Posted by
CmdrTaco
on from the still-no-power-at-my-house dept.
swestcott writes "The New York Times has an interesting article about the transition to the Obama administration and NASA's transition to the new Orion."
I'd like to see a move away from the Ares-Orion stack and a move towards the more versatile Jupitor plan.
I'd also like to see us make serious use of the press and make our move back to the Moon and eventually to Mars as much as an event as the original Mercury-Gemini-Apollo missions. You have to make it romantic for the public so they feel like writing their Congresscritters to support funding.
-- Politics is the art of looking for trouble, finding it everywhere, diagnosing it incorrectly and applying the wrong fix.
But teh gubment is BAD! Corporations are teh GUD!
by
damburger
·
· Score: 5, Interesting
NASA is being set up to fail, because of the prevailing pro-corporate attitude in the US. The idea is that private entities are efficient, responsible, and capable of long-term planning and technological development. So nobody wants to be accused of being 'socialist' by giving more money to a government agency.
The original Apollo program cost $135 billion in modern(ish) money over about 10 years:
So the US government is expecting a great deal more, for a lot less money, when there has been no real development in interplanetary manned travel since Apollo.
-- If we can put a man on the moon, why can't we shoot people for Apollo-related non-sequiturs?
Re:Are all the news stories sensationalist?
by
oneiros27
·
· Score: 4, Interesting
Griffin's quote and basic sentiment reminded me of JFK's 1962 Rice University speach:
... We choose to go to the moon. We choose to go to the moon in this decade and do the other things, not only because they are easy, but because they are hard, because that goal will serve to organize and measure the best of our energies and skills, because that challenge is one that we are willing to accept, one we are unwilling to postpone, and one which we intend to win, and the others, too....
-- Build it, and they will come^Hplain.
Interesting conversation...
by
RobBebop
·
· Score: 4, Interesting
"I don't frankly know what the answer is," [Dr. Crowley, of MIT] said, "but I know it's a lot closer and a lot more complicated answer than the one playing out in the media and the blogs."
I think they're talking about us.
===
But in all seriousness, the cost of running the shuttle for 5 years is $x and the cost of developing the Constellation program in 5 years is $y. Meanwhile, NASA's budget is not x+y and if they wanted to try to develop Constellation in 3 years its cost would be closer to $y^2.
It seems like people can't grasp the rudimentary guideline of engineering development: you've got limitations in quality, cost, and timeliness, and on any challenging project you need to pick one of those limitations that you won't particularly worry about.
I do like the articles conclusion though... NASA's budget is way too small for the amount of good that it can do for the world and for the amount of high-tech science jobs that it can create. As long as everybody in the nation has food, shelter, telecommunications, and power... there is no reason NASA's budgets shouldn't balloon.
Re:Cancel Orion, keep the Shuttle
by
Amiga+Trombone
·
· Score: 4, Interesting
We managed to find $25 billion to fund bailing out a moribund auto industry. It seems to me putting that money into a forward-looking industry rather than a backwards-looking one would have been a much more worthwhile use of the money.
Re:Alternatives : DIRECT / JUPITER
by
Dawn+Keyhotie
·
· Score: 3, Interesting
Well, since you asked...
The Jupiter is a straightforward evolution of the Shuttle system into a traditional rocket. 1) The Shuttle itself is removed from the stack. 2) The external tank is modified and strengthened to carry a payload on top and engines on the bottom. 3) The three expensive shuttle main engines are replaced by two expendable engines and moved to the bottom of the external tank. 4) A 10 meter payload fairing is mounted on top of the fuel tank, with a capacity of up to 20 tons of hardware. 5) The Orion spacecraft is placed on top of the payload fairing. 6) A crew escape system is placed on top of the Orion.
Now, that sounds complicated, but it is much simpler once you see the results: DIRECT Launcher.
What that gives you is a versatile rocket for placing a six man crew PLUS 20 tons of cargo at the space station in a single launch. This configuration by itself is almost a complete replacement for the Shuttle, except for the Shuttle's ability to return payloads to Earth. Or, the Jupiter could lift 50 tons of payload to LEO in an unmanned configuration. Ares-I can't do either of those jobs, now or ever. No existing or planned EELV can do that. Ares-V would be such a behemoth (if it ever flies) that it would be much too expensive to fly on a regular basis. That is why Jupiter-120 is more versatile than Ares-I.
The second phase of the Jupiter proposal is to add a second liquid rocket stage on top of the core stage, while at the same time adding a third engine at the bottom. That will enable the Jupiter to place up to 110 tons of payload in LEO in a single launch. For the lunar mission there would be two launches, just as for Ares. One launch would carry the Orion CEV and the Altair lunar lander. The second launch would just lift extra fuel and the upper stage. The Orion and Altair would dock with the upper stage, then use the upper stage to send them to lunar orbit.
Jupiter can also be used to launch exploration missions to Near Earth Orbit (NEO) objects, launch large scientific payloads such as really big telescopes, Earth recon sats, etc. Jupiter is small enough and affordable enough to be used on a regular basis, but still twice as powerful as any existing or planned commercial launcher (including SpaceX).
Because Jupiter is so cleanly derived from the Space Shuttle, it needs much less development money than Ares. In fact, the entire Jupiter project, including lunar capability, would cost less than half of what is planned for Ares. The Ares-I project is going to cost around $15 billion by itself, with another $16-17 billion for Ares-V. Jupiter is projected to cost less than $12 billion for both the initial LEO version and upper stage. This economy is possible because both versions use the exact same "common core", with only the addition of the third main engine and the upper stage to allow lunar missions.
So the whole DIRECT premise is to build a single new "medium" sized rocket from the Shuttle heritage, which can be used for Earth orbit and lunar exploration. Ares requires the development of two entirely new rockets, neither of which have much at all in common with Shuttle or each other. Jupiter can use most of the existing launch infrastructure, including crawlers, crawlerways, and the fixed portion of the existing launch towers. Ares-I and -V both require extensive modifications of the launch pads, and both launch pads will be dedicated to one or the other vehicle, since they are so different. And at this point, the Ares-V is getting so large that it may require completely new pads and crawlerways to be built.
Jupiter can be used with or without an upper stage. It can launch manned missions with or without payloads. It can launch payloads with or without crew. It can be ready up to three years sooner than Ares-I, which is actually planning their first manned flight for 2016. 2016! Jupiter will still take until late 2013, but that is because it has to wait for the Orion CEV to be finished.
And that's why Jupiter is more versatile, affordable, and sensible than Ares.
Troll biter's rehab. Damn but it's hard to ignore the clueless trolls. I guess I'm off the wagon again, I have to respond.
"Pork"? WTF??? Do you have any idea how many technological advances, especially in medicine, that have come from the space program?
Do you have cable TV? A cell phone? GPS? None of these would be possible were it not for the "pork spending" on space. All of them rely on sattelites.
"physics"? What kind of drooling anti-nerd can't understand that launching a heavy machine into outer space doesn't use physics?
"Chemistry?" You realise how much chemistry work is involved in fuels?
If I were modding I would be undecided whether to mod the parent as "troll" or "funny". Who let all these clueless MBAs in here anyway?
Free Martian Whores!
I'd like to see a move away from the Ares-Orion stack and a move towards the more versatile Jupitor plan.
I'd also like to see us make serious use of the press and make our move back to the Moon and eventually to Mars as much as an event as the original Mercury-Gemini-Apollo missions. You have to make it romantic for the public so they feel like writing their Congresscritters to support funding.
Politics is the art of looking for trouble, finding it everywhere, diagnosing it incorrectly and applying the wrong fix.
NASA is being set up to fail, because of the prevailing pro-corporate attitude in the US. The idea is that private entities are efficient, responsible, and capable of long-term planning and technological development. So nobody wants to be accused of being 'socialist' by giving more money to a government agency.
The original Apollo program cost $135 billion in modern(ish) money over about 10 years:
http://en.wikipedia.org/wiki/Apollo_program#Program_costs_and_cancellation
Whereas Constellation is being given $3 billion a year for about 20 years, or about $60 billion in current money.
http://www.whitehouse.gov/omb/expectmore/detail/10004394.2006.html
So the US government is expecting a great deal more, for a lot less money, when there has been no real development in interplanetary manned travel since Apollo.
If we can put a man on the moon, why can't we shoot people for Apollo-related non-sequiturs?
Griffin's quote and basic sentiment reminded me of JFK's 1962 Rice University speach:
Build it, and they will come^Hplain.
"I don't frankly know what the answer is," [Dr. Crowley, of MIT] said, "but I know it's a lot closer and a lot more complicated answer than the one playing out in the media and the blogs."
I think they're talking about us.
===
But in all seriousness, the cost of running the shuttle for 5 years is $x and the cost of developing the Constellation program in 5 years is $y. Meanwhile, NASA's budget is not x+y and if they wanted to try to develop Constellation in 3 years its cost would be closer to $y^2.
It seems like people can't grasp the rudimentary guideline of engineering development: you've got limitations in quality, cost, and timeliness, and on any challenging project you need to pick one of those limitations that you won't particularly worry about.
I do like the articles conclusion though... NASA's budget is way too small for the amount of good that it can do for the world and for the amount of high-tech science jobs that it can create. As long as everybody in the nation has food, shelter, telecommunications, and power... there is no reason NASA's budgets shouldn't balloon.
Support the 30 Hour Work Week!!!
We managed to find $25 billion to fund bailing out a moribund auto industry. It seems to me putting that money into a forward-looking industry rather than a backwards-looking one would have been a much more worthwhile use of the money.
Well, since you asked...
The Jupiter is a straightforward evolution of the Shuttle system into a traditional rocket. 1) The Shuttle itself is removed from the stack. 2) The external tank is modified and strengthened to carry a payload on top and engines on the bottom. 3) The three expensive shuttle main engines are replaced by two expendable engines and moved to the bottom of the external tank. 4) A 10 meter payload fairing is mounted on top of the fuel tank, with a capacity of up to 20 tons of hardware. 5) The Orion spacecraft is placed on top of the payload fairing. 6) A crew escape system is placed on top of the Orion.
Now, that sounds complicated, but it is much simpler once you see the results: DIRECT Launcher.
What that gives you is a versatile rocket for placing a six man crew PLUS 20 tons of cargo at the space station in a single launch. This configuration by itself is almost a complete replacement for the Shuttle, except for the Shuttle's ability to return payloads to Earth. Or, the Jupiter could lift 50 tons of payload to LEO in an unmanned configuration. Ares-I can't do either of those jobs, now or ever. No existing or planned EELV can do that. Ares-V would be such a behemoth (if it ever flies) that it would be much too expensive to fly on a regular basis. That is why Jupiter-120 is more versatile than Ares-I.
The second phase of the Jupiter proposal is to add a second liquid rocket stage on top of the core stage, while at the same time adding a third engine at the bottom. That will enable the Jupiter to place up to 110 tons of payload in LEO in a single launch. For the lunar mission there would be two launches, just as for Ares. One launch would carry the Orion CEV and the Altair lunar lander. The second launch would just lift extra fuel and the upper stage. The Orion and Altair would dock with the upper stage, then use the upper stage to send them to lunar orbit.
Jupiter can also be used to launch exploration missions to Near Earth Orbit (NEO) objects, launch large scientific payloads such as really big telescopes, Earth recon sats, etc. Jupiter is small enough and affordable enough to be used on a regular basis, but still twice as powerful as any existing or planned commercial launcher (including SpaceX).
Because Jupiter is so cleanly derived from the Space Shuttle, it needs much less development money than Ares. In fact, the entire Jupiter project, including lunar capability, would cost less than half of what is planned for Ares. The Ares-I project is going to cost around $15 billion by itself, with another $16-17 billion for Ares-V. Jupiter is projected to cost less than $12 billion for both the initial LEO version and upper stage. This economy is possible because both versions use the exact same "common core", with only the addition of the third main engine and the upper stage to allow lunar missions.
So the whole DIRECT premise is to build a single new "medium" sized rocket from the Shuttle heritage, which can be used for Earth orbit and lunar exploration. Ares requires the development of two entirely new rockets, neither of which have much at all in common with Shuttle or each other. Jupiter can use most of the existing launch infrastructure, including crawlers, crawlerways, and the fixed portion of the existing launch towers. Ares-I and -V both require extensive modifications of the launch pads, and both launch pads will be dedicated to one or the other vehicle, since they are so different. And at this point, the Ares-V is getting so large that it may require completely new pads and crawlerways to be built.
Jupiter can be used with or without an upper stage. It can launch manned missions with or without payloads. It can launch payloads with or without crew. It can be ready up to three years sooner than Ares-I, which is actually planning their first manned flight for 2016. 2016! Jupiter will still take until late 2013, but that is because it has to wait for the Orion CEV to be finished.
And that's why Jupiter is more versatile, affordable, and sensible than Ares.
"The only good windmill is a tilted windmill."