The maths that made Voyager possible
bbc.co.uk
bbc.co.uk
This is misleading. The three-body problem is known to be insoluble in closed form, but anyone cam model it numerically. The person being describes was one of the first to do this, but the comparison with Newton is misleading.
Many kinds of problems are soluble through numerical modeling that aren't remotely soluble in closed form, and it is important to distinguish between the two kinds of solution.
On reading the article, it occurs to me that the author simply doesn't understand the math well enough to grasp the difference between an analytical and a numerical solution.
Similarly, I am not ringing up the Clay Institute to claim my $1M prize for 'solving' Navier-Stokes because I've just run a toy computational-fluid-dynamics problem in OpenFoam.
There is nothing good to be gained from obfuscation and sensationalisation in the public understanding of science.
Your point of argument is a metaphor which a non technical author would have used or even used in exaggeration by mistake.
Sorry but pedantic arguments make a persons case look bad. Its like complaining about Khan academy's Python course. Smart intelligent people feel guilty when solving a problem well within their reach, was taken by somebody else and solved by them. It makes them feel more bad, when the solution becomes famous and brings a lot of fame to the inventor. It seems that is what you are going through here.
> I don't know what you are complaining about.
Indeed, and the rest of your reply goes on to confirm this, with the additional quite needless, but amusing, psychological analysis. I'm sorry if I worded it poorly in my first reply, although I can't see that it's particularly ambiguous.The issue is quite orthogonal to him personally and his achievements, for which I have the utmost respect. I am fascinated by the early days of space exploration and am as impressed by this work as I was when I first read about it a few years ago.
The issue is with the journalism, written by the journalists, which attempts to sensationalise the achievements (which can stand on their own two feet without it) by making comparisons with famous mathematicians that are not valid comparisons, as Paul Lutus explains in his first post. It's just apples and oranges, and will at best be lost on the lay reader and at worst confuse the lay reader who looks into the three body problem further. Hence my point that it is unhelpful to the public understanding of science.
"At the time, Nasa couldn't guarantee a spacecraft for more than a few months of operational life, and so the outer planets were considered out of reach.
"That was until a 25-year-old mathematics graduate called Michael Minovitch came along in 1961."
Which is followed by,
"To reach Neptune [Voyager 1 and 2] would have to last for over a decade in space, operating in the darkest reaches of the Solar System billions of km from the Sun."
Solving a limited three-body problem and inventing the gravitational slingshot is way cool. Throwing in a mess of red herrings and yellow journalism detracts from the point of the article.
Oh, and anyone know why the Bbc doesn't want to capitalize 'NASA'?
Nonetheless, kudos to the guy to understand that a gravitational slingshot is possible, and proving it.
There's also a bit of a multiple endpoints situation in singling out the 4-out-of-4 giant planets scenario. That is indeed infrequent, but say a 3-out-of-4 lineup with either Uranus or Neptune, or 4-out-of-5 with Uranus and Pluto as the final two [dwarf] planets, also would have made for a fine and successful mission.
OTOH, we could even argue that we were unlucky that the giant planet alignment occured for that 1977 launch window. If it occurred this decade instead, we could send a much better spacecraft with the capabilities of Cassini or Messenger or New Horizons.
He sounds rather bitter that his story has not made him more famous, and comes off as something of a crank at that ("How Did Minovitch Discover (Create) His New Theory Of Space Travel?"). I think Minovitch is basically an engineer at heart, and is resentful that all of the attention seems to go to the scientists, i.e. people who come up with the actual physical theories about mass and energy and so forth.
Our culture does value scientists more than engineers. You could argue that this is good because theories are universally applicable and represent fundamental understanding, or that this is bad because many theories have absolutely no applications and that it's the engineers who deliver value to society. You could also argue that the amount of prestige that we heap on scientists tends to go to their heads and they stop doing good work. But whatever. Stay sharp, do what you're best at, and don't pay attention to other people's benefits packages.
He also mentions his solution as addressing the three-body problem, so maybe that's where the writer of the linked article got misled on that point. Too bad the writer of TFA didn't check this out with an independent expert.
The group at JPL that Minovitch mentions is still intact (http://ssd.jpl.nasa.gov/). They provide the highest-quality ephemeris available anywhere (AFAIK) to all NASA missions.
Does somebody here who's knowledgeable on the subject have some reference?
Even Stereo, a two-satellite pair in earth-trailing and earth-following orbits looking at the Sun, used gravity assist (with the Moon).
Gravity assist is one way to provide "delta-v" (velocity change, the coin of the realm in propulsion). You can provide negative delta-v using aerobraking -- orbiting your destination, Mars say, and slowing down using atmospheric friction. This is used on the Mars orbiters.
As usual, see: http://en.wikipedia.org/wiki/Delta-v_budget
My understanding is that if they left the ion drive on long enough, the craft would continue to accelerate.
[1]http://en.wikipedia.org/wiki/Dawn_%28spacecraft%29#Propulsio...
https://en.wikipedia.org/wiki/High_Power_Electric_Propulsion
https://www.lpi.usra.edu/meetings/jimo2003/hartman.pdf
delta-v is proportional to the specific impulse (or exhaust velocity), and logarithmic in the propellant ratio. For instance, with a propellant ratio of e = 2.7, you can get a delta-v equal to the exhaust velocity. For a delta-v twice that, you need a propellant ratio of e^2 = 7.4. Obviously it's not practical to go much faster the exhaust velocity; the propellant demand grows exponentially.
Their model is definitely simplified (no lagrange points, for example), but the major aspects are modeled well enough to give you an idea of how interplanetary space travel works.
http://www.lpi.usra.edu/meetings/jimo2003/hartman.pdf
It's a completely doable project sidelined by budget priorities (NASA thinking space tourism more important than science).
There are other fun things that we can do with gravity assists as well:
A rocket burn is significantly more effective when close to a large gravitational source.
http://en.wikipedia.org/wiki/Oberth_effect
If you are willing to wait long enough there is a way to get almost anywhere in the solar system for very little fuel.
http://en.wikipedia.org/wiki/Interplanetary_Transport_Networ...
What do they have to gain from it?