Re: OT: Ares engine test
- From: Jack Linthicum <jacklinthicum@xxxxxxxxxxxxx>
- Date: Sun, 13 Sep 2009 02:58:21 -0700 (PDT)
On Sep 13, 1:30 am, Fred J. McCall <fjmcc...@xxxxxxxxx> wrote:
"David E. Powell" <David_Powell3...@xxxxxxx> wrote:
:On Sep 12, 6:49 pm, Jack Linthicum <jacklinthi...@xxxxxxxxxxxxx>
:wrote:
:>
:> Not necessarily, there was a comparison between Apollo technology and
:> Saturn technology and some of each was included in Ares. Now there is
:> another factor in that the moon mission seems to be thought of as
:> unnecessary.
:>
:
I'm curious just what from Saturn Jack thinks was incorporated in
Ares.
:
:The workups in computers, wind tunnels and so forth still take huge
:time, then the mock up phase etc.
:
:The space program has been dragged out for so long. Punting it another
:couple years isn't a good idea with the Space Shuttle due to phase out
:soon.
:
:If it is a feasible design, there is something to be said for just
:going with it.
:
This is how we got the Shuttle. A history of bad decisions isn't a
good reason to go with the bad decisions.
:
:If there are other boosters under consideration, then they need to be
:put out in the open, tested and man rated. Without doing that it
:removes a program without anything in the pipe to take its place.
:
:The moon mission may be needed to get the program going. Direct to
:Mars is a big jump in capacity, and there is a lot of generational
:knowledge that would be nice to have before a Mars shot.
:
Mars is a whole new rocket. Ares V will never get built under this
Congress and Administration. Trillions for shovels but not a nickel
for anything more sophisticated.
--
"The reasonable man adapts himself to the world; the unreasonable
man persists in trying to adapt the world to himself. Therefore,
all progress depends on the unreasonable man."
--George Bernard Shaw
The J-2X engines were considered
Earth Departure Stage
The upper stage (Earth Departure Stage) being designed at Marshall, is
propelled by a J-2X main engine fuelled with liquid oxygen and liquid
hydrogen. The J-2X is an evolved variation of two historic
predecessors: the powerful J-2 upper-stage engine that propelled the
Apollo-era Saturn 1B and Saturn V rockets to the moon and the J-2S, a
simplified version of the J-2 developed and flight-tested in the early
1970s but never flown.
http://www.aerospaceguide.net/spacerocket/aresv.html
and the NASA version, longer, of course
http://www.nasa.gov/mission_pages/constellation/ares/aresV/index.html
.
- References:
- OT: Ares engine test
- From: Jack Linthicum
- Re: OT: Ares engine test
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- Re: OT: Ares engine test
- From: Keith Willshaw
- Re: OT: Ares engine test
- From: Andrew Swallow
- Re: OT: Ares engine test
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- Re: OT: Ares engine test
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- Re: OT: Ares engine test
- From: David E. Powell
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