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Science Forum Index » Space - Shuttle Forum » Future of Orion??
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| Derek Lyons |
Posted: Thu Mar 08, 2007 2:20 am |
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André, PE1PQX <pe1pqx_geenviagra@planet.nl> wrote:
Quote: Op 8-3-2007, heeft Derek Lyons verondersteld :
André, PE1PQX <pe1pqx_geenviagra@planet.nl> wrote:
Derek Lyons was zeer hard aan het denken :
"Jorge R. Frank" <jrfrank@ibm-pc.borg> wrote:
It's not like we had a significant experience base to go stale in the
first place Jorge. Not only did the Mercury-Gemini-Apollo series
overlap each other to a large degree, they were all essentially first
generation systems.[1] Each program experienced significant flight
anomalies, and in Apollo's case, had at least two inflight failures
(15 docking, 17 SPS) that could easily have lead to LOM or LOCV.
inflight failures: What about Apollo 13 (exploded O2 tank)??
I discounted Apollo 13 because the accident was caused by component
damage during handling - unlike 15 and 17 where the causes are unknown
and could easily be failure modes which are rare but inherent to the
design. Apollo 13 type accidents from human error can happen even in
a mature program, 15 and 17 type incidents we cannot classify as the
causes are unknown.
D.
Then I'd like to know what happened on Apollo 15 and 17, did not know
there were some accidents during those flights.
15 was unable to dock to the LM during initial T&D - until 'brute
forced'. 17 suffered a failure of the primary control cables across
the gimbals between the SM and the SPS.
D.
--
Touch-twice life. Eat. Drink. Laugh.
-Resolved: To be more temperate in my postings.
Oct 5th, 2004 JDL |
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| Derek Lyons |
Posted: Thu Mar 08, 2007 2:22 am |
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"Greg D. Moore \(Strider\)" <mooregr_deleteth1s@greenms.com> wrote:
Quote: I dread another Mr. Fenyman interviewing NASA folks who believe Orion has a
1 in a 100,000 (or better) risk of mission failure based on sheer hope.
I dread another generation learning nothing about a spacecraft
accident except from Mr. Fenyman or his equivalent.
D.
--
Touch-twice life. Eat. Drink. Laugh.
-Resolved: To be more temperate in my postings.
Oct 5th, 2004 JDL |
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| Greg D. Moore (Strider) |
Posted: Thu Mar 08, 2007 2:34 am |
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"Derek Lyons" <fairwater@gmail.com> wrote in message
news:45faaae3.856300171@news.supernews.com...
Quote: André, PE1PQX <pe1pqx_geenviagra@planet.nl> wrote:
15 was unable to dock to the LM during initial T&D - until 'brute
forced'.
Which as I recall was a potential reason for aborting the mission. Since a
failur to dock in lunar orbit could have been a major problem.
(and wasn't the probe reused on a Skylab mission with similar results?)
Quote: 17 suffered a failure of the primary control cables across
the gimbals between the SM and the SPS.
Hmm, wasn't aware of that one.
Quote:
D.
--
Touch-twice life. Eat. Drink. Laugh.
-Resolved: To be more temperate in my postings.
Oct 5th, 2004 JDL
--
Greg Moore
SQL Server DBA Consulting
sql (at) greenms.com http://www.greenms.com |
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| Jorge R. Frank |
Posted: Thu Mar 08, 2007 9:49 am |
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fairwater@gmail.com (Derek Lyons) wrote in news:45faaae3.856300171
@news.supernews.com:
Quote: André, PE1PQX <pe1pqx_geenviagra@planet.nl> wrote:
Op 8-3-2007, heeft Derek Lyons verondersteld :
André, PE1PQX <pe1pqx_geenviagra@planet.nl> wrote:
Derek Lyons was zeer hard aan het denken :
"Jorge R. Frank" <jrfrank@ibm-pc.borg> wrote:
It's not like we had a significant experience base to go stale in the
first place Jorge. Not only did the Mercury-Gemini-Apollo series
overlap each other to a large degree, they were all essentially first
generation systems.[1] Each program experienced significant flight
anomalies, and in Apollo's case, had at least two inflight failures
(15 docking, 17 SPS) that could easily have lead to LOM or LOCV.
inflight failures: What about Apollo 13 (exploded O2 tank)??
I discounted Apollo 13 because the accident was caused by component
damage during handling - unlike 15 and 17 where the causes are unknown
and could easily be failure modes which are rare but inherent to the
design. Apollo 13 type accidents from human error can happen even in
a mature program, 15 and 17 type incidents we cannot classify as the
causes are unknown.
D.
Then I'd like to know what happened on Apollo 15 and 17, did not know
there were some accidents during those flights.
15 was unable to dock to the LM during initial T&D - until 'brute
forced'. 17 suffered a failure of the primary control cables across
the gimbals between the SM and the SPS.
You sure you got the mission numbers right? I recall the docking failure on
14, and the SPS gimbal problem on 16.
--
JRF
Reply-to address spam-proofed - to reply by E-mail,
check "Organization" (I am not assimilated) and
think one step ahead of IBM. |
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| Jeff Findley |
Posted: Thu Mar 08, 2007 3:34 pm |
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"Brian Thorn" <bthorn64@cox.net> wrote in message
news:vrfuu2l45or6sd1qs9ei04jkjqi25dhk8u@4ax.com...
Quote: On Wed, 07 Mar 2007 14:04:17 -0500, John Doe <jdoe@doe.org> wrote:
To a certain degree, yes. It will get mission designers back into the
practice of deep space operations sooner than a straight-to-Mars
project would, so we should (re-)learn many lessons before we start
the much higher risk Mars expeditions.
Going to the moon is like a weekend camping trip. Going to Mars is a real
expedition lasting more than a year.
You forget, NASA isn't re-doing Apollo sorties. Their plan is to build
a moonbase beginning with Landing No.1. That, most decidedly, will be
useful for follow-on Mars operations.
Not so much. Experience on the Moon does not necessarily apply to Mars
missions. The difference in day/night cycles makes a difference in power
and cooling systems for any lander/base. The difference in transit times
makes your transport ships a lot different. For the moon, the little CEV is
likely good enough to use as a lifeboat. A Mars mission lifeboat will have
to be a lot bigger and likely more fault tolerant due to the much longer
transit times.
Plus the gravity and atmosphere of Mars makes for much larger spacecraft in
general, since you need a lot more fuel to take off and return to the Earth.
Quote: So will any sorties from the
Moonbase that later astronauts make for exploration missions. That
will really help pave the way for how to explore Mars.
The presence of an atmosphere on Mars, as thin as it is, makes things like
spacesuit cooling systems much harder to build for a Mars miission. And the
higher Mars gravity makes suit design even tougher. The lunar soil is
likely harder to deal with because lack of erosion means the grains of dust
are extremely sharp. Hopefully Martain dust isn't as abrasive.
Quote: Besides, if Mars is the real expedition and the moon is the weekend
camping trip, then we are currently just doing jaunts around the
block.
Sort of. LEO makes a lot of things easier due to the lack of gravity, but
in some ways it's a hindrance.
Jeff
--
"They that can give up essential liberty to obtain a
little temporary safety deserve neither liberty nor
safety"
- B. Franklin, Bartlett's Familiar Quotations (1919) |
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| John Doe |
Posted: Thu Mar 08, 2007 3:50 pm |
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Jeff Findley wrote:
Quote: Sort of. LEO makes a lot of things easier due to the lack of gravity, but
in some ways it's a hindrance.
Unless NASA buys the Starfleet warp drive designs from Paramount Pictures, it
will still take a large number of months to get to and from Mars. And much of
that time will be spent in 0g. Experience on the ISS and Mir has shown that many
of the ECLSS systems are very hard to get right and remain reliable over a long
period of time when operated in 0g.
Therefore, the space station is far more relevant to a trip to mars than some PR
stunt in a weekend trip to the moon.
And the landing, takeoff, as well as habitat on mars would be very different
than on the moon, especially if there is the expectation that such an expedition
will draw from Martian atmosphere/ground for water, O2 and fuel for the return
trip (at least to get back to mars orbit to redock with the expedition ship. |
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| Jeff Findley |
Posted: Thu Mar 08, 2007 4:20 pm |
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"John Doe" <jdoe@doe.org> wrote in message
news:cdeaf$45f0691c$cef8887a$10257@TEKSAVVY.COM...
Quote: Jeff Findley wrote:
Sort of. LEO makes a lot of things easier due to the lack of gravity,
but in some ways it's a hindrance.
Unless NASA buys the Starfleet warp drive designs from Paramount Pictures,
it will still take a large number of months to get to and from Mars. And
much of that time will be spent in 0g. Experience on the ISS and Mir has
shown that many of the ECLSS systems are very hard to get right and remain
reliable over a long period of time when operated in 0g.
Mostly this has to do with the low reliability of the Elektron O2 generation
system. At this point, it's unclear if US O2 generator will be more
reliable. The low tech way out is just to launch with enough O2 for the
entire mission instead of trying to make it from waste water.
From a NASA web page, "A man needs 0.63 kg of oxygen per day". Say this is
a three year mission, so that's only about 700 kg of oxygen per person for
the entire mission. Throw on a factor of safety and you can round that up
to maybe 1000 kg of oxygen per person. You'll have to add some mass to that
for tanks and possibly radiators (assuming its stored as LOX), but still, it
doesn't seem to be orders of magnitude heavier than a few Elektrons (for
redundancy) and a boat load of spare parts to keep them going.
Jeff
--
"They that can give up essential liberty to obtain a
little temporary safety deserve neither liberty nor
safety"
- B. Franklin, Bartlett's Familiar Quotations (1919) |
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| Herb Schaltegger |
Posted: Thu Mar 08, 2007 5:24 pm |
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On Thu, 8 Mar 2007 14:20:07 -0600, Jeff Findley wrote
(in article <5513d$45f06ff7$927a2cda$22724@FUSE.NET>):
Quote: Mostly this has to do with the low reliability of the Elektron O2 generation
system. At this point, it's unclear if US O2 generator will be more
reliable. The low tech way out is just to launch with enough O2 for the
entire mission instead of trying to make it from waste water.
It should be more reliable but probably won't be. Prototypes were running
weeks and months-long closed-loop in the POST test chamber at MSFC back in
the early 90's, but that was in a 1-g field of course.
One of the benefits to a fully closed-loop ECLSS is making your O2 not just
out of waste water (which would have to be purified), but out of metabolic
H20, of which the human body produces a LOT. A truly reliable O2 generator
would be a boon for missions that are more than just there-and-back
excursions. After all, an outpost on Deimos or an asteroid, or even a
relatively nearby lunar base shouldn't require routine resupply of an element
which would otherwise have to be dumped overboard due to over-abundance (as
waste water).
--
You can run on for a long time,
Sooner or later, God'll cut you down.
~Johnny Cash |
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| Geoffrey |
Posted: Thu Mar 08, 2007 5:52 pm |
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On Mar 7, "Greg D. Moore (Strider)" <mooregr_deleteth1s@greenms.com>
wrote:
"Jorge R. Frank" <jrfr...@ibm-pc.borg> wrote:
Quote: The reasons you cite are all
reasons why Orion *should* *theoretically* be safer. The only way Orion
can *prove* itself safer is via flight record. I don't believe Orion will
ever fly enough to prove that; at NASA's projected flight rates, it won't
hit 58 flights until around 2040 or so.
Of course ultimately new systems have to replace old ones. But I do agree.
And this is one reason why it bothers me we're losing the shuttle. It's
slowly become a mature system, and we're tossing it away for something newer
and shinier.
This is a good point, but one that you don't see much on sci.space.*,
where the analysis seems to usually be that anything paper is better
than anything actually flying. If reliability is the goal, the best
way to get it is to evolve by fixing flaws, not to throw it out and
invent something new. Roughly, there were 25 successful flights
between the first shuttle launch and the first failure, and about 85
flights between this and the second failure; if this trend kept on, by
the technique of fixing flaws after they are revealed, you would
expect roughly 300 flights before the next failure, and reliability
rising asymptotically from there. (Notably, this is the technique
that the Russians use. Soyuz is reliable because it has been used a
lot.)
However, politically, "fix the shuttle and make it better" was a non-
starter. There was no point in even proposing it; the whole point of
the "replace the shuttle" politics was to *replace* the shuttle, not
upgrade it.
Quote: (Personally I'd argue we would have been "better" off treating the shuttle
more like the developmental system it was and simply fly more flights for
the sake of more flights. the focus on "we need a payload" so we can
justify the cost just made things worse. Had we dropped say another billion
a year on the shuttle program just to fly 25-50% more flights and mark them
as pure "development testing" probably would have created a far safer
system.)
====
in a different post,
"Jorge R. Frank" wrote:
Quote: Soyuz has two fatal accidents in 95 flights (1 in 47.5) and four fatalities
in 228[*] person-trips (1 in 57). Soyuz has had 85 safe landings since the
last fatal accident.
The space shuttle has had two fatal accidents in 117 flights (1 in 58.5)
and fourteen fatalities in 698 person-trips (1 in 49.9). It had 87 safe
landings between the 51L and 107 accidents.
Within the wide statistical uncertainty imposed by the small sample sizes,
those numbers are essentially identical
Good analysis.
It's notable-- although nobody ever does seen to note it-- that the
Shuttle is actually the most reliable launch vehicle ever designed, in
that no other vehicle in history ever made twenty-five successful
orbital launches before the first failure, nor, for that matter, 87
launches before a second failure.
--
Geoffrey A. Landis
http://www.sff.net/people/geoffrey.landis |
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| Revision |
Posted: Fri Mar 09, 2007 1:44 am |
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"Derek Lyons"
Quote: I dread another generation learning nothing about a spacecraft
accident except from Mr. Fenyman or his equivalent.
You'd be lucky to have had a seat in one of his classes. Moronic insult
of a Nobel Laueate.
Derek Lyons....
--
Posted via a free Usenet account from http://www.teranews.com |
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| Jorge R. Frank |
Posted: Fri Mar 09, 2007 10:59 pm |
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"Greg D. Moore \(Strider\)" <mooregr_deleteth1s@greenms.com> wrote in
news:KSKHh.7576$PL.5321@newsread4.news.pas.earthlink.net:
Quote: (Personally I'd argue we would have been "better" off treating the
shuttle more like the developmental system it was and simply fly more
flights for the sake of more flights. the focus on "we need a
payload" so we can justify the cost just made things worse. Had we
dropped say another billion a year on the shuttle program just to fly
25-50% more flights and mark them as pure "development testing"
probably would have created a far safer system.)
Sentimentally I'd agree. Realistically, although the shuttle *should* have
been designed and built as a "developmental" system, it was instead
designed and built to be "operational". This is evident all the way down to
program terminology; true developmental systems have "cockpits" and
"instrument bays", not "crew cabins" and "payload bays". Unfortunately, the
shuttle turned out rather too expensive to utilize in a truly developmental
fashion, and has been assigned "operational" missions, of which two remain:
assembling ISS and servicing HST. This will remain a source of conflict
between the program and the recommendations of both accident investigation
boards, unfortunately.
Quote: I dread another Mr. Fenyman interviewing NASA folks who believe Orion
has a 1 in a 100,000 (or better) risk of mission failure based on
sheer hope.
I already shudder when I hear people quote the 1:2000 LOCV risk for Orion
cited in the ESAS report as if it were fact.
--
JRF
Reply-to address spam-proofed - to reply by E-mail,
check "Organization" (I am not assimilated) and
think one step ahead of IBM. |
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| Greg D. Moore (Strider) |
Posted: Sun Mar 11, 2007 10:26 pm |
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"Jorge R. Frank" <jrfrank@ibm-pc.borg> wrote in message
news:Xns98EED5970CDD4jrfrank@216.196.97.131...
Quote:
Sentimentally I'd agree. Realistically, although the shuttle *should* have
been designed and built as a "developmental" system, it was instead
designed and built to be "operational". This is evident all the way down
to
program terminology; true developmental systems have "cockpits" and
"instrument bays", not "crew cabins" and "payload bays". Unfortunately,
the
shuttle turned out rather too expensive to utilize in a truly
developmental
fashion, and has been assigned "operational" missions, of which two
remain:
assembling ISS and servicing HST. This will remain a source of conflict
between the program and the recommendations of both accident investigation
boards, unfortunately.
Ayup. It's so easy to look back on what we "should have done".
Heck, it amazes me just some of the instrumentation being flown on the
shuttle since Columbia to collect data (like the cameras).
Some of this strikes me as stuff that should have been done from day one.
Now how many flights before Orion gets called "operational"?
Quote:
I dread another Mr. Fenyman interviewing NASA folks who believe Orion
has a 1 in a 100,000 (or better) risk of mission failure based on
sheer hope.
I already shudder when I hear people quote the 1:2000 LOCV risk for Orion
cited in the ESAS report as if it were fact.
Ayup. I'd be highly surprised if a) we get anywhere near 1/10th that
number of flights and if we don't either have a LOCV during that time or
come REAL close.
Watching FTETTM episode Spider, I was reminded of what a huge risk Apollo 8
had been. Just imagine if the LOX tank on that flight had failed.
(oh gawd, ok.. who's responsible for this quote on Wikipedia...
http://en.wikipedia.org/wiki/From_the_Earth_to_the_Moon_%28TV_series%29
"That's All There Is - The story of Lunar Module Pilot Alan Bean and his
experiences on the Apollo 12 mission. The episode is a humorous depiction of
the most tight-knit crew to serve on an Apollo mission. On virtually all
online usenet and internet episode popularity polls, such as ones conducted
by Pat Flannery shortly after the series ended, this episode is consistently
ranked as the best of the series."
Umm Pat?
Quote:
--
JRF
Reply-to address spam-proofed - to reply by E-mail,
check "Organization" (I am not assimilated) and
think one step ahead of IBM.
--
Greg Moore
SQL Server DBA Consulting
Email: sql (at) greenms.com http://www.greenms.com |
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| Derek Lyons |
Posted: Sun Mar 18, 2007 10:48 pm |
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"Revision" <ttsremove@nojunkr.net> wrote:
Quote: "Derek Lyons"
I dread another generation learning nothing about a spacecraft
accident except from Mr. Fenyman or his equivalent.
You'd be lucky to have had a seat in one of his classes.
Very true - but having nothing whatsoever to do with the discussion at
hand.
Quote: Moronic insult of a Nobel Laueate.
Nope, a simple statement of fact.
D.
--
Touch-twice life. Eat. Drink. Laugh.
-Resolved: To be more temperate in my postings.
Oct 5th, 2004 JDL |
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