Just reposting.

A spaceship is on a straight-line path between the Earth and the Moon. At what distance from Earth is the net gravitational pull on the probe from the Earth and the moon zero? Mass of Earth = 6×10^24 kg. Mass of Moon = 7×10^22 kg. The distance from the sun to the moon is 150×10^6 km.

I need to confirm if my answer of 4678km is right. I used the centre of mass equations.... M1S1+M2S2/M1+M2.

To determine at what distance from Earth the net gravitational pull on the spaceship from Earth and the Moon is zero, you can use the concept of the center of mass.

The formula you used, M1S1 + M2S2 / (M1 + M2), is indeed the correct formula for finding the center of mass between two objects with masses M1 and M2 and respective distances from the center of mass S1 and S2.

Let's calculate the center of mass distance using the masses and distances given in the problem:

Mass of Earth (M1) = 6 x 10^24 kg
Mass of Moon (M2) = 7 x 10^22 kg
Distance from the Sun to the Moon (S2) = 150 x 10^6 km

Assuming the distance from Earth to the spaceship is S1, we can set up the equation:

M1S1 + M2S2 = 0

(6 x 10^24 kg)S1 + (7 x 10^22 kg)(150 x 10^6 km) = 0

It's important to convert the distance from kilometers to meters (1 km = 1000 m):

(6 x 10^24 kg)S1 + (7 x 10^22 kg)(150 x 10^6 km)(1000 m/km) = 0

Simplifying the equation:

(6 x 10^24 kg)S1 + (7 x 10^22 kg)(1.5 x 10^8 m) = 0

(6 x 10^24 kg)S1 = -(7 x 10^22 kg)(1.5 x 10^8 m)

Dividing both sides by (6 x 10^24 kg):

S1 = -[(7 x 10^22 kg)(1.5 x 10^8 m)] / (6 x 10^24 kg)

Calculating this expression:

S1 ≈ -17.5 x 10^6 m

As you can see, the distance (S1) is negative, indicating that it lies in the opposite direction from the Moon. However, the magnitude of the distance is about 17.5 x 10^6 meters, which is approximately 17,500 km.

Therefore, the correct answer is approximately 17,500 km (or -17.5 x 10^6 m) from Earth, not 4,678 km.

To find the distance from Earth where the net gravitational pull on the spaceship is zero, you can use the concept of the center of mass. The formula you mentioned, M1S1+M2S2/M1+M2, is correct.

Let's break down the problem step by step:

1. Determine the total mass of the system:
The total mass of the system is the sum of the mass of the Earth and the mass of the Moon.
Total mass (M) = Mass of Earth (M1) + Mass of Moon (M2)
M = 6×10^24 kg + 7×10^22 kg.

2. Calculate the distance of the center of mass from Earth (S1):
The center of mass of a two-body system lies along the line connecting the two bodies. We know that the distance from the Earth to the Moon is 150×10^6 km, which we can convert into meters.
Distance of the center of mass from Earth (S1) = (M2 × Distance from the Sun to the Moon) / Total mass
S1 = (7×10^22 kg × 150×10^6 km) / M.

3. Calculate the distance of the center of mass from the Moon (S2):
Since the spaceship is on a straight-line path between the Earth and the Moon, the distance of the spaceship from the Moon is the distance from the Sun to the Moon minus the distance from the Earth to the center of mass.
Distance of the center of mass from the Moon (S2) = Distance from the Sun to the Moon - S1.

4. Find the distance from Earth where the net gravitational pull on the spaceship is zero:
At this point, the net gravitational pull is zero when the spaceship is at equal distance from both the Earth and the Moon. In other words, S1 + Distance from the Earth to the spaceship = S2.
Distance from the Earth to the spaceship = S2 - S1.

Now you can substitute the values into the equation and calculate the distance from Earth where the net gravitational pull is zero.