Two primary methods exist for deflecting asteroids: the nuclear approach, which involves detonating bombs to destroy the asteroid but risks fragmenting it into multiple dangerous pieces that could still hit Earth; and the gravitational tractor beam approach, which uses a space probe to match the asteroid's orbit, apply gentle gravitational forces through retro rockets, and slowly redirect the asteroid's path away from Earth without breaking it apart.
Deflecting an Asteroid: Planetary Defense Science Explained
Added:Basic orbital mechanics, including Kepler's laws of planetary motion and how celestial bodies orbit the Sun.

Kepler's three laws form the foundation of celestial mechanics, describing how celestial bodies move under gravitational influence. The two-body problem involves two bodies interacting through a central force following the inverse-square law, resulting in conic section trajectories. Kepler's First Law states planets orbit in ellipses with the Sun at one focus. An ellipse is defined as the set of points where the sum of distances to two foci is constant, with eccentricity (e = c/a) characterizing shape: e = 0 gives a circle, 0 < e < 1 gives an ellipse, e = 1 gives a parabola, and e > 1 gives a hyperbola. Kepler's Second Law states that a line joining a planet to the Sun sweeps out equal areas in equal times, following from conservation of angular momentum L = r × mv. Kepler's Third Law states that the square of the orbital period is proportional to the cube of the semi-major axis: T² ∝ a³, with the general form T² = (4π²/GM)a³ for systems where one body dominates the mass.

Johannes Kepler formulated three fundamental laws describing planetary motion: (1) Planets orbit the Sun in ellipses with the Sun at one focus; (2) Planets sweep out equal areas in equal times, meaning they move faster when closer to the Sun and slower when farther away; (3) The square of a planet's orbital period is proportional to the cube of its semi-major axis (distance from the Sun). These laws describe the basic mechanics of orbital motion. To describe any orbit mathematically, six orbital elements are needed: orbital inclination (angle between orbital plane and ecliptic), length of ascending node (orientation of intersection line relative to vernal equinox), argument of perihelion (orientation of closest approach point), eccentricity (shape of orbit: 0=circular, 0-1=elliptical, 1=parabolic, >1=hyperbolic), semi-major axis (size of orbit), and mean anomaly (position in orbit at a specific time).

Kepler's three laws describe the motion of celestial bodies in orbit around the Sun. The first law states that all planets move in elliptical orbits with the Sun at one focus. The second law states that a line connecting a planet to the Sun sweeps out equal areas in equal times, meaning planets move faster when closer to the Sun (perihelion) and slower when farther away (aphelion). The third law states that the square of the orbital period is proportional to the cube of the semi-major axis of the orbit, relating the size of an orbit directly to its period.

Kepler's three laws describe planetary motion around the Sun. First Law: Planets orbit in ellipses with the Sun at one focus. Second Law: A line from the Sun to a planet sweeps equal areas in equal times, meaning orbital speed increases when closer to the Sun. Third Law: The square of the orbital period is proportional to the cube of the semi-major axis (T² ∝ a³). These laws were discovered by Kepler in the early 1600s from Tycho Brahe's observations, but the physical explanation (gravity) was not found until Newton in 1686.

Johannes Kepler formulated three fundamental laws describing planetary motion. First Law: Planets orbit the Sun in elliptical paths with the Sun at one focus. Second Law: A line connecting the Sun to a planet sweeps equal areas in equal time intervals, meaning planets move faster when closer to the Sun. Third Law: The square of a planet's orbital period equals the cube of its semi-major axis, establishing a mathematical relationship between orbital distance and time.
Newton's laws of motion and gravity, specifically the principles of momentum transfer, kinetic energy, and gravitational attraction.

Gravity is just about momentum - it gives things momentum. It functions just like heat or other mechanical things. Bigger things can be understood by hitting something and transferring energy. Gravity is giving something momentum through the same process as an electron hitting inside an atom.

Newton formulated three fundamental laws of motion that form the basis of classical mechanics. The First Law states that a body remains at rest or in uniform rectilinear motion unless acted upon by another body. The Second Law states that the net force applied to a body is proportional to the acceleration it acquires, with the constant of proportionality being the body's mass. The Third Law states that when one body exerts a force on another, the second body exerts an equal and opposite force on the first. Newton applied these principles to celestial mechanics, proposing that the force keeping the Moon in orbit around Earth is the same force keeping Earth in orbit around the Sun. This led to the Law of Universal Gravitation, which states that gravitational force between two bodies depends on their masses and the distance between them. This law enables calculation of gravitational attraction between any two bodies and prediction of celestial movements.

This section covers Newton's laws of motion and gravitational principles. Newton's First Law states that a body remains at rest or moves with constant velocity unless acted on by an external force. Newton's Second Law states that force equals mass times acceleration (F = ma), with force measured in newtons. Newton's Third Law states that for every action, there is an equal and opposite reaction. Weight equals mass times gravitational acceleration (W = mg). The acceleration of gravity on Earth is 9.8 m/s², representing gravitational field strength. All objects free fall at the same rate regardless of mass because gravitational force per unit mass is constant. Momentum (p) is the product of mass and velocity (p = mv). The Law of Conservation of Momentum states that total momentum before any interaction equals total momentum after the interaction.

Building on Galileo and Descartes, Newton developed new theories about gravity. He discovered that objects exert force over one another when they collide, sending them in different directions along a straight line of center of gravity. He concluded that particles or atoms attract each other with gravitational force correlating to mass and distance between them. His third law states that every action has an equal and opposite reaction—for example, when jumping, gravity pulls you back downward by the same distance. These laws represented a fundamental expansion of human understanding of how gravity and motion work.

Newton's First Law states objects remain at rest or in uniform motion unless acted upon by an external force. Newton's Second Law states acceleration depends on mass and applied force (F=ma). Newton's Third Law states every action has an equal and opposite reaction. Gravitational attraction is mutual between all objects in the universe—the Earth and Moon attract each other, not just one attracting the other.
The definition and classification of Near-Earth Objects (NEOs) and the general composition of asteroids.

Near-Earth Objects (NEOs) are asteroids and comets that orbit the Sun very close to Earth's orbit. Some NEOs orbit at the same distance as Earth, making them co-orbital objects. These objects are classified into three categories based on their orbital characteristics: Apollo asteroids (cross Earth's orbit with larger orbits), Aten asteroids (cross Earth's orbit with smaller orbits), and Atira asteroids (completely inside Earth's orbit). Scientists have identified approximately 14,000 NEOs, which represent potential threats to Earth due to their proximity.

Near Earth Objects (NEOs) are space objects such as asteroids or comets whose orbits around the Sun place them close to Earth. The term 'close' in astronomical terms means being less than 1.3 astronomical units from Earth, where one astronomical unit equals 93 million miles (150 million km). This distance is approximately equal to the distance from Earth to the Sun. An object classified as a NEO does not necessarily mean it will collide with Earth; it simply means scientists must monitor it carefully.

Near-earth objects (NEOs) are celestial bodies in our solar system, including comets and asteroids, whose orbits bring them within 1.3 astronomical units (AU) of the Sun—where 1 AU equals Earth's distance from the Sun. These objects are remnants from solar system formation, with NASA cataloging approximately 18,500 asteroids and 107 comets. Asteroids form between Mars and Jupiter in the asteroid belt, consisting of rocky and metallic material with impact craters. Comets originate from the outer solar system in the Kuiper belt and Oort cloud, composed of ice, dust, and rock, earning them the nickname 'dirty snowballs.' Both types lack sufficient mass for spherical shapes and have impacted Earth throughout history, including events potentially linked to dinosaur extinction.

Asteroids are classified into three broad composition types based on spectral analysis: C-type (carbonaceous, over 75% of known asteroids, dark, clay/silicate rocks, oldest solar system objects, found in outer belt); S-type (silicaceous, ~17%, bright, iron-magnesium silicates, dominate inner belt); and M-type (metallic, bright, mostly iron, inhabit middle belt). Near-Earth asteroids (NEAs) within 1.3 AU of the Sun represent fragments ejected from the main belt by collisions and Jupiter's gravity, potentially including dead comet nuclei. NEAs are categorized into three groups: Amor asteroids crossing Mars' orbit but not reaching Earth; Apollo asteroids crossing Earth's orbit with orbital periods over one year; and Aten asteroids crossing Earth's orbit with periods under one year. NASA monitors NEAs due to potential impact risks.

The solar system contains billions of objects beyond the commonly known planets, including asteroids, meteoroids, and comets orbiting in stable regions like the asteroid belt, Kuiper belt, and Oort cloud. Near Earth Objects (NEOs) are asteroids or comets whose closest approach to the Sun is 1.3 astronomical units or less, and whose closest approach to Earth is 0.3 astronomical units or less. NEOs are classified into three types: Amor asteroids (orbits cross Mars and Jupiter but never Earth), Apollo asteroids (orbits extend beyond Earth's orbit), and Aten asteroids (most dangerous, remain in proximity to Earth's orbit). Potentially Hazardous Asteroids (PHAs) are objects with a minimum diameter of 140-150 meters and a closest approach to Earth of no more than 7.5 million kilometers. Currently, approximately 1,800 PHAs have been cataloged, though none are expected to impact Earth in the near future.
Prerequisite Knowledge
- Concept 01Basic orbital mechanics, including Kepler's laws of planetary motion and how celestial bodies orbit the Sun.
- Concept 02Newton's laws of motion and gravity, specifically the principles of momentum transfer, kinetic energy, and gravitational attraction.
- Concept 03The definition and classification of Near-Earth Objects (NEOs) and the general composition of asteroids.
Subsequent Learning
- Step 01Case studies of real-world planetary defense missions, such as NASA's Double Asteroid Redirection Test (DART).
- Step 02Advanced deflection technologies, including gravity tractors, laser ablation, solar sails, and nuclear mitigation strategies.
- Step 03The physical properties of asteroids, such as the difference between solid monoliths and 'rubble piles', and how this affects deflection dynamics.
- Step 04The geopolitical and legal frameworks of planetary defense, including international space law and global coordination groups like the Asteroid Warning Network (IAWN).
Two Deflection Ways
0:00- 1
Asks for top two asteroid deflection methods.
- 2
First method is explosive nuclear destruction.
- 3
Second is a gentle gravitational tractor approach.
The Deflection Dilemma and Dual-Use Risks
While asteroid deflection methods like kinetic impactors are scientifically feasible, they introduce a profound geopolitical risk known as the 'Deflection Dilemma,' first popularized by Carl Sagan and Steven J. Ostro. This perspective argues that any technology capable of deflecting an asteroid away from Earth could also be weaponized to steer a benign asteroid toward a target on Earth, creating an existential dual-use hazard. Additionally, technical critics emphasize the risk of 'disruption' over deflection: attempts to nudge a rubble-pile asteroid could accidentally shatter it, creating a swarm of smaller, unpredictable fragments that could still devastate Earth. Consequently, some experts argue that developing these technologies before establishing foolproof international governance poses a greater threat to humanity than the natural impact hazard itself.
Case studies of real-world planetary defense missions, such as NASA's Double Asteroid Redirection Test (DART).

NASA's Double Asteroid Redirection Test (DART) was a $325 million mission that intentionally crashed a spacecraft into asteroid Dimorphos on September 26th, marking humanity's first planetary defense test. The mission tested kinetic impactor technology, which uses spacecraft to deflect near-Earth objects by changing their orbits. DART targeted the binary asteroid system Didymos, colliding at 14,000 miles per hour. The mission employed SMART Nav for autonomous navigation and LICIACube for imaging. Scientists will measure orbital changes using light curves and the European Space Agency's Hera mission will conduct follow-up surveys in 2026. This real-world test demonstrates humanity's capability to handle asteroid deflections and informs future planetary defense strategies.

NASA's DART (Double Asteroid Redirection Test) mission represents humanity's first real-world planetary defense test. The 500-kilogram satellite will impact Dimorphos, a 160-meter asteroid orbiting Didymos, to test whether spacecraft can successfully alter asteroid trajectories. The satellite will travel at 6.6 km/s in the opposite direction to Dimorphos's motion, slowing it slightly to reduce its orbit. The mission demonstrates that even small initial impacts can produce massive trajectory changes over millions of miles. NASA's Sentry program tracks near-Earth asteroids and maintains risk tables, with current highest-risk objects having only a 2.5% chance of impact by 2082.

NASA's Double Asteroid Redirection Test (DART) mission demonstrates humanity's first planetary defense test to see if intentionally crashing a spacecraft into an asteroid can change its course, using the binary asteroid system Didymos and Dimorphos as a safe testbed; the spacecraft will autonomously navigate to impact Dimorphos at approximately 15,000 miles per hour to alter its orbital period around Didimos, with scientists measuring the deflection effects through telescopic observations, onboard cameras, and future missions like the Italian cubesat LICIACube and ESA's Hera spacecraft.

NASA's Double Asteroid Redirection Test (DART) was the first planetary defense mission to successfully demonstrate the kinetic impactor technique by intentionally crashing a spacecraft into the asteroid Dimorphos, thereby altering its orbital period around its parent asteroid Didymos by 33 minutes—far exceeding the mission's minimum requirement of 73 seconds—and proving that human intervention can change an object's trajectory in space.

The Double Asteroid Redirection Test (DART) is NASA's first demonstration of the kinetic impactor technique to change an asteroid's motion in space. The mission intentionally crashes a spacecraft into the binary asteroid Dimorphos (160m diameter) to deflect its trajectory, testing whether this approach could protect Earth from hazardous asteroids. The spacecraft uses electric propulsion (NEXT-C system) and autonomous navigation with DRACO camera. The mission targets the Didymos system because Dimorphos's size represents typical Earth-threatening asteroids. Despite no known large asteroids threatening Earth for 100 years, only 40% of such asteroids have been discovered. The mission will be monitored by Earth-based telescopes and planetary radar to measure the orbital period change caused by the impact.
Advanced deflection technologies, including gravity tractors, laser ablation, solar sails, and nuclear mitigation strategies.

Several deflection strategies exist: kinetic impactors (colliding spacecraft with asteroids), asteroid-versus-asteroid (using non-threatening asteroids to knock Earthbound objects off course), and nuclear explosions (standoff detonations that heat and blow off surface material). Solar sails concentrate sunlight to vaporize surface rock, creating propulsion jets. Lasers cause material to fly off asteroids, pushing them away. Each method has trade-offs - nuclear options are most efficient but banned from space by treaty, while lasers and solar sails face implementation challenges with long-term positioning and dust management. The gravity tractor, developed by the B612 Foundation, uses ion engines to hover near an asteroid, using gravitational pull to slowly change its trajectory. It's about the size of a golf cart and can make precise adjustments over weeks, months, or years. The B612 Foundation aims to perform a test deflection on a non-threatening asteroid by 2015.

Advanced deflection technologies include solar sails and laser systems. Solar sails use concentrated sunlight to heat asteroid surfaces, creating vapor jets that push the asteroid away from its trajectory. A 1980s experiment accidentally discovered that laser pulses can cause material to vaporize and be ejected from surfaces, demonstrating the principle behind these deflection methods. A proposed super-laser system, powered by rockets and solar panels, could be positioned 5 kilometers from an asteroid and use short pulses to vaporize surface material, creating thrust. The laser can be directed precisely and gradually, potentially over several years. However, maintaining the laser or solar sail in the correct position for extended periods is challenging, and the expelled dust could affect the system's effectiveness. Nuclear deflection, while potentially most effective for large asteroids, is complicated by international treaties prohibiting nuclear weapons in space.

Alternative asteroid deflection methods include using solar sails and lasers. One innovative concept involves spraying paint on an asteroid to make it highly reflective, so sunlight exerts radiation pressure to push it off course—similar to how solar sails work. More practical is using powerful lasers to ablate (heat and vaporize) the asteroid's surface, creating a rocket-like effect where the vaporized material provides thrust. Lasers offer advantages over nuclear weapons: they deliver energy continuously rather than in single bursts, can be precisely controlled, and the light travels near-instantaneously across interplanetary distances, allowing real-time adjustments to deflection efforts.

Advanced deflection technologies include laser systems and solar sails. Laser deflection uses powerful light beams to vaporize surface material on asteroids, creating jets that push the object off course. This method is economical and can be performed by a robotic spacecraft over a 3-month period. The technology was discovered accidentally in the 1980s when researchers observed material being ejected from silicon wafers during laser experiments. A super laser 5,000 times more powerful than everyday lasers could be used, positioned up to 5 km away from the asteroid. Solar sails use orbiting reflectors to concentrate sunlight on asteroids, vaporizing surface rock and creating propulsion. Both methods eject only dust, posing no threat to Earth, but require precise positioning over extended periods. The gravity tractor, developed by the B612 Foundation, uses gravitational attraction to slowly pull asteroids off course without physical contact. It hovers near asteroids using ion engines to counteract gravitational pull, making precise adjustments after primary deflection.

Advanced planetary defense methods include using solar sails to change asteroid trajectories. By reflecting sunlight off a reflective surface, the radiation pressure can gradually push an asteroid off course. Alternatively, a gravity tractor spacecraft could use gravitational attraction to slowly pull an asteroid away from a collision course without physically touching it.
The physical properties of asteroids, such as the difference between solid monoliths and 'rubble piles', and how this affects deflection dynamics.

When OSIRIS-REx's manipulator touched Bennu's surface, instead of bouncing off like a concrete wall, it sank 50 centimeters into the asteroid with almost no resistance. The spacecraft could have completely sunk into Bennu's interior if emergency thrusters hadn't fired. This was not landing on rock but jumping into a pool of plastic balls. Laboratory analysis confirmed density is only 1.2 grams per cubic centimeter—slightly denser than water and much less dense than any Earth rock. This means up to 40% of the asteroid's volume is empty space. These asteroids are essentially giant cosmic sponges made of stone. For laypeople, this sounds like good news (easier to destroy), but for ballistics specialists, it's a nightmare scenario. Impact physics differs dramatically between solid and rubble-pile asteroids. A strike on a monolith transfers energy throughout the body, changing its trajectory. A strike on a rubble pile is absorbed internally, dissipated through friction between rocks and compression of voids. Like trying to push a heavy oak cabinet versus a bag filled with feathers and down, the same force produces vastly different results. Rubble piles can absorb enormous kinetic energy while maintaining their trajectory. Explosive deflection methods also fail against rubble piles. Shock waves that would crack or push a solid monolith dissipate almost instantly in porous material. The explosive energy is absorbed as heat, leaving only a small crater on the surface while the asteroid continues its deadly path. The Yarkovsky effect, predicted by Russian engineer Ivan Yarkovsky in 1900, describes how solar heating creates tiny but persistent forces on rotating asteroids. One side of an asteroid heats up during the day, then cools and radiates heat into space during the night. By Newton's third law, this creates a constant sideways thrust. This force is tiny—equivalent to the weight of a sheet of paper on a palm—but in the frictionless vacuum of space, it accumulates over years, potentially shifting a 40-million-ton asteroid by tens or hundreds of kilometers. For Apophis, flying toward a 600-meter keyhole, even a 0.5 km shift is the difference between life and death. The Yarkovsky effect makes precise orbit prediction impossible because we don't know Apophis's exact shape, thermal properties, or rotation axis.

Many asteroids are 'rubble piles' - loose aggregations of rocks held together by gravity rather than solid bodies. This structure affects deflection strategies because impactors may not penetrate deeply, and fragments may re-aggregate. The OSIRIS-REx mission to asteroid Bennu demonstrated that rubble pile asteroids have complex surface dynamics that complicate sample collection and deflection attempts.

Scientists do not know the internal structure of the target asteroid Dimorphos until after the DART impact. The asteroid could be either a solid rock or a 'rubble pile' - a loosely bound collection of rocks and dust held together by gravity. This uncertainty is significant because the impact effectiveness depends heavily on the asteroid's structure. If Dimorphos is a rubble pile, much of the impact energy will be absorbed in crushing the spaces between particles, resulting in less effective deflection. If it is a solid rock, the impact will transfer momentum more efficiently, similar to hitting a solid bowling ball.

Models describing how asteroids form, how they evolve after collisions, and how they might be approached, redirected, or mined for resources all depend heavily on assumptions about internal structure. A rubble pile responds to an impact, a gravitational tug, or an attempted deflection maneuver completely differently than something closer to a single solid mass. If a meaningful fraction of large asteroids turn out to be built more like solid rock than loose gravel, held together by cohesive strength rather than gravity alone, every calculation involving how to nudge a dangerous asteroid off a collision course would need to be re-examined against a completely different set of physical assumptions. A deflection technique calculated to work against a loosely bound pile of rubble, gently redirecting its overall trajectory without disturbing its fragile internal structure, could behave in an entirely unpredictable way if aimed instead at something closer to a single cohesive mass.

Most smaller asteroids are rubble pile asteroids—collections of rock and debris held together loosely by mutual gravity rather than being solid monolithic bodies. These form when asteroid collisions break up larger bodies into debris clouds that gravity pulls back together into loose aggregates. They are less dense and more porous than solid asteroids. This structure means destroying them with nuclear weapons is ineffective, as the explosion simply disperses debris that gravity will reassemble. Defense strategies must instead focus on deflecting these asteroids entirely rather than attempting to destroy them.
The geopolitical and legal frameworks of planetary defense, including international space law and global coordination groups like the Asteroid Warning Network (IAWN).

The International Asteroid Warning Network (IAWN) is a global coordination system operated by NASA that tracks asteroids and comets worldwide. It serves as the primary mechanism for planetary defense, coordinating international efforts to monitor potentially hazardous objects and assess potential threats to Earth.

The International Asteroid Warning Network (IAWN), an independent international collaboration under the United Nations Office for Outer Space Affairs and the International Astronomical Union, has launched a public campaign to monitor the interstellar comet 3I/ATLAS, which is older than Earth and the Sun (estimated 7,000-11,000 million years old) and has a nucleus of approximately 5-11 km diameter; this campaign is not a military defense operation but a scientific initiative to improve astrometric measurements of comets, open to public participation through a virtual workshop and observation coordination, with the goal of contributing to future planetary defense systems.

This segment details the international planetary defense framework. The International Asteroid Warning Network (IAWN) serves as the 'eyes,' detecting and tracking hazardous objects. The Space Situational Awareness program acts as the 'brain,' developing response plans. NASA's Planetary Defense Coordination Office serves as the 'hands,' implementing actions. Alert thresholds exist: objects over 10 meters with greater than 1% collision probability trigger formal warnings. This system requires coordination between scientific assessment and political will, with exercises conducted in 2019 and 2024 to test response capabilities.

Planetary defense requires international cooperation because asteroid impacts transcend national boundaries. The United Nations Office for Outer Space Affairs coordinates global efforts through the International Asteroid Warning Network (IAWN) and Space Mission Planning Advisory Group (SMPAG). ESA maintains comprehensive planetary defense capabilities including observation, orbit prediction, and mitigation planning. The FlyEye network addresses observational gaps. Astronaut perspectives highlight that while robotic missions like Hera are preferable for dangerous destinations, human missions to asteroids may become feasible in the future. This framework enables coordinated response planning among space agencies, representing a model for addressing global challenges through international scientific cooperation.

Since September, NASA and the European Space Agency activated a planetary defense observation campaign under the International Asteroid Warning Network (IAWN). This is not because there is danger, but as a real exercise in tracking a real interstellar visitor. The campaign continues as the comet moves away from the solar system.
Two Deflection Ways
0:00- 1
Asks for top two asteroid deflection methods.
- 2
First method is explosive nuclear destruction.
- 3
Second is a gentle gravitational tractor approach.
The Deflection Dilemma and Dual-Use Risks
While asteroid deflection methods like kinetic impactors are scientifically feasible, they introduce a profound geopolitical risk known as the 'Deflection Dilemma,' first popularized by Carl Sagan and Steven J. Ostro. This perspective argues that any technology capable of deflecting an asteroid away from Earth could also be weaponized to steer a benign asteroid toward a target on Earth, creating an existential dual-use hazard. Additionally, technical critics emphasize the risk of 'disruption' over deflection: attempts to nudge a rubble-pile asteroid could accidentally shatter it, creating a swarm of smaller, unpredictable fragments that could still devastate Earth. Consequently, some experts argue that developing these technologies before establishing foolproof international governance poses a greater threat to humanity than the natural impact hazard itself.
Give me your top two ways to deflect an asteroid.
>> Uh, well, there's the macho way. You're imagining the the war general. You know, let's blow the sucker out of the sky.
You know, we got nukes. Let's So, you send out nukes and you destroy it and then it becomes harmless little bits that then burn up in an atmosphere. But the problem is we're really good at blowing stuff up and we're less good at knowing where the pieces go afterwards.
Suppose you blow up and then now it's two pieces. Now, you have to evacuate two parts of Earth instead of just one.
A kindler, gentler solution would be they've worked on a gravitational tractor beam where you send a space probe and you match orbits and you put it adjacent to the asteroid and watch what happens and you park it there and there they are moving. Well, they'll feel each other's gravity and they'll want to move towards one another, but you have little retro rockets on your space probe and you don't let that happen. You have actually attracted it out of the path of harm's way. It'll still be there to harm you in another day.
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