More New Details on NASA's CEV Launcher Studies
TheEqualizer writes "Continuing on the NYT story on NASA's current CEV launcher plans, spaceref has an even
more extensive look with detailed assessments of the available options. By all accounts, it looks like NASA is picking up where it left off with Apollo but also combining it with established Shuttle technology -- the capsule concept of the 1960s atop the shuttle boosters of the 1970s being the winning combination under the current budgetary limitations. However, is this coupling of
old technology and designs really the best we can do?"
.. space planes? Take off and land just like an airplane. Whatever happened to that idea?
The unforgiving results of the rocket equation when applied to the orbital velocity (as determined by the Earth's mass and radius) and the chemical energy available per lb of propellant. They all combine to make the task just barely possible. You get the impression that that some god wanted us to be able to get to space - but that it should be a serious challenge.
When your spacecraft must be made almost entirely of propellant it wants to be as close as possible to a sphere: lots of internal volume for propellant, minimum weight of the enclosing envelope. Airplanes really don't want to be anything like a sphere. They like un-spherelike protrusions known as wings. These weigh a lot, especially when you need to cover that much surface area with a heavy thermal protection system.
Landing with wings or lifting bodies can make sense in some circumstances but taking off with wings is ridiculous. The weight of the spacecraft at launch is much higher. If you size your wings for take-off weight you will pay the penalty of those big wings all the way to orbit and back (if it can even make it to orbit).
Just because the idea is intuitively appealing doesn't mean that it makes sense from an engineering point of view.
Weight happens.
Stop worrying about the risks of nuclear power and start worrying about the risks of not using nuclear power.