—18 km/s
(64,800 km/h; 40,265 mph) vs. 30 km/s (108,000 km/h; 67,108 mph). This would
give the spacecraft more time to analyze 'Oumuamua during approach and
departure. Based on a launch window of 2028, they determined that a Project
Lyra spacecraft would be able to catch up to 'Oumuamua by 2054.
Given that 'Oumuamua is the closest piece of interstellar material
accessible to us, the scientific returns for a rendezvous mission would be
immeasurable. For the relatively low cost of a rendezvous mission, humanity
could get its first glimpse of what goes on in other star systems by
mid-century. More to the point, it would be a chance to finally resolve the
many questions 'Oumuamua raised when it made its historic flyby of Earth
years ago.
Was it a nitrogen iceberg? Was it aliens? Was it something else entirely? If
we play our cards right, we will know the answers to all of these questions
by mid-century.
Reference:
Adam Hibberd, Andreas Hein, Marshall Eubanks, Robert Kennedy III, Project
Lyra: A Mission to 1I/'Oumuamua without Solar Oberth Manoeuvre.
arXiv:2201.04240v1 [astro-ph.EP],
arxiv.org/abs/2201.04240
Tags:
Space & Astrophysics