NASA's Plans for the Future
FleaPlus writes "ABC News, Pasadena Star-News, and Space Politics report on a recent statement by NASA chief Michael Griffin on NASA's plans for the future and how it will be reflected in their annual budget. Griffin has ordered preparations for one last shuttle servicing mission to the Hubble Space Telescope. He also plans to greatly accelerate development of the Crew Exploration Vehicle to have it ready when the Space Shuttles retire in 2010, stating that the CEV 'needs to be safe, it needs to be simple, it needs to be soon.' Some other highlights include $34 million for the Centennial Challenges prize program and the possibility of completing the space station with unmanned rockets after the shuttles retire. However, due to budget limitations, the cost of returning the Space Shuttles to flight, and over $400 million in Congressional earmarks, a number of other areas will see delays, including space station, aeronautics, and exploration research. NASA also plans on restructuring Project Prometheus to focus on developing space-qualified nuclear power systems for use in human and robotic surface operations, instead of a probe to Jupiter's moons." The Washington Post has a look at NASA's future as well.
Atleast the Russians will send you up if you're fit enough and loaded, NASA doesn't even do that.
So why would this plan be a good one?
-WolfWithoutAClause
"Gravity is only a theory, not a fact!"... they could have a new type of spacecraft much earlier. Russian engineers are pretty advanced in their plannings for a soyuz replacement: Kliper
http://www.russianspaceweb.com/kliper.html
http://www.astronautix.com/craft/kliper.htm
http://en.wikipedia.org/wiki/Kliper
the maiden flight was originally planned for 2007-2008 if I remember that correctly (read it in a German aviation magazine (Fliegerrevue) some time ago), but as usual with such projects and russia: sadly they have no more money to complete it. Relatively little american money could have a huge effect here. But I guess national pride on both sides will prevent this from coming true.
regards, sqar
Forget the Ramjet, I think you meant Scramjet ala the X-43.
I'm still not so sure about the Scramjet. The engine itself is a great idea, but the structural requirements are terrible. Even a minor flaw in the surface of the vessel would lead to catastrophe.
The grandparent probably has it right. If you use Jet engines to get to a higher altitude, the efficiency of nuclear thermal engines can take you the rest of the distance without having to go hypersonic in thick atmosphere.
Interestingly, the "best" solution may even be a ramjet engine. Since a nuclear engine can run on any fluid, what more efficient method exists than pulling oxygen from the atomosphere? And if you afterburn with hydrogen, you're going to get one hellva kick in the pants. (Alternatively, you can turn it around and heat the hydrogen while "burning" the oxygen")
Amazingly, we already have the engine to do this. Pratt & Whitney's TRITON engine is the perfect solution. As a "tri-modal" engine, it's capable of three modes of operation:
1. Low atmosphere afterburning for high powered launches.
2. Upper atmosphere and orbital transfer propulsion using pure hydrogen fuel.
3. Low fission rate "idle" mode which produces ~200 kW of power. (More than enough for onboard systems.)
The implications of this engine are staggering. Thanks to the tungsten clad design, it can be used anywhere without polution. Which means that we can have a single engine type that can not only produce massive thrust on takeoff, perhaps even produce the much covettd and highly efficient ramjet. (Rocket scientists love the idea of taking oxygen from the atmosphere, but don't normally want their rockets spending enough time in the lower atmosphere to make it worthwhile). But also an engine type that is highly efficient in upper-atmosphere and "space" areas. Plus, the craft can ditch heavy batteries and fuel cells in favor of drawing all its power from the engines. That power would even be available for electrical manuvering thrusters so that the amount of propellant carried can be reduced. Thus some of the weight you pay for in heavier engines can be regained in reducing redudant systems.
If we're going to get a bird in the air in the near future that can get people to orbit cheaply and safely, nuclear is where my money is.
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