Re: How big would an SSTO be?
- From: Monte Davis <monte.davis@xxxxxxxxxxx>
- Date: Fri, 06 Jul 2007 08:50:29 GMT
einarbb@xxxxxxxxx wrote:
One way to
square the equation might be for the thing to take off only partially
fuelled, then once airborne and at a reasonable altitude it could tank
up in the air.
How does that sound like?
Sounds like the fine old space-fan approach of "we'll solve tough
Problem X by assuming the solution of comparably tough (if not
tougher) Problem Y."
If the refueling is done in a speed/altitude regime comparable to
air-to-air refueling as done today, you've just reinvented Orbital
Sciences and other air-launch approaches (which have their merits, but
aren't exactly paradigm-busters)..
If you're talking about hypersonic refueling -- i.e. bringing two
shock envelopes that close together and then separating without
problems -- you've just bought yourself a loooooooong R&D program.
And, of course, an operations model in which every launch is in fact
two launches.
Sounds like a sure way to drive costs down.
.
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