Solve Max Velocity Increase of 100kg Probe in Gravity Assist from Mars

  • Thread starter zebra1707
  • Start date
In summary, the maximum increase in velocity that can be achieved by a 100 kg space probe traveling at 12,000 ms^-1, in a gravity assist manoeuvre around the planet Mars with an orbital velocity of 24,200 ms^-1 is 60,400 ms^-1. If the probe only completed a 120 degree arc in its flyby, the maximum increase in velocity would be slightly more than 60,400 ms^-1. To calculate this, the conservation of momentum and kinetic energy equations can be used, along with the equation vf = vi + 2Vi. Additionally, for a real gravitational sling-shot maneuver, the maximum change in speed can be calculated using the equation \Delta v = 2 v
  • #1
zebra1707
107
0

Homework Statement



I have a question which asks for the maximum increase in velocity that can be achieved by a 100 kg space probe traveling at 12 000 ms -1, in a gravity assist manoeuvre around the planet Mars, which has an orbital velocity of 24200 ms -1.

Homework Equations



vf = vi + 2vi
= 12000 + 2(24200)
= 60400, therefore max increase in velocity is 60400 ms -1

The Attempt at a Solution



See above. The next part asks how would your answer be if the probe only completed 120 degree arc in its flyby? Support with vector diagram.

You are not told what the original arc is, so I assume it is greater than 120 degrees. However, that does not assist with the answer to this problem?

If I draw the Before and After vectors diagrams and resultant incoming and outgoing velocities relative to the planet by using pythag - but I am still no closer to a solution.
 
Last edited:
Physics news on Phys.org
  • #2
You have gotten the speeds mixed up. First note, that the speeds are (I assume) given relative to the sun and that the speeds in the first equation should be relative to the planet (mars), so you should transform the speed for the probe to be relative to the planet (by coincidence this also gives 12 km/s). Second, the initial and final speed in the equation refer to that of the probe, not the planet. Third, the text ask for the change in speed (vf minus vi).

If you are given an arc (angle between initial and final velocity vector) you also need another formula that contains this angle (or you need to derive it from geometry), but its difficult to provide help without knowing a bit more about what you have been given.
 
  • #3
The question is as stated no additional information.

Formula comes from
1. Applying the conservation of momentum to this collision KVi - vi = KVf + vf
2. Applying the conservation of kinetic energy KVi^2 + vi^2 = KVf^2 + vf^2

Solving equations simultaneously for vf leads to the following equation:

vf = vi + 2Vi

where: vf = maximum exit velocity of spacecraft ms -1
vi = entry velocity of spacecraft - relative to the sun (12000 ms -1)
Vi = velocity of the planet (in this case Mars - 24 200 ms -1)

Therefore vf = 12,000 + 2(24 200)
= 60 400 ms -1

Therefore this is the max increase in velocity is 60 400 ms -1. The question then asks what would the answer be if the probe only completed 120 degree of arc in this fly by (support with vector diagram).
 
Last edited:
  • #4
OK, ignoring for a minute how mind-numbing unrealistic this "collision" is, the change in speed in first case must be vf-(-vi), that is, a tad more than vf.

To calculate how much speed changes if the initial velocity is only turned 60 degrees (instead of 180), you could reformulate the momentum equation by looking only at the momentum projected onto one particular direction and then solve this equation together with the kinetic energy equation as before. For instance, if you draw the velocities before and after in a diagram with the planet velocities parallel to the x-axis, you could write an equation for conservation of momentum onto the x-axis. You can probably apply some assumptions along the way to simplify the calculations. Alternatively, you could look up how to calculate the final speeds in a two-dimensional elastic collision and apply this to your problem.

I must admit that I originally thought the problem text were concerned with real gravitational sling-shot maneuvers. If it were, it would be instructive to know that the maximum change in speed for a passive Mars gravity assist is around 3.5 km/s, and can be calculated as

[tex]\Delta v = 2 v_\infty \sin(\varphi / 2)[/tex]

where [itex]v_\infty[/itex] is the hyperbolic excess speed and [itex]\varphi[/itex] is the rotation of the velocity vector which depends on the minimum distance the probe passes by the planet center (this is the equation I thought you referred to originally, just with the rotation angle set to 180 deg). Setting the minimum distance to the planet radius for Mars and finding the hyperbolic excess speed which maximizes change of speed gives the mentioned value of 3.5 km/s for mars.
 
  • #5
Thank you Filip for your assistance. Now this makes sense.

CHeers P
 

1. What is "Max Velocity Increase" in the context of a gravity assist maneuver?

"Max Velocity Increase" refers to the maximum amount of speed that can be gained by a spacecraft during a gravity assist maneuver. In this case, it refers to the maximum increase in velocity that a 100kg probe can achieve while using Mars' gravity to slingshot towards its destination.

2. How does a gravity assist maneuver work?

A gravity assist maneuver, also known as a slingshot maneuver, involves using the gravitational pull of a planet or other massive object to accelerate a spacecraft. The spacecraft approaches the planet in a specific trajectory, taking advantage of the planet's gravitational pull to increase its speed. As the spacecraft passes the planet, its trajectory is altered, allowing it to continue on towards its destination with a higher velocity.

3. Why is Mars often used for gravity assist maneuvers?

Mars is often used for gravity assist maneuvers because of its relatively large size and close proximity to Earth. Its gravitational pull is strong enough to provide a significant boost in velocity, but not so strong as to cause damage to the spacecraft. Additionally, Mars' orbit is similar to Earth's, making it easier to plan and execute a gravity assist maneuver.

4. What factors affect the amount of velocity gained during a gravity assist maneuver?

The amount of velocity gained during a gravity assist maneuver depends on several factors, including the mass of the spacecraft, the mass of the planet, and the distance and angle at which the spacecraft approaches the planet. The timing of the maneuver also plays a crucial role, as the spacecraft must be in the correct position to take advantage of the planet's gravitational pull.

5. How do scientists calculate the max velocity increase of a spacecraft during a gravity assist maneuver?

Scientists use mathematical equations and computer simulations to calculate the potential velocity increase of a spacecraft during a gravity assist maneuver. They take into account the various factors mentioned above, as well as the specific trajectory and speed of the spacecraft before and after the maneuver. These calculations help determine the optimal approach and timing for a successful gravity assist maneuver.

Similar threads

  • Introductory Physics Homework Help
Replies
6
Views
3K
  • Introductory Physics Homework Help
Replies
3
Views
2K
  • Computing and Technology
Replies
2
Views
2K
Back
Top