Voyager 1 this close to leaving solar system
theatlantic.com
theatlantic.com
"For example the Voyager missions which started in the late 1970s were made possible by the "Grand Tour" alignment of Jupiter, Saturn, Uranus and Neptune. A similar alignment will not occur again until the middle of the 22nd century."
source: http://en.wikipedia.org/wiki/Gravitational_slingshot#Limits_...
I'd also want to use some of that power to make the probe 'bright'. It could transit telemetry back to us with more power so we could keep contact with it longer, and it could also broadcast its presence in every other direction too. That way if there is anyone out there, they'll have a chance to find the probe. With the Voyager probes, even if the galaxy is teeming with intelligent space-traveling life it's unlikely that anyone will every find the tiny little things.
In other words, even the best rockets we have now are not as good as that rare lineup of all four gas giants in this system.
Also, we don't have a better energy source. Voyager used RTGs, and that's still what we have. In any case, power isn't the limiting factor, it's exhaust velocity and amount of fuel.
http://en.wikipedia.org/wiki/File:Voyager_2_velocity_vs_dist...
Looks like Uranus gave a tiny boost and Neptune a negative boost -- not through any intrinsic property of the planet, mind you, just the constraints applied when you want to tour the whole solar system without burning any fuel.
It shows that my earlier reading was incorrect. It looks like the delta-V from Jupiter is 11km/s, Saturn is 8km/s, Uranus is 1km/s and Neptune, as you point out, is a negative delta V w.r.t distance from the Sun. Note that the comment says it's because Voyager 2 deflected out of the plane of the ecliptic as a consequence of doing a flyby of Triton, and not because of fuel constraints.
In any case, I had forgotten that Voyager I did not do the grand tour of the giants. I haven't been able to find a similar velocity profile for Voyager I.
From what I can find, the best ion craft we have now (Dawn) is about 1/2 as effective as a Jupiter flyby, and 1/6 as effective as the series of flybys that Voyager did.
If we wanted to send a probe to the middle of nowhere right now and had a billion or two to do it we'd strap our best ion drive to our best RTGs and then send it via a Jupiter slingshot. No idea how fast we could get it. Of course it would continue to accelerate until the power or the propellant ran out.
How do RTGs help?
Let's say they somehow do (perhaps I have the numbers wrong). How much more delta V would you get using an RTG? Twice the delta V as solar panels? Note: momentum transfer goes as the square root of the energy, so you would need 4x as much power as Dawn uses. On the other hand, you wouldn't be carrying heavy panels.)
If so, 20km/s is about what a Jupiter or Saturn flyby gives. So RTG+ion thruster+Jupiter is about equivalent to the Jupiter+Saturn part of Voyager. Except Voyager also used the outer gas giants.
My point is that to get the same speed you'll need at least both of Jupiter and Saturn lined up right, and preferably at least one of Uranus or Neptune. Your proposal isn't enough.
This doesn't mean that RTGs don't have value. They are continuous and keep things warm, which may be very important depending on your mission.
Unfortunately, a probe to Uranus is still a fairly low priority for NASA. I think the worry is that we'd be spending a billion dollars on funding obvious toilet humor.
In this article I see some very slight hinting towards that possibility. Does anyone know what I'm referring to? Anyone have any more input on that?
But there are significant problems picking up 'intelligent' signals like the ones being transmitted by Voyager because of the 'free space attenuation' of the radio signal caused by the spreading of the radio signal: http://en.wikipedia.org/wiki/Free-space_path_loss
The attenuation of radio signals in this way is one of the reasons why it will be difficult for any other civilisations to pick up our radio signals. There were some calculations done by the SETI folks on how far out our common Earth radio signals would be detectable (such as FM radio or broadcast TV) using a very large radio telescope and the answer was that they wouldn't make it our of the solar system.
Unless you mean to imply the heliosphere might be blocking low powered radio signals from other spacecraft?
It's not a far stretch of the imagination to say radio waves can suffer from interference and even reflection off magnetic fields. It happens here on Earth; bouncing shortwave off the ionosphere is a very common way to communicate long distances.
The microwave was a separate but related example of electromagnetic interference on radio transmissions. Both combined paint a picture showing it's possible we might not hear from Voyager again and might not get a good picture of intelligent transmissions outside the heliosphere.
It just that we can't seem to find any intelligent message buried in heaps of information that's falling on Earth.
http://www.reddit.com/r/junk001/comments/v122m/test1/?alread...
http://www.dailydot.com/news/reddit-ban-the-atlantic-phsyorg...
(oh and Solar System != Universe :-) )
At what point would equipment failure be considered, especially given the notable lack of experience in this scenario? Seems that corroborating evidence would be highly desirable before publicizing this. (Or perhaps I am underestimating the data already gathered on this topic...)
The repressed space geek within me is jumping to all kinds of conclusions as to what will happen when it leaves the solar system, what it will find and what it may accidentally discover.
http://physics.stackexchange.com/questions/26712/what-is-the...
http://wiki.answers.com/Q/What_is_the_average_distance_betwe...
The asteroid belt is so unbelievably sparse, you would never even know you are flying through it. Absolutely no concern was given to the prospect of a collision.
To give you some perspective, as a test they flew one of the pioneer spacecraft through the rings of saturn, even the rings of saturn are so sparse that the spacecraft flew through completely untouched.
Absolutely no concern was given to the prospect of a collision.
Doesn't NASA have to constantly deal with and prepare for one-in-a-million chance scenarios? It seems reasonable to have a collision detector and "auto-route-arounder" that help here (among many other scenarios).http://physics.uoregon.edu/~jimbrau/BrauImNew/Chap06/7th/AT_...
Dr. Marc D. Rayman on the Dawn Project: Dawn will travel 7.7 astronomical units (AU), or nearly 1.2 billion kilometers (almost 720 million miles), to its July 2011 rendezvous with Vesta. Yet in all that time, and across all that distance, the closest the probe will come to a catalogued asteroid is 1.0 million kilometers (greater than 600 thousand miles), or more than 2.5 times the distance between Earth and the moon.
Reference to Star Trek: The Motion Picture, for anyone who may not immediately get the reference. The plot of the story revolves a giant space cloud containing a vessel that's ultimately returning Voyager to Earth.
It was a very appropriately timed movie and really explores the idea of Man's impact even beyond our solar system with the devices we shoot off into the stars.
There's still a fair few people working on Voyager, and they don't have much to do now except stare at slightly different types of vacuum, so they feel the need to issue a press release every couple of years.
http://www.sciencedaily.com/releases/2000/12/001219073936.ht...
The Voyager 1 spacecraft, the farthest human-made object from Earth, may reach the beginning of his boundary region between early next year and the end of 2003
Now, that was the termination shock, this is the heliopause. Next comes the bow shock.
Also, there's a more ambitious project that keeps getting delayed: http://en.wikipedia.org/wiki/KEO