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Thruster May Shorten Mars Trip (from six months to a week!)
Photonics.com News ^
| 9/7/07
Posted on 09/10/2007 11:31:01 AM PDT by LibWhacker
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To: LibWhacker
The bad news is it works just like the flux capaciter and requires 1.26 gigawatts to run.
41
posted on
09/10/2007 1:02:32 PM PDT
by
DungeonMaster
(John 2:4 Jesus saith unto her, Woman, what have I to do with thee?)
To: SampleMan
2. A lot of braking power. No, it wouldn't. They said that they would get you there in a week. Nothing about you being in any shape to ever come back. Just keep on accelerating until impact.
42
posted on
09/10/2007 2:50:14 PM PDT
by
PAR35
To: Clioman
Anybody know how long a human can function under sustained multiple g-loads?
It wouldn't be a heavy g-load. The thruster produces 35 micronewtons. 1 micronewton is 1,000,000th of a newton. The g-load would be very low.
43
posted on
09/10/2007 2:51:43 PM PDT
by
JamesP81
To: SamAdams76
So unless we can develop some kind of sophisticated radar that can allow our spacecraft to see these objects millions of miles away and automatically make slight corrections in course to avoid these tiny objects or unless we develop an exterior to the spacecraft that is impervious to collisions at high rates of speed, we are going to continue to be limited in how fast we can go in space.
There are only three solutions to the collision problem: deflector shields, sophisticated armor plating, or highly accurate and reliable weapons (probably lasers or particle beams) that can incinerate the objects. The weapons solution is likely unworkable; we're talking about having a computer system with a radar that can detect a tiny pebble from a million miles out, target, and fire on it before you run over it, correcting for lag imposed by the lightspeed barrier on your radar.
44
posted on
09/10/2007 2:55:18 PM PDT
by
JamesP81
To: ShasheMac; brityank; Forest Keeper; swatbuznik; Potts Mtn. Pappy; Kevmo; wastedyears; ...
45
posted on
09/10/2007 6:30:57 PM PDT
by
KevinDavis
(Mitt Romney 08)
To: FReepaholic
If you wanted to start and stop at rest you would need to have your thrusters on for half the trip in one direction and then reverse direction for the second half.
In the simple case of a constant force (assuming a constant mass):
x(t) = x_0 + v_0t + 0.5 * a t² (x_0 and v_0 are assumed to be zero)
a = 2*x(halfway)/t² = 2*50e9 m/(3.5 days)² = 1.09 m/s²
This is about 1/9th of a g. If they had the capability to have 1 g of acceleration then the transit time would only be 56 hours (1/3 of a week).
46
posted on
09/10/2007 6:53:15 PM PDT
by
burzum
(None shall see me, though my battlecry may give me away -Minsc)
To: FReepaholic
Oh, I should also mention that since power equals force times velocity, it probably wouldn’t be feasible to be able to power the thrusters after the beginning of the trip so the initial forces will have to be much higher.
47
posted on
09/10/2007 7:00:53 PM PDT
by
burzum
(None shall see me, though my battlecry may give me away -Minsc)
To: burzum
Oh, I should also mention that since power equals force times velocity, it probably wouldnt be feasible to be able to power the thrusters after the beginning of the trip so the initial forces will have to be much higher. Err, I mean that the thrusters will have the same power applied, but will lose thrust the faster you go, so your initial thrust has to be much higher than the lower thrust (using the same power) later in the trip (because KE = 1/2 mv² and you have to pay 4 times the energy for every doubling of velocity).
48
posted on
09/10/2007 7:05:10 PM PDT
by
burzum
(None shall see me, though my battlecry may give me away -Minsc)
To: burzum
Ummmmm ... no.
Whatever mass you're kicking out of the back of the vehicle is accelerated relative to the vehicle. No matter how fast the vehicle is going, if the mass-flow-rate and the delta-v is the same, the thrust produced is the same and the energy cost is the same.
49
posted on
09/10/2007 7:13:29 PM PDT
by
DuncanWaring
(The Lord uses the good ones; the bad ones use the Lord.)
To: LibWhacker
Once you go warp, you’ll never look back.
50
posted on
09/10/2007 7:14:44 PM PDT
by
toddlintown
(Five bullets and Lennon goes down. Yet not one hit Yoko. Discuss.)
To: LibWhacker
“That was just his desktop prototype. He says it’s scalable.
But I have a lot of doubts about it myself. We see too many of these too-good-to-be-true scams.
But... IF it’s real... OH, BOY!”
Maybe, just MAYBE, I’ll get to visit Mars before I die, after all.
Old Student <————CROSSES FINGERS REAL HARD!
51
posted on
09/10/2007 7:28:38 PM PDT
by
Old Student
(We have a name for the people who think indiscriminate killing is fine. They're called "The Bad Guys)
To: Red Badger
“If it was built by using off the shelf parts then its not patentable, IIRC.......”
Which means anyone who could read the blueprints could build one. (Given the cash, of course.)
Power to the People! ;)
I can see a LOT of people taking off on their own. Also a lot of debris fluttering down...
52
posted on
09/10/2007 7:31:09 PM PDT
by
Old Student
(We have a name for the people who think indiscriminate killing is fine. They're called "The Bad Guys)
To: DuncanWaring
You do not conserve energy in your case. KE = 1/2 mv². The higher the velocity, the higher the cost per incremental change in velocity. Since, P = F * v, your rocket would become much more powerful the faster it goes if it had a constant force. Does it make sense to you that an object that hasn’t changed its mass becomes more powerful the faster it goes when it is only powered by a constant power source?
53
posted on
09/10/2007 7:31:58 PM PDT
by
burzum
(None shall see me, though my battlecry may give me away -Minsc)
To: DuncanWaring
Oh, and before you mention it, an accelerating body is, by definition, not in an inertial reference frame. So your Galilean transformation arguments do not apply.
54
posted on
09/10/2007 7:36:27 PM PDT
by
burzum
(None shall see me, though my battlecry may give me away -Minsc)
To: timer; Shuttle Shucker
Feel like weighing in? ;)
55
posted on
09/10/2007 7:55:57 PM PDT
by
anymouse
To: Red Badger
35 µN? That aint a lot of cookies.................... That depends, actually -- space is funny that way. We used to model continuous thrust forces of 0.05 lb for the Shuttle (which weighs 225,000 lb). That's a tiny acceleration, but very noticeable over the course of an orbit.
If you can keep even this small thruster firing for long periods of time, it adds up to a lot. Of course, it really all boils down to power: how much does it take to get this mouse-fart thrust?
56
posted on
09/10/2007 8:09:19 PM PDT
by
r9etb
To: chrisser
if photons have no mass, how can they provide acceleration in a vacuum? They have no rest mass. But they have a small mass by virtue of the fact that they have energy:
Ephoton = mc2, so m = Ephoton/c2
And they have an exhaust velocity = c.
Thrust = mass flow rate * exhaust velocity. So if you have some number N photons per second, then
T = NEphoton/c2 * c = NEphoton/c.
I don't rightly know how you'd count photons, but it occurs to me that NEphoton is the total photon energy flux, so you don't really need to count photons, you just need to know the photon energy output by the thrust "beam".
57
posted on
09/10/2007 8:16:05 PM PDT
by
r9etb
To: LibWhacker
If my back of the napkin calculations are right, and If he can scale it up by a billion-fold (i.e., to 35,000 Newtons), a million kilogram ship (i.e., one of respectable size), starting at an initial velocity of zero, would travel about one kilometer towards Mars in a weeks time Uh, no. a = 35e3/1e6 = 35e-3 m/sec2.
It would take about 28.6 sec per meter per second -- so a day's thrust would give you around 3 km/sec of delta-V.
58
posted on
09/10/2007 8:20:44 PM PDT
by
r9etb
To: KevinDavis
To: FReepaholic
F=ma
F = 35 µN
m = Mass of your spacecraft
Solve for a!
(Hint, not a lot of G’s, but you don’t need a lot as long as the acceleration is constant for a long period of time...)
60
posted on
09/10/2007 9:11:42 PM PDT
by
Frank_Discussion
(May the wings of Liberty never lose a feather!)
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