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Derek Lyons
Posted: Wed Mar 07, 2007 12:04 pm
Guest
"Jorge R. Frank" <jrfrank@ibm-pc.borg> wrote:

Quote:
2) All spacecraft have design flaws; unlike aviation, we have not gone
through enough design generations to weed them out. The staleness of the
current US experience base due to the long gap between design generations
increases the likelihood of a flaw in Orion.

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.

The brutal fact is that we only avoided losing more crews by sheer
good luck and the extremely limited number of flights. The
'experience base' and 'design generations' are non issues - because
niether existed then or now.

[1] In the sense that experience with one had only an extremely
limited 'feed forward' to the next.

D.
--
Touch-twice life. Eat. Drink. Laugh.

-Resolved: To be more temperate in my postings.
Oct 5th, 2004 JDL
Derek Lyons
Posted: Wed Mar 07, 2007 12:06 pm
Guest
"Danny Deger" <dannydeger@hotmail.com> wrote:

Quote:
Is Orion to the moon a good "practice" mission for a trip to Mars?

No.

D.
--
Touch-twice life. Eat. Drink. Laugh.

-Resolved: To be more temperate in my postings.
Oct 5th, 2004 JDL
ed kyle
Posted: Wed Mar 07, 2007 12:12 pm
Guest
On Mar 7, 8:42 am, "Jorge R. Frank" <jrfr...@ibm-pc.borg> wrote:
Quote:
"ed kyle" <edkyl...@hotmail.com> wrote innews:1173244154.705840.40180@j27g2000cwj.googlegroups.com:

On Mar 6, 10:24 pm, "Jorge R. Frank" <jrfr...@ibm-pc.borg> wrote:
"ed kyle" <edkyl...@hotmail.com> wrote
innews:1173240759.534853.186140@c51g2000cwc.googlegroups.com:

But it will fly. When it does, I think that it has a very good
chance
of proving to be the safest human launch system ever fielded.

I think Orion's chances of flying over fifty flights in its entire
operational lifetime are low, but assuming it does, its chances of
getting through its first 58 flights without a fatal accident (which
is what it will need just to match the shuttle's safety record,
currently the best of any manned spacecraft) are even lower.

What makes you think that?

Several reasons. I've been thinking about it overnight to try to rank
them and right now this is the best I have:

1) Human error is the cause of 80% of aviation accidents and this pattern
is continuing in spaceflight. Out of five fatal accidents (Apollo 1,
Soyuz 1 and 11, STS-51L and 107), human error was a primary cause of all
but Soyuz 11. .... There is no reason to believe that Orion will be
immune to this.

2) All spacecraft have design flaws; ... And Orion already has one
obvious flaw, common to all current and historical capsules: the
necessity of jettisoning critical parts of the spacecraft during the
window between deorbit and entry interface. ....

3) Orion's projected flight rate is so low that I believe reusability
will prove to be non-viable. That means a big hit to component
reliability since Orion's systems will never get out of the "infant
mortality" part of the "bathtub curve."

I attribute at least some of the failures you mentioned
(the U.S. failures especially) to design flaws.

It is true that Orion won't be immune to any type of
failure, but I believe that it has a good chance of
being measurably safer than Shuttle and Soyuz and
Shenzhou, for the following reasons.

Orion should be quite a bit safer for crews than shuttle
simply because it will have the launch escape system
that shuttle lacks. It will be at least as safe as shuttle
in the reentry phase, and probably safer because
it will have a smaller, more rugged heat shield less
exposed to damage and will spend less time exposed
to the reentry heating phase. Yes, Orion will have to
jettison its service module, but shuttle has to retract
antennas, close its payload bay doors, start its APUs,
etc. before reentry. Yes Orion will have to deploy
parachutes, but shuttle has to fly to a precision
landing, deploy landing gear, etc.

Orion has a chance to prove safer than Soyuz and
Shenzhou for the following reasons. It will ride what
should be a more reliable launch vehicle than either
Soyuz or Shenzhou. Ares I will have one big solid
motor and one liquid upper stage engine with two
separation events. Both the Soyuz and the CZ-2F
launchers have six propulsion units with six engines
and six separation events. In reentry, Orion will
have fewer modules to jettison than either Soyuz or
Shenzhou.

This is all on paper, of course. Orion should, and
could, prove safer, but the development has a long
way to go. The CEV design was born with safety
as the primary design driver in the immediate wake
of the Columbia disaster. It remains to be seen if
safety will remain paramount during the execution
of the spacecraft's development phase.

- Ed Kyle
ed kyle
Posted: Wed Mar 07, 2007 12:34 pm
Guest
On Mar 7, 10:12 am, "ed kyle" <edkyl...@hotmail.com> wrote:
Quote:
Ares I will have one big solid
motor and one liquid upper stage engine with two
separation events. Both the Soyuz and the CZ-2F
launchers have six propulsion units with six engines
and six separation events.

- Ed Kyle

Addendum: CZ-2F actually has a total of nine main
engines on six propulsion units. Soyuz has six main
engines on six propulsion units, but each engine has
four primary thrust chambers - making a total of 24
main thrust chambers. There are 16 or so smaller
steering thrusters as well.

- Ed Kyle
John Doe
Posted: Wed Mar 07, 2007 12:36 pm
Guest
Danny Deger wrote:
Quote:
I have another question. Is Orion to the moon a good "practice" mission for
a trip to Mars?

It has nothing to do with Mars, except when politicians talk. The space station
has a hell of a lot more to do with a trip to mars than some glorified telephone
booth barely big enough to hold a few people for a dozen days.

A real mission to mars will have to involve first either a shuttle (current or
new), or development of robotics and guidance systems to allow remote assembly
of mars expedition ship components in LEO.

Where the CEV might be of use in in ferrying people to/from the space station
and/or the mars expedition assembly site.
Herb Schaltegger
Posted: Wed Mar 07, 2007 12:37 pm
Guest
On Wed, 7 Mar 2007 08:42:50 -0600, Jorge R. Frank wrote
(in article <Xns98EC58A4DD032jrfrank@216.196.97.131>):

Quote:

2) All spacecraft have design flaws; unlike aviation, we have not gone
through enough design generations to weed them out

I would argue strongly that design flaws still exist in just about every
aircraft ever built and flown. They just haven't all bitten anyone on the
ass yet.

--
You can run on for a long time,
Sooner or later, God'll cut you down.
~Johnny Cash
Jan Vorbrüggen
Posted: Wed Mar 07, 2007 1:06 pm
Guest
Quote:
I would argue strongly that design flaws still exist in just about every
aircraft ever built and flown. They just haven't all bitten anyone on the
ass yet.

Indeed. What was that thing about the 737's elevator going hard over in
certain environmental conditions, first "noticed" after several decades of use
of several thousand planes?

Jan
Brian Thorn
Posted: Wed Mar 07, 2007 2:08 pm
Guest
On Wed, 07 Mar 2007 08:25:08 -0600, "Jorge R. Frank"
<jrfrank@ibm-pc.borg> 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.

[*] - this is the only number I'm not certain of - it may be 225 but I
don't have my spreadsheet handy.

It's 228.

Brian
Brian Thorn
Posted: Wed Mar 07, 2007 2:12 pm
Guest
On Wed, 07 Mar 2007 16:58:37 +0100, Jochem Huhmann <joh@gmx.net>
wrote:

Quote:
Because one major difference between Soyuz and STS is the fact that a
launch failure with STS almost surely means loss of the crew, while this
is not neccessarily the case with Soyuz.

Not really. Loss of one engine on the Shuttle means bail-out, RTLS
abort, TAL abort, Abort Once Around, or perhaps a nominal mission,
depending on when it happens. Loss of one engine on Soyuz means a
high-risk, high-g abort on the escape tower.

Brian
Brian Thorn
Posted: Wed Mar 07, 2007 2:18 pm
Guest
On Wed, 7 Mar 2007 06:49:14 -0600, "Danny Deger"
<dannydeger@hotmail.com> wrote:


Quote:
I have another question. Is Orion to the moon a good "practice" mission for
a trip to Mars?

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.

More importantly, though, Orion gets our foot in the door. "Back to
the Moon" is less scary to politicians than "Go to Mars" would be both
in costs and in risk. When (if) NASA proves it can handle deep space
again with Orion lunar missions, it will be that much easier to get
Congressional approval for the follow-on Mars program. (Unfortunately,
by going down the Ares path, I don't think NASA's going to prove it
can go to the moon. Those expensive rockets will leave no funding to
do anything else on a reasonable time scale, and in the end Congress
will say, "see, you can't even go to the moon, forget about Mars...)

Brian
Brian Thorn
Posted: Wed Mar 07, 2007 2:38 pm
Guest
On 7 Mar 2007 08:12:53 -0800, "ed kyle" <edkyle99@hotmail.com> wrote:
Quote:
Yes, Orion will have to
jettison its service module, but shuttle has to retract
antennas, close its payload bay doors, start its APUs,
etc. before reentry.

Before re-entry but not before the entry burn. Soyuz is committed
after the burn and *must* seperate cleanly. Shuttle can make sure
everything is good before committing to the burn.

Brian
John Doe
Posted: Wed Mar 07, 2007 3:04 pm
Guest
Brian Thorn wrote:
Quote:
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.

In fact, going to Earth would be better training than going to the moon.
Launching some habitat from KSC and landing it at some designated spot on earth
(rough terrain etc) would be far better training since it would involve
atmospheric re-entry and landing with parachutes etc. If you can do that, then
you can do Mars.

Going on on a couple of camping trips to the moon is just some token
compensation for killing the USA manned space programme. The lack of a true
construction vehicle will ensure that NASA cannot build structures needed to go
to Mars.

Besides, it isn't even a given that this CEV thing will go to the moon, and not
even given that it will actually fly. They've already split the moon mission as
a second step for CEV. And as time progresses, talk of an actual habitable moon
base for permanent use will also vanish since there just won't be any funds for
that.

And without a real cargo vessel, the USA will not be able to replace/upgrade the
ISS, so when the later is ditched into the Pacific, CEV will have nowhere to go.
Danny Deger
Posted: Wed Mar 07, 2007 4:36 pm
Guest
"ed kyle" <edkyle99@hotmail.com> wrote in message
news:1173283973.145899.139360@64g2000cwx.googlegroups.com...

snip

Quote:
Orion should be quite a bit safer for crews than shuttle
simply because it will have the launch escape system
that shuttle lacks. It will be at least as safe as shuttle
in the reentry phase, and probably safer because
it will have a smaller, more rugged heat shield less
exposed to damage and will spend less time exposed
to the reentry heating phase. Yes, Orion will have to
jettison its service module, but shuttle has to retract
antennas, close its payload bay doors, start its APUs,
etc. before reentry. Yes Orion will have to deploy
parachutes, but shuttle has to fly to a precision
landing, deploy landing gear, etc.

And don't forget that a capsule has a good chance of bringing a crew home
alive its entry flight control system fails. This was THE requirement that
took NASA from winged vehicles back to capsules during the Orbital Space
Plane program. The entry without flight control requirement has been
watered down now, but a capsule will give the crew a good shot of surviving
a passive entry.

Danny Deger
Danny Deger
Posted: Wed Mar 07, 2007 4:41 pm
Guest
"Brian Thorn" <bthorn64@cox.net> wrote in message
news:9k1uu29pl3r83n3727i7qg493r6v77napu@4ax.com...
Quote:
On 7 Mar 2007 08:12:53 -0800, "ed kyle" <edkyle99@hotmail.com> wrote:
Yes, Orion will have to
jettison its service module, but shuttle has to retract
antennas, close its payload bay doors, start its APUs,
etc. before reentry.

Before re-entry but not before the entry burn. Soyuz is committed
after the burn and *must* seperate cleanly. Shuttle can make sure
everything is good before committing to the burn.

Brian

Soyuz 5 had a failure to separate and the crew lived. The mount between the
entry and orbit module failed due to heat and the entry capsule brought the
crew back alive. I tried to get a failure to separate requirement into the
system, but I was shot down. If you make the attachments out of aluminum
and expose them to the airstream, they should fail in time for the entry
capsule to flip around in time. There were also more than one separation
failures in Vostok with no fatalities.

Danny Deger
Greg D. Moore (Strider)
Posted: Wed Mar 07, 2007 5:12 pm
Guest
"Danny Deger" <dannydeger@hotmail.com> wrote in message
news:45ef2259$0$16964$4c368faf@roadrunner.com...
Quote:

"ed kyle" <edkyle99@hotmail.com> wrote in message
news:1173283973.145899.139360@64g2000cwx.googlegroups.com...

snip

Orion should be quite a bit safer for crews than shuttle
simply because it will have the launch escape system
that shuttle lacks. It will be at least as safe as shuttle
in the reentry phase, and probably safer because
it will have a smaller, more rugged heat shield less
exposed to damage and will spend less time exposed
to the reentry heating phase. Yes, Orion will have to
jettison its service module, but shuttle has to retract
antennas, close its payload bay doors, start its APUs,
etc. before reentry. Yes Orion will have to deploy
parachutes, but shuttle has to fly to a precision
landing, deploy landing gear, etc.

And don't forget that a capsule has a good chance of bringing a crew home
alive its entry flight control system fails. This was THE requirement
that took NASA from winged vehicles back to capsules during the Orbital
Space Plane program. The entry without flight control requirement has
been watered down now, but a capsule will give the crew a good shot of
surviving a passive entry.

Right up until the parachute fails to open.

Or the de-orbit burn fails.

ultimately there are no truly passive systems. Just different re-entry
failures.


Quote:

Danny Deger



--
Greg Moore
SQL Server DBA Consulting
sql (at) greenms.com http://www.greenms.com
 
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