On Wednesday, February 20, 2013 12:50:44 PM UTC-6, pnyikos wrote:
> Thanks for posting on this theme, John. It's good to have a
> participant who has discussed Project Orion at length.
>
[snip]
>
> > It is a lot of moving parts, and they'd be moving over a long
> > period of time in a thermally hostile environment.
>
> Why thermally hostile? The bombs would not have to be positioned in
> rapid fire, like the pellets in Project Daedalus. If there are
> 100,000 of them, there could be plenty of time for the heat from one
> to dissipate before the next one is positioned. The whole firing
> process could take place over several years, with only a hundred or
> fewer per day.
"Thermally hostile" in terms of dealing with heat from the Sun and shedding
waste heat from your internal power sources. The main way to dissipate
heat in a vacuum is via radiation, and if you look at most advanced spacecraft
designs you'll see huge radiators or heat sinks. The Shuttle had radiators
inside the bay doors, which is why the were kept open while in orbit.
(You could also quickly shed heat by venting steam, but that's not viable
for a long-term mission except in a dire emergency situation).
For an Orion spacecraft, you have a bunch of pulse units (boom-booms) stored
in one or more magazines, and there's a mechanical system that removes them
one at a time and ejects them out the back, like a big juke box or vending
machine. Depending on the pulse unit's mass, that's going to require a
non-trivial amount of wattage. Over time, enough waste heat would build
up to damage those systems, so you need away to dump it.
Then you have heat beating on you from the Sun, at least early on in the
mission; that needs to be dealt with as well. The Apollo spacecraft did a
"barbeque roll", basically rotating on the long axis so that heat didn't
build up on one side.
Also, from what I remember of the Orion project, the pulse units were
to be ejected and detonated on the order of every few seconds.
>
> > I've seen some
> > discussion of what would happen with the pusher plate in the event
> > of a dud and how to mitigate the damage from that.
>
> The only kind of dud that could cause damage is a "dud" that exploded
> prematurely, and I think that problem has already been solved by
> available technology. Certainly we aren't going to send bombers with
> bombs that explode so soon that they damage the plane that dropped
> them.
>
In this case, a dud is a dud; a bomb that *doesn't* explode, or explodes later
than expected. The pusher plate has a series of shock absorbers to even out
the pulse, and with the expected firing rate those shock absorbers would always
be in some compressed state. In the event of a dud the absorbers would extend
fully, and the force of that could conceivably damage the spacecraft.
That's an engineering issue, and can be surmounted, but it's one of the things
that came up during the initial project.
>
> > �Having said that,
> > I don't think the engineering is insurmountable, just bloody difficult
> > compared to building something like a VASIMR.
>
> What's that?
>
Variable Specific Impulse Magnetoplasma Rocket; basically an electronic
propulsion system, sort of (but not quite) like the ion drives on the
Deep Space 1 and Dawn spacecraft. Ion drives have very high specific
impulse (they're very efficient), but have very low thrust; you could
not launch a spacecraft from the ground using ion propulsion. The VASIMR
concept allows you to switch between high-thrust, low Isp and low-thrust,
high Isp modes, although I don't think it offers sufficient thrust for
ground launch, at least not from Earth.
>
> > And that's just the propulsion end; nobody talks about the habitat
> > end, which has non-trivial engineering challenges of its own.
>
> My DP hypothesis has the panspermists sending prokayotes to all but
> the nearest systems. They would be in the form of spores, so the
> habitat problem is minimal.
They still have to be protected from radiation, and they probably need to be
kept at some minimum temperature. However, I'll admit I was thinking in
terms of crew, not seeding.
The thing about seeding, though, is that you have to get from here to there
before your spacecraft simply falls apart from age, meaning you need to
accelerate to some appreciable fraction of the speed of light, meaning you'll
need to *slow back down* when you reach your destination (otherwise your seeds
are going to slam into their target at some appreciable fraction of c, which I
don't think would be survivable).
>
> > The issues *I* worry about are gathering and securing all that
> > fissionable material in one place, and actually launching the bastard.
> > I've seen proposals to use SRBs or other types of boosters to lift a
> > fully-assembled spacecraft out of the atmosphere,
>
> Panspermia is many centuries away for us. By the time we have
> gathered enough information to undertake such a project, we will have
> long-established colonies on the moon and on various asteroids, where
> the spaceships can be built, and then launched conventionally from
> these low-gravity bases.
>
I don't take that as a given. Setting up self-sustaining colonies on the
Moon or Mars is going to be a lot more difficult than most people realize,
I think. And colonization is about a) getting rich, or b) extending political
influence. So far, there aren't any resources on either the Moon or Mars
that are worth the effort and expense of setting up permanent colonies to
extract. Yeah yeah yeah, 3He, aneutronic fusion, blah blah blah radioactive
fishcakes. As has been pointed out in this thread, we've yet to create a
working fusion power plant; until then, there's really not point in getting
excited about 3He.
[snip]
>
> > Low-yield, not-horrible-fallout, but still...nukes.
>
> The hydrogen bombs would only start to explode when the ship is
> millions of miles from any place where the fallout could cause a
> problem.
Which goes back to something I said in the part I snipped; ideally,
the Orion should launch under its own power because it has an insane
lifting capacity. Using conventional rockets to lift it out of the
magnetosphere before having it go nuclear is like using a bunch of go-carts
to push a semi up an on-ramp, at which point the semi starts its engine.
That's a silly conops. Yes, driving a semi up an on-ramp won't increase
anyone's chances of dying of cancer (at least, not appreciably), but I
think it's a reasonable illustration.
*If* we could develop "clean enough" nukes and *if* we could find a way to
launch it safely, then that would be the right course of action (provided
there's a customer willing to fund the development and acquisition of several
thousand nuclear bombs). I just don't know enough about nuclear physics to
make a judgement on how possible that is.