Simulation of the Mars Science Laboratory Sky Crane
An anonymous reader points us to Gizmodo for a fascinating video of NASA's Sky Crane. "When I read that the UFO-looking Mars Science Laboratory's aeroshell would use a floating crane — called Sky Crane by NASA — to softly land the rover on Mars, I couldn't believe it. Now, watching this hyper-realistic NASA simulation, I still can't believe how the whole thing works. I don't know about you, but the whole operation mesmerizes me to no end."
That is so complicated. The "beach ball" idea from the two current rovers was much better.
Maybe if the Sky Crane was a ballon system so it can float around Mars would make this better. But still way too complicated.
Almost realistic: the simulation approaches what the same inputs would do to the real system.
Realistic: the simulation behaves the same way as the real system.
Hyper-realistic: the simulation is better at realism that they real system?
What next, über-realistic? Or is profit next?
If I have nothing to hide, don't search me
Trebuchet's don't scale very well. AFAIR, neither did the beach ball. This thing is lots bigger and heavier.
Faster! Faster! Faster would be better!
We've got to flex some of our engineering muscle in front of our Martian friends so they will less inclined to invade us. In this light, clearly this > bouncing beach ball delivery.
Maybe have an external speaker system that blasts Ride of the Valkyries during descent, too.
It has to do with mass, the MSL rover, at 900 kg, is much too heavy to land using the airbag methods that landed the 180 kg Spirit and Opportunity rovers. To give a sense of scale, the MSL rover is the size of a minivan, while Spirit and Opportunity are the size of small riding mowers. See:
http://en.wikipedia.org/wiki/Image:Mars_Science_Laboratory_empty_chassis.jpg
The video showed the lander dropping straight down on the wheels without any side motion at all. This seems unlikely to me. The rover would be swinging like my dick on those cables unless there were some thrusters used to stop any swinging motion.
Other than that, it's a pretty neat idea, ESPECIALLY for a spacecraft which is not a rover. A rover can move out of the landing zone, but a stationary spacecraft cannot. It would be sitting on soil which has traces of hydrazine from the landing rockets - but this system would avoid that problem.
Fascism trolls keeping me up every night. When I starts a preachin', he HITS ME WITH HIS REICH!
So what? This thing is much larger than anything landed anywhere before, with the exception of the manned LEM.
The Apollo capsule had an atmosphere much thicker (as in height) and much thicker (as in density) than the Mars landers have available. The Apollo LEM could use rocket braking because of the Moon's low gravity.
Mars is a stone cold bitch to land on because the atmosphere is too thin to completely rely on parachutes, and Mars' gravity is too high to rely completely on rockets.
Not exactly. It is radioisotope power but it is not nuclear power in the sense that there is a reaction going on. The simple decay gives off heat. As I recall it's not that much, either. Something on the order of 110 watts. Still, it's much better than relying on solar panels. Here's a nice page of fact sheets for the mission.
http://www.rootstrikers.org/
The problem with soft-landing heavy objects on Mars is that there's not enough atmosphere for aerobraking and parachutes to do the job, so the approaches used for Earth re-entry won't work. There's too much gravity for landing on rockets. as with lunar landers, without most of the payload being landing fuel. The problem gets harder as the mass goes up. This was realized only about five years ago, to the embarrassment of some within NASA. So there are now various complicated hybrid schemes, like this.
The scheme with the cables does not look promising. Unlike Luna, Mars has winds and weather. This looks like one of the student lander designs from NASA's high school curriculum.
One bad feature of this design is that the actual landing forces have to be taken by the rover's suspension. Previous designs had the rover inside the landing module, not underneath it. That approach uses crushable components (air bags, crushable blocks, collapsible legs, etc.) to cushion the landing. With this "flying crane" approach, the autopilot has to do a really, really smooth landing or the rover will be broken.
Even in their most recent plan for this Mars descent, their first mode of descent is to drop the module like a stone, using elaborate and expensive heat shielding to protect the even-more-expensive gear. But maybe -- just maybe -- they could take a lesson from Spaceship One and just take their time getting this thing down to the ground.
Sorry - but you have no clue. Mars' atmosphere at the surface has about 1% of the Earth's density, making something like aerodynamic flying impossible.
There simply isn't any other way than "dropping like a stone" - even on their parachutes, the rovers did exactly that. Those parachutes were supersonic, and their
main purpose was trajectory stabilization (although they did of course contribute to the braking).
Go read this article already linked above for a well written explanation about why
landing on Mars is actually very hard and cannot in any way be compared to landing on Earth.