davefoc said:
lyghtningbyrd said:
lyghtningbyrd,
I'd like to take a shot at an answer, but I'm no expert so take what I say with a grain of salt.
The big problem with getting into space is something called the rocket equation and the fact that you need to be going more than 15,000 miles an hour even for a low earth orbit. The concept is that you have to lift the fuel, to lift the fuel, to lift the fuel,......., to accelerate you to the final speed. So if you accelerate too slowly you have to carry too much extra fuel to support the flying rather than the accelerating.
I'm no expert either, but if i talk real fast maybe nobody will notice.
Wings and jet engines are useful to maybe 2,000 mph. For the remaining 16,000 mph they're dead weight. And for every pound that you've wasted on wings and jet engines, you need to carry ten pounds of fuel. That adds up real fast.
There is some advantages to something like you talk about if you could use air breathing engines for the first part of the trip so you didn't need to lift all the oxygen you needed. NASA and others have been theorizing around ideas like this for years. All of which seemed to have been abandoned for now. The scramjet engine was conceived to do just this.
So far as i know, we still don't have a practical scramjet engine. I saw a post claiming that scramjets wouldn't be practical much past Mach 11, which is only about 40% of the way to orbital velocity. However, that might be good enough for a first stage. My guess is that we're at least 30 years away from something like this.
There are other air-breathing proposals--LACE (liquid air cycle engine, i think) was a proposal to use the hydrogen rocket fuel with oxygen from the air. There was a British horizontal take-off horizontal landing proposal based around this. Unfortunately, they couldn't get funding.
The really cool idea to me, has been mass launchers. Just fling the stuff towards space getting a big chunk of the acceleration on the ground where you can accelerate the stuff with energy on the ground so you don't need to accelerate a lot of the fuel so you get around at least some of the consequences of the rocket equation. Alas, I haven't seen any articles suggesting this idea is going anyplace either.
There are a couple of proposals to keep most of the hardware on the ground. The mass launcher mechanism is going to submit the load to enormous accelerations--a 100 g launcher is still going to be 20 miles long. You'd want most of that in vacuum.
Another proposal was a launch laser--you put reaction mass on the bottom of your capsule and zap it with a whopping big laser beam. The energy from the laser gets depositied into the bottom layer of the reaction mass, which essentially explodes, but with more energy than any chemical reaction. Jerry Pournelle used this in some of his SF.