Europe is a full partner for this Artemis ll flight.
Europe is a full partner for this Artemis ll flight.
Gemini Ai:
Gravity-assist; all fine and good that Artemis will be speeding up thanks to gravity-assist from the Moon, but won't the Moon be pulling Artemis back once the latter starts returning to Earth??
That is a sharp observation. It seems counterintuitive that a celestial body can "give" speed to a spacecraft without immediately "taking it back" as the craft pulls away.
The resolution lies in the fact that the Moon is not stationary; it is moving in its own orbit around the Earth at approximately 1,022 meters per second. A gravity assist is less about "falling" into a gravity well and more about hitching a ride on a moving target.
The Frame of Reference
To understand why the speed isn't lost, we have to look at the maneuver from two different perspectives:
Relative to the Moon: As Artemis approaches, it speeds up due to gravity. As it departs, it slows down by the exact same amount. In this local frame, there is no net gain in speed—only a change in direction.
Relative to the Earth (or Sun): This is where the magic happens. Because the Moon is moving, Artemis "steals" a tiny fraction of the Moon's orbital momentum.
The "Tennis Racket" Analogy
Think of the Moon as a moving tennis racket and Artemis as a tennis ball.
If you throw a ball at a stationary racket, it bounces back at the same speed it arrived.
If you swing the racket toward the ball, the ball leaves the strings with its original speed plus the speed of your swing.
When Artemis flies "behind" the Moon in its orbital path, the Moon’s gravity pulls the spacecraft along with it. By the time Artemis begins to move away, it has already been accelerated forward by the Moon’s own orbital velocity.
Why the Moon doesn't "pull it back"
While the Moon does exert a backward pull as Artemis departs, it is pulling on a spacecraft that is now traveling much faster relative to the Earth than it was before the encounter.
The "cost" of this maneuver is technically a slowdown of the Moon. Because the Moon is trillions of times more massive than the Artemis capsule, the Moon slows down by a distance roughly equivalent to the width of a single atom over billions of years, while the light spacecraft gains several hundred meters per second in velocity.
Key Factors in the Artemis Return
For the return trip, NASA uses a Powered Flyby. This involves:
Vectoring: Aiming the craft so the Moon’s gravity bends the trajectory toward Earth.
The Oberth Effect: Firing engines at the "Periapsis" (the closest point to the Moon). Burning fuel while moving at high speeds deep in a gravity well is significantly more efficient than burning it in empty space, allowing Artemis to maximize the "kick" it gets for the trip home.
Copilot:
Artemis Moon Mission; does saying that Artemis will approach the Moon 'from the back' come down to saying it will be crossing over in the same direction as the moon is rotating?
Here’s the clean, physics‑based answer you’re looking for — and the short version is no: “approaching the Moon from the back” does not mean Artemis is crossing the Moon’s rotation direction.
🌙 Short Answer
Saying Artemis approaches the Moon “from the back” refers to approaching the Moon from its far side along a free‑return, figure‑8 trajectory — not the direction of the Moon’s rotation.
It’s about orbital geometry relative to Earth, not about matching the Moon’s spin direction.
🛰️ What “from the back” actually means
NASA’s Artemis missions (including Artemis II) use a free‑return trajectory, where the spacecraft:
Leaves Earth on a path that naturally swings it behind the Moon (the far side)
Uses the Moon’s gravity to bend the trajectory back toward Earth
Does not enter lunar orbit
This is described in the sources as a “figure‑8” path” that “swings the spacecraft around the far side of the Moon” .
This geometry is chosen for:
Safety (automatic return to Earth if propulsion fails)
Efficiency (gravity assist instead of braking into orbit)
Mission design (Artemis II is a flyby, not an orbital insertion)
🔄 Why it has nothing to do with the Moon’s rotation
The Moon rotates very slowly — one rotation every ~27 days — and its rotation direction is irrelevant to Artemis’s approach.
Key points:
The spacecraft is not trying to match the Moon’s spin.
The approach direction is determined by Earth–Moon orbital mechanics, not lunar rotation.
“Back” is a geometric term: the far side relative to Earth, not the trailing side relative to the Moon’s motion.
Even if the Moon rotated the opposite way, Artemis’s trajectory would be the same.
🧭 A clearer way to visualize it
Imagine the Moon orbiting Earth. Artemis is launched into a path that intersects the Moon’s orbit on the far‑side arc, so that:
It passes behind the Moon relative to Earth
The Moon’s gravity bends the spacecraft’s path back toward Earth
The spacecraft never needs to brake into lunar orbit
This is exactly the “figure‑8” free‑return path described in the Artemis II mission coverage .
🧩 If you did mean “trailing side” (the Moon’s orbital motion)
Sometimes people confuse “back of the Moon” with the trailing hemisphere — the side opposite the direction of the Moon’s orbit around Earth.
That’s a different concept entirely, and Artemis is not specifically targeting the trailing hemisphere either.
✔️ Bottom Line
“From the back” = from the far side (geometric), not from the trailing side (orbital motion), and not aligned with the Moon’s rotation.
It’s all about the free‑return trajectory that loops behind the Moon and slingshots back toward Earth.
If you want, I can sketch the geometry in words or walk you through the figure‑8 trajectory step by step — it’s a beautiful piece of orbital mechanics.
Seen from the Top, does the Moon rotate clockwise or counterclockwise?
The Moon rotates counterclockwise when viewed from above the Earth’s North Pole (i.e., “from the top”). This is the same direction in which it orbits Earth.
🌙 Direction of the Moon’s Rotation (Seen From Above the North Pole)
Rotation on its axis: Counterclockwise
Revolution around Earth: Counterclockwise
Why: The Moon is tidally locked, so its rotation period matches its orbital period, but both motions still have a definite direction — counterclockwise when viewed from the north.
This is the standard “prograde” direction shared by most major bodies in the Solar System.
🧭 What if you looked from the South Pole instead?
Perspective flips everything:
From above the South Pole, the same physical rotation appears clockwise.
This is purely a viewpoint effect — the Moon’s actual rotation direction doesn’t change.
If you want, I can also explain how this ties into the “far side,” “leading/trailing hemispheres,” or Artemis mission trajectories — they’re all related but often confused.
Does Artemis' speed gain while circling the Moon happen because one adds its proper speed to that of the Moon's rotation speed?
Great question — and this is exactly where many explanations of Artemis trajectories accidentally create confusion.
Let’s clear it up cleanly and precisely.
🚀 Short Answer
No. Artemis does not gain speed by adding its own velocity to the Moon’s rotation.
The Moon’s rotation is far too slow to matter, and it plays no role in the spacecraft’s speed gain.
Artemis gains (or loses) speed because of gravity assist mechanics — the spacecraft exchanges energy with the Moon’s orbital motion around Earth, not its rotation.
🌙 Why the Moon’s rotation is irrelevant
The Moon rotates once every ~27 days.
That’s only 4.6 km/h at the equator — slower than a brisk walk.
Artemis travels at thousands of km/h.
So adding the Moon’s rotation speed would be like adding a bicycle’s speed to a jet airplane. It simply doesn’t matter.
🛰️ Where the real speed change comes from
The key is this:
✔️ The Moon orbits Earth at ~1 km/s
✔️ Artemis approaches the Moon with its own velocity
✔️ The Moon’s gravity bends Artemis’ trajectory
✔️ This bending changes Artemis’ speed relative to Earth, not relative to the Moon
This is the classic gravity assist (or gravitational slingshot) effect.
The spacecraft “steals” a tiny bit of the Moon’s orbital momentum, changing its own energy relative to Earth.
🔄 What actually happens during Artemis’ lunar flyby
Depending on the geometry:
If Artemis passes behind the Moon (relative to the Moon’s motion), it gets a speed boost.
If it passes in front of the Moon, it gets slowed down.
This is exactly the same physics used in Voyager, Galileo, Cassini, and New Horizons flybys.
The Moon’s rotation never enters the equation.
Only the Moon’s orbital motion and gravity matter.
🧭 Why people get confused
The phrase “approaching from the back” sounds like:
“the back of the Moon”
“the trailing side”
“the side opposite the rotation direction”
But in Artemis mission language, “from the back” simply means:
→ approaching the Moon from the far side,
→ on a free‑return trajectory,
→ where the Moon’s gravity bends the spacecraft back toward Earth.
It has nothing to do with rotation.
✔️ Bottom Line
Artemis’ speed gain comes from gravitational interaction with the Moon’s orbital motion, not its rotation.
The Moon’s rotation is too slow to matter and plays no role in the spacecraft’s velocity change.
If you want, I can also explain the difference between:
far side vs. trailing side,
free‑return vs. orbital insertion,
or draw a verbal diagram of the gravity‑assist geometry.
Just let me know — this is a fun topic to unpack.
And that is the Dark side??
Not quite — and this is one of the most persistent space‑myth traps out there.
Let’s untangle it cleanly.
🌑 Is the “far side” the “dark side”?
No.
The “dark side of the Moon” is a misleading phrase. The far side is not permanently dark.
✔️ Far side
The hemisphere that always faces away from Earth
This is what people mean when they say “the back of the Moon”
Artemis swings around this side on its free‑return trajectory
✔️ Dark side
A poetic but incorrect term
Every part of the Moon experiences day and night
The far side gets just as much sunlight as the near side
The only time a whole hemisphere is dark is during a lunar phase, and it alternates
So the far side ≠ dark side.
☀️ Why the far side isn’t dark
The Moon rotates once every ~27 days, and it orbits Earth in the same period.
Because of this synchronous rotation:
The same face always points toward Earth
But the Sun still illuminates both hemispheres over the lunar month
The far side has a “lunar noon,” “lunar sunset,” etc., just like the near side
The only reason we don’t see the far side is geometry, not darkness.
🚀 How this relates to Artemis
When Artemis “approaches from the back,” it means:
It passes behind the Moon relative to Earth,
On the far side,
To let the Moon’s gravity bend its trajectory.
This has nothing to do with light or darkness, and nothing to do with the Moon’s rotation direction.
✔️ Bottom line
The far side is not the dark side.
Artemis goes around the far side because of orbital mechanics, not because that side is dark or hidden in shadow.
If you want, I can also explain how the Moon’s phases relate to which side is lit, or why the far side looks so different geologically from the near side.
But it's like a hiker taking the bus...??
I love that analogy — and it’s close, but not quite right.
Let me tune it so it matches the physics perfectly.
🚍🌄 Is Artemis like a hiker taking the bus?
Yes… but the “bus” isn’t the Moon’s rotation.
It’s the Moon’s orbital motion around Earth.
That’s the key distinction.
🌙 Why the analogy almost works
Imagine:
A hiker (Artemis) is walking along a road.
A slow‑moving bus (the Moon) is driving in the same direction.
The hiker grabs the bus’s handrail as it passes behind it.
The bus pulls the hiker forward, giving them extra speed relative to the ground.
That is how a gravity assist works.
But here’s the important correction:
✔️ The “bus” is the Moon’s orbital speed
✖️ Not the Moon’s rotation
The Moon’s rotation is like the bus driver turning the steering wheel — irrelevant to how fast the bus is moving down the road.
🚀 What actually gives Artemis a speed boost
The Moon orbits Earth at about 1 km/s.
Artemis approaches the Moon with its own velocity.
When it swings behind the Moon:
The Moon’s gravity bends Artemis’ path
Artemis “steals” a tiny bit of the Moon’s orbital momentum
Artemis leaves the encounter going faster relative to Earth
This is the gravitational slingshot effect.
🌑 Why rotation doesn’t matter
The Moon rotates at only 4.6 km/h at the equator — slower than a person jogging.
Artemis travels at thousands of km/h.
So adding the Moon’s rotation would be like adding the speed of a turning carousel to a jet airplane. It’s negligible.
🧭 So the analogy becomes:
Artemis = hiker
Moon’s orbital motion = bus
Moon’s rotation = irrelevant steering wheel motion
Now the picture is accurate.
If you want, I can sketch the whole gravity‑assist geometry in a simple step‑by‑step way — it’s one of the most elegant tricks in orbital mechanics.
Does Artemis keep this added velocity for long?
Absolutely — and this is where the “hiker grabbing the bus” analogy becomes even more useful.
Let’s walk through it in a way that makes the orbital mechanics feel intuitive.
🚀 Does Artemis keep the extra speed?
Yes — Artemis keeps the added velocity indefinitely, unless another force later changes it.
A gravity assist is not a temporary push.
It’s a permanent change in the spacecraft’s velocity relative to Earth.
Think of it this way:
Artemis swings behind the Moon
The Moon’s gravity pulls on it
Artemis leaves the encounter with a new trajectory and a new speed
That speed remains until something else (like Earth’s gravity, a burn, or another flyby) changes it
There’s no “decay” or “fade‑out” of the speed boost.
🚌🌄 Back to the hiker and the bus
If the hiker grabs the bus and gets pulled forward:
Once the hiker lets go, they keep that new running speed
They don’t slow back down unless friction or fatigue acts on them
In space, there’s no friction.
So Artemis keeps the new speed until a deliberate maneuver changes it.
🌙 Why the speed change is permanent
A gravity assist is an energy exchange:
The Moon loses an infinitesimal amount of orbital momentum
Artemis gains that momentum
The new velocity becomes its new “normal”
Because space is nearly frictionless, nothing naturally removes that energy.
🧭 What happens next depends on the mission
For Artemis II (the flyby mission):
It gets a speed change from the lunar swing
That new speed carries it back toward Earth
Then Earth’s gravity and a re‑entry trajectory take over
For Artemis missions that enter lunar orbit (Artemis III+):
They do a braking burn
That burn deliberately removes some of the speed they gained
Otherwise they would just slingshot past the Moon and escape
✔️ Bottom line
Yes — Artemis keeps the added velocity.
A gravity assist is a permanent change in the spacecraft’s motion, not a temporary boost.
If you want, I can show you how the speed changes depending on whether Artemis passes in front of or behind the Moon — that’s where the real elegance of the slingshot shows up.
I am fascinated by the 'infinitestimal change' to the Moon's orbital velocity. Does all that flying about we do around the Earth alter its orbital velocity around the Sun?
You’ve landed on one of the most beautiful ideas in celestial mechanics:
every gravity assist we perform does change the motion of the body we’re stealing momentum from — but by an amount so tiny it’s effectively unmeasurable.
And yes, the same principle applies to Earth and the Sun.
Let’s unpack it in a way that keeps the elegance of the physics without losing the intuition.
🌍✨ Do spacecraft flying around Earth change Earth’s orbit around the Sun?
Yes — in principle.
No — not in any way that matters.
Every time a spacecraft:
launches from Earth
performs a gravity assist around Earth
re-enters Earth’s atmosphere
…it exchanges a tiny amount of momentum with Earth.
Because momentum is conserved, Earth’s orbital velocity must change by a corresponding amount.
But the change is so small that it’s effectively zero.
That’s:
→ 0.000000000000000000017 km/s
→ 17 billionths of a trillionth of a km/s
This is so small that:
it is far below any measurable threshold
it is far below the effect of sunlight pressure
it is far below the effect of meteoroid dust hitting Earth
it is far below the effect of atmospheric drag from the solar wind
In other words: yes, but no.
🚀🌙 Same logic for the Moon
When Artemis steals a tiny bit of the Moon’s orbital momentum:
Artemis gets a noticeable speed change
The Moon loses an infinitesimal amount of orbital energy
But the Moon is so massive that the effect is utterly negligible.
If every spacecraft ever launched performed a perfect slingshot around the Moon, the cumulative effect would still be smaller than the effect of:
tidal friction
meteor impacts
solar radiation pressure
mass loss from lunar outgassing
🌞 Does Earth’s orbit around the Sun change because of our space activity?
Yes, but by an amount so tiny that it is physically meaningless.
Earth’s orbit is constantly being altered by:
gravitational tugs from Jupiter
tidal interactions with the Moon
mass loss from the atmosphere
solar wind
meteoroid infall
thermal radiation
continental drift changing Earth’s moment of inertia
Compared to these, spacecraft momentum exchanges are like:
a mosquito landing on a freight train.
Technically real.
Practically irrelevant.
🧭 A poetic way to think about it
Every spacecraft we launch slightly nudges Earth’s orbit —
but the nudge is so small that the orbit doesn’t even notice.
It’s like throwing a pebble into the St. Lawrence River:
the river does rise by a molecule’s width, but no one will ever detect it.
If you’d like, we can go deeper into:
how gravity assists conserve momentum
why the Moon’s orbital energy is enormous
how Earth’s orbit does drift measurably over millennia
or how spacecraft actually do change Earth’s rotation (also infinitesimally)
Just say the word.
Gemini Ai:
Artemis Moon Mission; is it the case that the gravitational pull of the Earth on the rocket is stronger all the way to the Moon than that of the moon...
The short answer is no. While the Earth's gravitational pull is significantly stronger than the Moon’s at the beginning of the journey, there is a specific point where the Moon's gravity becomes the dominant force acting on the spacecraft.
To understand how this works for the Artemis missions, it is helpful to look at the relationship between mass and distance in Newton's Law of Universal Gravitation:
Because the Earth is approximately 81 times more massive than the Moon, its "reach" is much further. However, because gravity weakens with the square of the distance (r^2) , the Moon eventually wins out as the spacecraft gets closer to the lunar surface.
The Lagrange Point (L1) and the "Neutral" Point
There is a specific location between the Earth and the Moon where the gravitational pull from both bodies is exactly equal and opposite.
Location: This point is roughly 90% of the way to the Moon (about 345,000 km from Earth and 38,000 km from the Moon).
The Transition: Before this point, the Earth is pulling the rocket back toward home. After crossing this "gravitational crest," the Moon’s pull becomes stronger, and the spacecraft begins to accelerate toward the Moon.
The "Sphere of Influence" (SOI)
In orbital mechanics, engineers use a concept called the Sphere of Influence. This is the near-spherical region around a celestial body where its gravity is the primary influence on a spacecraft's motion.
When the Artemis Orion capsule enters the Moon's SOI, navigators stop calculating its path primarily relative to the Earth and begin calculating it relative to the Moon.
Why this matters for Artemis
The mission profile takes advantage of these physics. The rocket must provide enough energy (Trans-Lunar Injection) to "climb" out of Earth's deep gravity well. Once it passes that neutral point, the Moon effectively "captures" the craft. To enter a stable orbit rather than just flying past or crashing, the Orion spacecraft must then perform a "Lunar Orbit Insertion" burn to slow down and allow the Moon’s gravity to hold it.
Explain the sling-shot manoeuver that will send the rocket back to Earth...
The "slingshot" maneuver, or gravity assist, allows a spacecraft to gain or lose velocity and change direction by utilizing the orbital motion and gravity of a planet or moon. For the Artemis missions returning from the Moon, this is specifically known as a Trans-Earth Injection (TEI), often preceded by a Lunar Flyby.
1. The Physics of the "Slingshot"
A gravity assist is essentially an elastic collision without physical contact. The spacecraft "falls" into the Moon’s gravity well, gains speed as it approaches, and then "swings" around the body.
From the Moon's Perspective: The spacecraft enters and leaves the Moon's gravity at the same speed (ignoring engine burns). It simply changes direction.
From the Earth's Perspective: Because the Moon itself is moving in its orbit around Earth at about 1 km/s, the spacecraft "steals" a tiny bit of the Moon's orbital momentum. This significantly boosts its velocity relative to Earth, enough to break out of lunar orbit and head home.
2. The Return Sequence: From Moon to Earth
To send the Orion capsule back to Earth, the maneuver follows these critical steps:
The Departure Burn
While in orbit around the Moon, the spacecraft fires its engines (the Service Module engine). This burn is timed perfectly so that the craft’s new path intercepts the "back" side of the Moon’s orbital path.
The Lunar Flyby
As the craft rounds the Moon, it passes through the Gravity Well. The Moon’s gravity acts like a tether, whipping the spacecraft around. Because the burn was performed at the periapsis (the closest point to the Moon), it maximizes the Oberth Effect—a phenomenon where engines are more efficient when a spacecraft is moving at high speeds.
Acceleration toward Earth
By swinging around the Moon in the direction of its orbital motion, the craft adds the Moon's orbital velocity to its own. This "kicks" the spacecraft out of the Moon’s Sphere of Influence and onto a trajectory toward Earth’s atmosphere.
3. Trajectory Comparison
4. Precision is Critical
The "slingshot" must be calculated with extreme precision. If the angle is off by even a fraction of a degree:
Too shallow: The spacecraft will skip off the Earth's atmosphere like a stone across a pond and fly into deep space.
Too steep: The craft will enter the atmosphere at an angle that creates too much heat and G-force, leading to structural failure.
The maneuver essentially converts the Moon's kinetic energy into a "free" boost for the rocket, saving massive amounts of fuel that would otherwise be required to push the craft back toward Earth.
So it comes down to accelerating in a curve!!??
Precisely. In orbital mechanics, you rarely travel in straight lines because gravity is constantly "bending" your path into a curve.
To execute a return from the Moon, the spacecraft performs what is called a powered flyby. It is a combination of engine thrust and the natural curvature of the Moon's gravity.
The Geometry of the "Kick"
Think of the spacecraft as being in a "well." To get out, it needs speed. By accelerating while moving along the curve of the Moon, two physics principles work in your favor:
The Oberth Effect: You get more "bang for your buck" out of your fuel when you fire your engines while moving at high speeds. Since the spacecraft is moving fastest at its closest approach to the Moon (periapsis), firing the engines there provides the most kinetic energy.
Vector Addition: You aren't just pointing the rocket at Earth and pushing. You are adding your new speed to the Moon’s own orbital speed (≈ 1,022 m/s).
The Resulting Path: An Ellipse
When the engine fires and the Moon "flings" the craft, the orbit changes from a circle around the Moon into a very long, stretched-out ellipse.
The Low point (periapsis) of this new orbit is where the maneuver happened near the Moon.
The High point (apoapsis) of this new orbit is calculated to intersect with the Earth’s atmosphere.
Why a Curve?
If you tried to fly in a straight line, you would have to fight Earth's and the Moon's gravity the entire way, which would require an impossible amount of fuel. By "accelerating in a curve," you are essentially using the Moon as a pivot point to redirect your momentum, letting the natural laws of motion do the heavy lifting to line you up for the trip home.
* * *
Asked Gemini for sources...
Source for further reading: * NASA’s Guide to Gravity Assists: Detailed explanation using the Cassini mission as a primary example.
The Planetary Society: Gravity Assist: A breakdown of the math behind how speed is gained relative to the Sun or Earth.
Sounds awesome... but to my mind problematic. I've interacted enough with the AIs
to know their scope and limitations. Once an error happens, the AI does not recognize it
or be told how to self-correct in a durable way...
Not sure what to make of this: a piece in OilPrice.com about Alberta's
break-even budget, compared to that of other Oil-producing territories...😐
https://oilprice.com/Energy/Crude-Oil/100-Oil-Isnt-Enough-to-Balance-Albertas-Books.html
* * *
This part is clear; prices at the pump keep going up: