Smallest perpendicular velocity to orbit

In summary: Yes, you're right about the perpendicular direction. It should be half the angular diameter in the perpendicular direction as well. Sorry about the confusion. In summary, the distance from Earth to the sun is 1.50 * 1011m and Earth's orbital period is 3.16 * 107 s. The distance from Venus to the sun is 1.08 * 1011m and Venus's orbital period is 1.94 * 107 s. Both orbits are coplanar and the transit of Venus about the sun is observed by a telescope on Earth. To calculate the smallest perpendicular velocity to its orbit, required by Venus so that the next expected transit does not occur, the relative period between Earth and Venus is
  • #1
unscientific
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Homework Statement


Distance from Earth to sun = 1.50 * 1011m
Earth's orbital period = 3.16 * 107 s

Distance from venus to sun = 1.08 * 1011m
Venus's orbital period = 1.94 * 107 s

Both orbits around the sun are coplanar, and the transit of venus about the sun is observed by a telescope on earth.QN: To calculate the smallest perpendicular velocity to its orbit, required by venus so that the next expected transit does not occur.

Homework Equations


Since venus and Earth are orbiting at different angular velocities, (with venus moving faster)
Relative period = 5.02 * 107 s

Therefore, time interval between successful transists = 5.02 * 107 s

The Attempt at a Solution



http://img200.imageshack.us/img200/2987/earthvenus.jpg"

The angle theta was found to be 0.00928 rad.

In order for the next transit not to occur (say originally both Earth venus are along the left line that connects to left extreme end of sun), in the 5.02 * 107 s that venus spends traveling relative to earth, it must be displaced by an angle of 0.00928 rad for venus to 'escape' being caught in the camera's frame that is pointing to the sun.But the answer says that " If during the interval between transits venus has a velocity vs perpendicular to its orbit and as a result, is displaced by (1/2)(0.00928) rad as observed from Earth (half aug. diameter of of sun at earth) , venus will not pass in front of the sun"

My question is - why only half the angle?!

The original question can be found here at Qn 8:
Qn paper: http://www.physics.ox.ac.uk/olympiad/Downloads/PastPapers/BPhO_Paper2_2005_QP.pdf

Answers:
http://www.physics.ox.ac.uk/olympiad/Downloads/PastPapers/BPhO_Paper2_2005_MS.pdf

Really appreciate any help offered!
 

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  • #2
If the orbits of Venus and Earth are coplanar when the first transit happens, Venus will pass through the exact centre of the image of the Sun. It only need to be displaced by half the angular diameter of the sun as seen from the Earth to not be Silhouetted by the Sun at the next expected transit. That's (1/2)(0.00928) rad.
 
  • #3
omoplata said:
If the orbits of Venus and Earth are coplanar when the first transit happens, Venus will pass through the exact centre of the image of the Sun. It only need to be displaced by half the angular diameter of the sun as seen from the Earth to not be Silhouetted by the Sun at the next expected transit. That's (1/2)(0.00928) rad.

If venus and Earth are aligned, through the Earth's lenses won't venus appear to be at the leftmost edge of the sun's diameter and not the centre?

the left picture shows the 3 planets, while the right picture shows what it looks like when viewed from earth.
 

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  • #4
It'll still pass through the centre of the sun as seen from Earth (pass from left to right through the centre of the sun).

Velocity component perpendicular to the plane of orbit means that velocity component is directed either up or down as seen from the earth.
 
  • #5
omoplata said:
It'll still pass through the centre of the sun as seen from Earth (pass from left to right through the centre of the sun).

Velocity component perpendicular to the plane of orbit means that velocity component is directed either up or down as seen from the earth.

oh i get it now! All venus needs to do is to move upwards/downwards by half of sun's diameter so it would be hidden behind! (Since originally Earth and venus are always on the same plane that passes through the centre of the sun) Without the vertical velocity, venus will always pass through from left to right of the sun's centre plane. Thank you!
 
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  • #6
unscientific said:
hmmm i thought that the transit starts when venus appears at the leftmost diameter of the sun (at the edge) and not when it is at the centre of the sun?
Yes, the transit starts at the leftmost diameter of the sun. But if Earth, Sun and Venus are coplanar (in the same plane), will Venus pass through the exact center of the Sun as seen from Earth or not? What do you think?

unscientific said:
I even if it moves up or down, why must it be half a diameter in the vertical direction? It would make more sense if it was displaced rightwards by half a diameter? that's one part i didnt get about the perpendicular velocity!
The question says velocity component perpendicular to its orbit. If Venus passes from left to right in front of the Sun as seen from the Earth, that means the plane is horizontal. So a direction perpendicular to that plane would be vertical as seen from the Earth.
 
  • #7
Oh, it seems I took too long to post.

You're welcome.
 

What is the smallest perpendicular velocity to orbit?

The smallest perpendicular velocity to orbit, also known as the orbital velocity, is the minimum speed required for an object to maintain a circular orbit around a larger body, such as a planet or a star. It is influenced by the mass and distance of the larger body.

How is the smallest perpendicular velocity to orbit calculated?

The smallest perpendicular velocity to orbit can be calculated using the formula: v = √(GM/r), where v is the orbital velocity, G is the gravitational constant, M is the mass of the larger body, and r is the distance between the two objects.

What factors influence the smallest perpendicular velocity to orbit?

The smallest perpendicular velocity to orbit is influenced by several factors, including the mass and size of the larger body, the distance between the two objects, and the gravitational constant. Other factors such as atmospheric drag and the shape of the orbit can also affect the orbital velocity.

Can the smallest perpendicular velocity to orbit be changed?

Yes, the smallest perpendicular velocity to orbit can be changed by altering the factors that influence it. For example, changing the mass or distance of the larger body, or using propulsion systems to increase or decrease the velocity of the orbiting object, can alter the orbital velocity.

Why is the smallest perpendicular velocity to orbit important?

The smallest perpendicular velocity to orbit is important because it determines the stability and trajectory of an object in orbit around a larger body. It is also essential for spacecraft and satellites to achieve and maintain their desired orbits around planets and stars.

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