1
00:00:00,510 --> 00:00:08,160
So we have varied the starting velocity, and we have seen what can happen if the starting velocity

2
00:00:08,160 --> 00:00:12,810
is just slightly increased from the circular trajectory, we get such an orbital trajectory.

3
00:00:13,380 --> 00:00:22,770
If we increase it by another factor of one point twenty five, approximately then the velocity is so

4
00:00:22,770 --> 00:00:26,700
large that we can even leave the gravitational field of the Earth.

5
00:00:26,790 --> 00:00:31,530
Roughly speaking, of course, it's always in the gravitational field, but then the force or the influence

6
00:00:31,530 --> 00:00:33,960
by the Sun is larger than the influence by the Earth.

7
00:00:35,490 --> 00:00:40,600
So what happens if we set an intermediate velocity where it is oval?

8
00:00:40,600 --> 00:00:47,550
This elliptical trajectory trajectory hits or intersects the trajectory of the Moon.

9
00:00:48,480 --> 00:00:57,690
So then we may get a so-called moon encounter where the object is so close to the moon that the motion

10
00:00:57,690 --> 00:01:02,060
is mostly affected by the Moon, even though the Moon is much lighter than the Earth.

11
00:01:02,070 --> 00:01:09,350
But due to the small distance, it's then strongly affected and there really funky stuff can happen

12
00:01:10,260 --> 00:01:10,860
so.

13
00:01:12,030 --> 00:01:15,600
I have just copied here a few lines of code from our previous examples.

14
00:01:15,960 --> 00:01:19,590
And now I can just change it once again, so I will change here.

15
00:01:19,890 --> 00:01:24,420
The starting velocity and though I will, we have one point twenty five.

16
00:01:24,840 --> 00:01:29,250
We had one point five zero and now I take one point three four.

17
00:01:29,670 --> 00:01:34,860
So here, of course, since this is a very sensitive maneuver, when we want to hit the Moon, it's

18
00:01:34,860 --> 00:01:36,690
very sensitive to this velocity.

19
00:01:36,720 --> 00:01:40,470
So if you changed as a tiny bit, it can give different results, of course.

20
00:01:41,460 --> 00:01:46,560
And I think the time period we can check if this is OK.

21
00:01:46,890 --> 00:01:50,610
And then I also fixed here the X limit and the Y limit as we had before.

22
00:01:51,360 --> 00:01:56,280
So instead of speaking, I just press shift enter and here we see our results.

23
00:01:57,080 --> 00:02:03,810
So we see here the trajectory of the Earth around sorry, the moon around the Earth and the spaceship

24
00:02:03,810 --> 00:02:06,030
around the Earth.

25
00:02:07,080 --> 00:02:11,900
And one thing that we can notice if we zoom in a bit more, if we could, for example, use here year

26
00:02:11,940 --> 00:02:13,770
two to zoom in a bit.

27
00:02:17,080 --> 00:02:22,810
What we can see, then, is that the trajectory is not always on the same oval.

28
00:02:22,900 --> 00:02:27,760
It is a bit shifted, so we see that there was some influence of the Moon already.

29
00:02:28,210 --> 00:02:33,940
So since our spaceship is in the vicinity of the Moon, the trajectory has been shifted a bit.

30
00:02:34,210 --> 00:02:36,190
But this effect is really not so large.

31
00:02:37,150 --> 00:02:41,650
So then let me increase this to a few months.

32
00:02:42,070 --> 00:02:45,790
So I will simulate here to zero point three years.

33
00:02:47,680 --> 00:02:56,020
And you see at the point where we almost hit the moon here, we will have an earth escape, where the

34
00:02:56,020 --> 00:03:01,540
spaceship will leave the Earth and we'll go on a trajectory around the sun.

35
00:03:02,440 --> 00:03:08,860
And the cool thing about this is that we achieved this with a lower velocity compared to the 1.5 that

36
00:03:08,860 --> 00:03:14,020
we had before for the Direct Earth Escape.

37
00:03:14,470 --> 00:03:21,790
So this was here 1.5 B orbits, and now we can get qualitatively the same result.

38
00:03:21,800 --> 00:03:27,310
We leave the sphere of influence by just using a lower starting velocity.

39
00:03:27,820 --> 00:03:32,530
So this is really useful for some maneuvers because you can save a lot of fuel.

40
00:03:32,530 --> 00:03:35,170
You don't have to accelerate to such a high velocity.

41
00:03:35,500 --> 00:03:40,600
You basically get something like a slingshot where you approach the moon.

42
00:03:40,600 --> 00:03:49,180
And since you are so close to this object, you get an additional acceleration and then you get thrown

43
00:03:49,180 --> 00:03:52,030
out of the rotation around the Earth.

44
00:03:53,170 --> 00:04:00,640
So that's a cool trick, and we can use this for leaving, leaving Earth and maybe traveling to Mars

45
00:04:00,640 --> 00:04:01,180
one day.

46
00:04:02,450 --> 00:04:08,540
But what's also really nice is that we are here pretty close to the Moon, we can actually check the

47
00:04:08,540 --> 00:04:09,290
distance here.

48
00:04:09,860 --> 00:04:13,820
This will be the distance spaceship to the Moon.

49
00:04:16,399 --> 00:04:20,810
And so we have to use here nine, 12 and six and nine.

50
00:04:23,100 --> 00:04:29,670
And you see, in the beginning, we are not so far, we always roughly oscillate here, but you see

51
00:04:29,670 --> 00:04:35,820
it's not really a nice oscillation, which means there is also stuff going on in the beginning and we

52
00:04:36,540 --> 00:04:41,730
oscillate approximately twice and then we are here very, very close to zero.

53
00:04:41,730 --> 00:04:45,000
So you see, this is really such a kink where we almost hit the moon.

54
00:04:45,000 --> 00:04:50,970
And since we are so close, we get thrown out of the trajectory and then we leave the moon and we also

55
00:04:50,970 --> 00:04:51,630
leave the Earth.

56
00:04:52,710 --> 00:04:57,960
And now the idea is we approached Moon here pretty closely.

57
00:04:58,590 --> 00:05:01,700
What happens if we break at this point of time?

58
00:05:02,100 --> 00:05:04,080
Can we achieve a moon orbit?

59
00:05:04,890 --> 00:05:06,240
And of course we can.

60
00:05:06,450 --> 00:05:12,570
And of course, this is also how it's done in reality, how you get to the moon orbit and from there,

61
00:05:12,960 --> 00:05:17,130
how you land on the moon by just breaking even more.

