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RTLS Abort

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albegasct@yahoo.com - 18 May 2006 15:14 GMT
In the event of an RTLS abort, are there shut off values on the
umbilical lines to prevent remainning fuel to leak out of the tank once
the orbiter separates? I could see leaking fuel being a danger at that
moment, not to mention pollution in the water. Also, when the tank hits
the water, would it remain intact or break apart?

Thanks.
Bob Haller - 18 May 2006 16:09 GMT
tank will disengrate, good news it fuels are hydrogen and oxygen so it
doesnt matter...
Jeff Findley - 18 May 2006 16:19 GMT
> In the event of an RTLS abort, are there shut off values on the
> umbilical lines to prevent remainning fuel to leak out of the tank once
> the orbiter separates? I could see leaking fuel being a danger at that
> moment, not to mention pollution in the water.

What pollution?  The ET contains cryogenic iquid oxygen and cryogenic liquid
hydrogen.

> Also, when the tank hits
> the water, would it remain intact or break apart?

I'd think it would be squashed a bit on impact.  ;-)

Seriously though, I think if you're performing an RTLS, you end up burning
most (all?) of the fuel in the ET in order to do the powered turn around
maneuver, but there are others here that know better than I.

Jeff
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   "They that can give up essential liberty to obtain a
    little temporary safety deserve neither liberty nor
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albegasct@yahoo.com - 18 May 2006 17:04 GMT
> > In the event of an RTLS abort, are there shut off values on the
> > umbilical lines to prevent remainning fuel to leak out of the tank once
[quoted text clipped - 19 lines]
>      safety"
> - B. Franklin, Bartlett's Familiar Quotations (1919)

Stupid me...what happens to super-chilled liquid hydrogen and oxygen
when it warms up. Duh! I do wonder how long after SRB SEP that the
shuttle stays with the tank. Maybe most of the fuel is indeed burned
off?
Bob Haller - 18 May 2006 17:08 GMT
the srbs cant seperate till they burn out, at just over 2 minutes
albegasct@yahoo.com - 18 May 2006 17:23 GMT
I'm aware of that. My question was how long after that separation does
the orbiter stay with the tank during an RTLS abort.
Mike Ross - 18 May 2006 18:40 GMT
> I'm aware of that. My question was how long after that separation does
> the orbiter stay with the tank during an RTLS abort.

I think during RTLS the Orbiter takes about 20 minutes after shedding the
SRBs to get turned around and headed back, and that burns off most of the
fuel.

Mike Ross
Brian Thorn - 18 May 2006 19:05 GMT
>I'm aware of that. My question was how long after that separation does
>the orbiter stay with the tank during an RTLS abort.

How long the Orbiter stays on the Tank depends on when the RTLS Abort
order is given. They'll burn the SSMEs until ET depletion, which means
at least 8 minutes of powered flight, longer if an engine-out is the
reason for the RTLS. So the actual RTLS flight profile will be
designed to get to ET depletion at the same time the Shuttle achieves
the necessary velocity to get back to KSC, and that depends on vehicle
weight, launch azimuth, etc.

By the way, a lot of that SSME burning will be into the velocity
vector, slowing the Shuttle's downrange progress and eventually
reaching a zero velocity point before the Shuttle starts accellerating
back to KSC. It would be, shall we say, very exciting.

Brian
Bob Haller - 18 May 2006 20:42 GMT
how many really think its survivable?
Chris Bennetts - 19 May 2006 00:01 GMT
> how many really think its survivable?

Who cares, as long as its better than the alternative.

--Chris
Bob Haller - 19 May 2006 01:39 GMT
doesnt matter if the crew dies anyway............

probably another feel good safety measure thats known as not
effective...
Burnham Treezdown - 18 May 2006 20:59 GMT
>>I'm aware of that. My question was how long after that separation does
>>the orbiter stay with the tank during an RTLS abort.
[quoted text clipped - 11 lines]
>reaching a zero velocity point before the Shuttle starts accellerating
>back to KSC. It would be, shall we say, very exciting.

Nobody really believes it will work, do they? But they have to do SOMETHING...
Jorge R. Frank - 19 May 2006 00:37 GMT
> Nobody really believes it will work, do they? But they have to do
> SOMETHING...

Many people do in fact think it will work, though it's risky enough that
it's not worth risking an orbiter and crew just to test it.

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Craig Fink - 19 May 2006 14:29 GMT
>> Nobody really believes it will work, do they? But they have to do
>> SOMETHING...
>
> Many people do in fact think it will work, though it's risky enough that
> it's not worth risking an orbiter and crew just to test it.

I'm one of those people. If they every have to do one, it will be one
exciting ride.
Mika Takala - 21 May 2006 10:32 GMT
>>> Nobody really believes it will work, do they? But they have to do
>>> SOMETHING...
[quoted text clipped - 4 lines]
> I'm one of those people. If they every have to do one, it will be one
> exciting ride.

..and exciting to see too. Lets hope it doesn't happen.

I'm secrectly hoping for a realistic 3D animation / CGI graphics from the
vantage point of a cape tracking camera to see how it would look like on
NASA TV, though.

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Mika Takala

Skylon - 21 May 2006 22:35 GMT
> >>> Nobody really believes it will work, do they? But they have to do
> >>> SOMETHING...
[quoted text clipped - 13 lines]
> --
> Mika Takala

I'd imagine the crew runs through the scenario in simulations...any
word how they typically do?

-A.L.
Jorge R. Frank - 22 May 2006 07:48 GMT
>> >>> Nobody really believes it will work, do they? But they have to do
>> >>> SOMETHING...
[quoted text clipped - 14 lines]
> I'd imagine the crew runs through the scenario in simulations...any
> word how they typically do?

They almost always survive. The few times they don't, it's usually because
the training team threw in extra malfunctions that combined with the RTLS
in ways the crew and/or flight control team failed to anticipate.

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Dale - 22 May 2006 13:34 GMT
>> I'd imagine the crew runs through the scenario in simulations...any
>> word how they typically do?
>
>They almost always survive. The few times they don't, it's usually because
>the training team threw in extra malfunctions that combined with the RTLS
>in ways the crew and/or flight control team failed to anticipate.

Are any simulations regularly run in which the odds of survival aren't so good?
Seems like that would be pretty demoralizing, but if there is a way to increase
their chances through simulations...

Dale
Jorge R. Frank - 23 May 2006 13:45 GMT
>>> I'd imagine the crew runs through the scenario in simulations...any
>>> word how they typically do?
[quoted text clipped - 7 lines]
> so good? Seems like that would be pretty demoralizing, but if there is
> a way to increase their chances through simulations...

Integrated sims are always scripted with at least one way out. They can
still end badly if the simulator misbehaves, if the script scenario turns
out to be unsurvivable because a novice training team fails to recognize
all the interactions between the malfunctions in the script, or if the crew
or flight control team fails to see a solution or otherwise makes an error.
So the "odds of survival" of a given sim depend to a large extent on the
skill level of the crew and flight control team.

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Brian Thorn - 19 May 2006 00:56 GMT
>>By the way, a lot of that SSME burning will be into the velocity
>>vector, slowing the Shuttle's downrange progress and eventually
>>reaching a zero velocity point before the Shuttle starts accellerating
>>back to KSC. It would be, shall we say, very exciting.

>Nobody really believes it will work, do they? But they have to do SOMETHING...

Would you rather face certain death, or possible death?

Brian
Joe Delphi - 19 May 2006 02:01 GMT
> Nobody really believes it will work, do they? But they have to do SOMETHING...

Its sort of like ejecting from a military aircraft where its your last
desperate chance to maybe live but your quality of life might not be 100%.
I remember Navy pilots use to refer to it as committing suicide to prevent
being killed.

JD
Jorge R. Frank - 19 May 2006 00:36 GMT
> Stupid me...what happens to super-chilled liquid hydrogen and oxygen
> when it warms up. Duh! I do wonder how long after SRB SEP that the
> shuttle stays with the tank. Maybe most of the fuel is indeed burned
> off?

Yes, the goal is to burn almost all of it off so that the tank is near
empty at ET sep. ET sep for RTLS occurs at lower altitude than nominal and
propellant slosh would create some very unfavorable dynamics.

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