Question:
What kind of rocket propulsion systems will we have in a f
few years?
What will be their acceleration (maximum) and their probable flight
velocity?
Any info would be appreciated.
Replies:
It is hard to tell. We have tried rockets with solid fuel, liquid
fuel, and for a while we tried nuclear reactors as engines. The
maximum acceleration will depend on the applied force. Accelerations of
a few times the earth's acceleration will be common as they are now.
The velocity will depend on the burn time. It is hard to be
specific unless you are working for nasa. It might be well to
ask them.
samuel p bowen
That is going to be an impossible question to answer, as the
folks at NASA do not know. I just saw an article in a recent
Aviation Week and Space Technology that a NASA committee is
just working on that right now. Their goal is to be totally
revolutionary instead of just rehashing old ideas, so the
answer to your question is truly difficult to answer. The
type of spacecraft this next generation will go in is pretty
well determined. The big goal there is a single-stage -to-
orbit (SSTO) craft. As the name implies it will launch as
one complete unit and remain that way until orbit. Some
versions on the drawing board have the ship also being
reusable. The first prototype has already been test fired,
the DC-X.
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