vociferous said:
I did read the entire article.
Did you read the part that said "Nobody knows how to do it"?
That is the key sentence in the entire article.
For instance, I do not interpret the article to imply that he felt it was impossible to use thrusters at all to slow the descent, which would be absurd since the Viking landers used thrusters on Mars.
That's a non sequitur. The Viking landers could use thrusters to land precisely because they were small. One of the myriad of nasty facts that confronts putting humans into space is the square-cube law. If you scaled a mouse up to the size of an elephant it would die. The square-cube law dictates that elephant physiology is very, very different from mouse physiology. The same applies to those little Viking landers. Space vehicles don't scale up because of the square-cube law. More mass needs to be added because of structural integrity issues. More thrusters needed to be added because thrust is proportional to throat area. That means even more mass. The end result is that a large vehicle is elephantine compared to the mouselike characteristics of a small vehicle.
Furthermore, I am not convinced that the turbulence is an insurmountable engineering program.
It is a huge issue, one we do not know how to solve.
We've been landing VTOL craft on Earth using nothing but thrust since before we landed men on the moon.
That's another non sequitur. Aircraft don't carry their own oxidizer, and they don't go anywhere close to the speed of a reentering spacecraft . It's more like 1/20th of the speed in the case of a VTOL aircraft vs a reentering spacecraft , and that means 1/400th the energy needs to be dissipated.
Even if, for the sake of argument, we just agree that it is impossible to land such a single mass on Mars, then we simply use a different engineering paradigm.
It's so simple if you simply hand-wave away all the problems!
There's only so much you can shrink a spacecraft that will safely land humans. The Apollo command modules were 6.5 times as massive as is the Mars Science Laboratory rover. Landing a vehicle that is 6.5 times heavier not just 6.5 times harder. It's harder than we can imagine.
We don't know how to do it. The Apollo command modules carried the barest minimum of life support needed to bring humans from separation from the service module down to the Earth, where they would be whisked away via helicopter shortly after splashdown. A Mars lander would need to carry a significant amount of life support (air, water, food, life support equipment, etc.). And a hefty rover. And a launch vehicle.
Why a launch vehicle? Not bringing the astronauts back home is a death sentence. We haven't the foggiest idea of how to grow food away from home. For a little while, and for a few bites of lettuce to augment otherwise boring freeze dried food, yes, we can do that. A fully sustaining farm? We don't know how to do that.
Why a rover? Unless we can land several months worth of life support with that one vehicle, we need to send multiple landing vehicles. Those other landers are likely to land tens of kilometers apart. The Mars Science Laboratory represents the state of the art in precision landing on Mars. It's one sigma landing ellipse was 20 km × 7 km. The probability of landing within that one sigma ellipse is about 39%. Tripling each dimension (60 km × 21 km) yields a probability of 98.9%. Those aren't great odds, but close to the target for human spaceflight activities. We'll need that rover to go pick up the water, food, and equipment that landed tens of kilometers away.
I think the crux of the difference is between understanding the distinction between us not having a fabrication-ready design for a Mars mission today and a Mars mission simply being beyond our current level of technology.
I think the crux of the problem is that you don't know how impossibly hard it is, even using technology that doesn't exist yet. We don't know how to do it. I've mentioned but three of the things we don't know how to do. There are a number more.