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Posted by Jose Pina Coelho on August 28, 2005, 3:35 pm
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> It is only fair since the shuttle puts a "drag" on ISS while attached.
I find it hard to beleive that the shuttle has more drag than the ISS
(unless the docking positions is belly forward).
--
Doing AIX support was the most monty-pythonesque
activity available at the time.
Eagerly awaiting my thin chocolat mint.
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Posted by Herb Schaltegger on August 28, 2005, 12:16 pm
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On Sun, 28 Aug 2005 10:35:31 -0500, Jose Pina Coelho wrote
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>
>> It is only fair since the shuttle puts a "drag" on ISS while attached.
>
> I find it hard to beleive that the shuttle has more drag than the ISS
> (unless the docking positions is belly forward).
>
>
>
That's not what Lynndel said. He said it adds drag, not that is has
MORE drag than the station.
--
"Fame may be fleeting but obscurity is forever." ~Anonymous
"I believe as little as possible and know as much as I can."
~Todd Stuart Phillips
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<www.angryherb.net>
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Posted by Jorge R. Frank on September 2, 2005, 5:12 pm
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> On Sun, 28 Aug 2005 10:35:31 -0500, Jose Pina Coelho wrote
>
>>
>>> It is only fair since the shuttle puts a "drag" on ISS while attached.
>>
>> I find it hard to beleive that the shuttle has more drag than the ISS
>> (unless the docking positions is belly forward).
>
> That's not what Lynndel said. He said it adds drag, not that is has
> MORE drag than the station.
And even that was wrong. The station had a ballistic number of 156.80 kg/m^
2 before the shuttle docked, and 163.31 kg/m^2 while it was docked. Lower
ballistic number means more "fluffy" hence more drag, so the shuttle
actually *reduced* the drag deceleration on the station while it was
docked.
--
JRF
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Posted by Ian Stirling on August 20, 2005, 5:04 pm
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> Space station gets free boost from shuttle
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<snip>
I should have asked this at the time.
When I was watching NASA-TV, I noted that the russians were unhappy
if the shuttle pushed the station more than 1m/s or so, WRT the next
progress.
Why is this?
Is there that little margin in the progress engines?
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Posted by John Doe on August 20, 2005, 4:34 pm
Please log in for more thread options Ian Stirling wrote:
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> When I was watching NASA-TV, I noted that the russians were unhappy
> if the shuttle pushed the station more than 1m/s or so, WRT the next
> progress.
> Why is this?
> Is there that little margin in the progress engines?
Progress has to carry as much cargo as it can. The higher the station,
the less cargo it can carry because they have to load more fuel. And
with shuttle gone for the foreseable future, Progress has to be loaded
to the brim with cargo. The next progress is in september so station
will still be "high" because the reboost was weeks late due to Discovery
launching late.
One can argue however that if progress has to spend more fuel to get to
the higher station, it will be spending less fuel to reboost the station
since the station will stayup a bit higher, so having less fuel when it
docks may not make that big a difference.
My guess is that it simply reduces margins, and they probably prefer to
have progress docked with more fuel for emergency manoeuvers to avoid
objects etc.
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