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Science Forum Index » Space - Shuttle Forum » In two years time...
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| Brian Thorn |
Posted: Wed Mar 12, 2008 6:19 pm |
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On Wed, 12 Mar 2008 13:12:46 -0400, "Jeff Findley"
<jeff.findley@ugs.nojunk.com> wrote:
Quote: True, but they at least reserved the space for it in the Block I design.
On page 119 and 121 (printed on the page, not what Acrobat says) there are
drawings of the Block I design showing where the docking/transfer tunnel
would go.
There are plenty of early Shuttle drawings showing docking hardware,
too... unsurprising since Shuttle was conceived as a support vehicle
for a Space Station.
Once the basic configuration of the vehicle was settled upon, the
docking apparatus was to be in the forward end of the payload bay
(before that, when Orbiters were straight winged and had other major
design differences, docking ports were all over the place, including
in the nose cone and between the nose and the cockpit, facing
upwards.) But Jenkins' book shows "Vehicle 4 Details Circa November
1973" with essentially the same docking configuration we use today.
The only major difference is that we're using Russian hardware.
Brian |
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| Derek Lyons |
Posted: Wed Mar 12, 2008 6:51 pm |
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"Jorge R. Frank" <jrfrank@ibm-pc.borg> wrote:
Quote: Derek Lyons wrote:
When the work was done is irrelevant - the capability was intended
from the start is my point. Providing those capabilities way delayed,
not added.
It is relevant, because even though the capability was intended from the
start, it was not part of the original vehicle design.
As I said - that appears to depend on what arbitrary point you select
as the 'original vehicle design'. The same general docking method as
used for Shuttle-Mir and more-or-less what is used to today was what I
saw back in the 70's... A docking system mounted in the cargo bay.
Even if it wasn't built until years later, the current system is
consistent with what seems to have been planned from very early on.
Quote: It wound up being upgraded later, in a rather kludgy way that makes no
sense from an overall system perspective but makes perfect sense once you
know that it was grafted on.
It makes perfect sense within the overall Shuttle system - the Shuttle
isn't versatile because what of is built in, but because of what can
be carried.
D.
--
Touch-twice life. Eat. Drink. Laugh.
http://derekl1963.livejournal.com/
-Resolved: To be more temperate in my postings.
Oct 5th, 2004 JDL |
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| Derek Lyons |
Posted: Wed Mar 12, 2008 6:53 pm |
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"Jeff Findley" <jeff.findley@ugs.nojunk.com> wrote:
Quote: Thanks for a great explanation of how a docking is actually flown. I'd
forgotten that the aft station allows the CDR to fly the shuttle.
<AOL>Me too</AOL> I kept thinking 'the CDRs window is in front of the
CDRs seat'.
D.
--
Touch-twice life. Eat. Drink. Laugh.
http://derekl1963.livejournal.com/
-Resolved: To be more temperate in my postings.
Oct 5th, 2004 JDL |
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| Brian Thorn |
Posted: Wed Mar 12, 2008 9:43 pm |
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On Tue, 11 Mar 2008 21:27:31 -0500, "Jorge R. Frank"
<jrfrank@ibm-pc.borg> wrote:
Quote: It is relevant, because even though the capability was intended from the
start, it was not part of the original vehicle design. It wound up being
upgraded later,
Jenkins 3rd Ed., Page 190 shows pretty much today's docking system
(part of the Spacelab tunnel) in the Orbiter proposed in November
1973. This is very soon after the current Orbiter design basics were
settled uponm so it does not appear on the surface to have been an
afterthought. Earlier concepts seem to have the docking adapter in the
nose, but these are also Orbiter concepts that have abort motors and
air-breathing engines. I guess it depends on what your definition of
"original vehicle design" is. I'm not at all sure there was *one*.
Quote: in a rather kludgy way that makes no sense from an
overall system perspective but makes perfect sense once you know that it
was grafted on.
Actually, it makes perfect sense. I suspect this was a design decision
made when the Shuttle had to become an all-purpose launch vehicle and
not just a Station Shuttle. Moving the docking adapter to the cargo
bay meant the Shuttle only needed to carry it on missions that needed
it (Station missions) in turn meaning more payload could be carried on
missions that didn't need to dock (Spysat launches.)
Brian |
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| Brian Thorn |
Posted: Wed Mar 12, 2008 11:08 pm |
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On Wed, 12 Mar 2008 20:05:43 -0700 (PDT), charliexmurphy@yahoo.com
wrote:
Quote: Moving the docking adapter to the cargo
bay meant the Shuttle only needed to carry it on missions that needed
it (Station missions) in turn meaning more payload could be carried on
missions that didn't need to dock (Spysat launches.)
It is not an easy thing to remove and installed. And now, it can't be
removed since it is the only airlock
Yes, but this was 1973, when NASA had deluded itself into thinking the
Shuttle could fly 50 times a year. Realistic processing schedules
weren't exactly the order of the day.
Brian |
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| Derek Lyons |
Posted: Thu Mar 13, 2008 1:21 am |
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Brian Thorn <bthorn64@suddenlink.net> wrote:
Quote: On Wed, 12 Mar 2008 20:05:43 -0700 (PDT), charliexmurphy@yahoo.com
wrote:
Moving the docking adapter to the cargo
bay meant the Shuttle only needed to carry it on missions that needed
it (Station missions) in turn meaning more payload could be carried on
missions that didn't need to dock (Spysat launches.)
It is not an easy thing to remove and installed. And now, it can't be
removed since it is the only airlock
Yes, but this was 1973, when NASA had deluded itself into thinking the
Shuttle could fly 50 times a year. Realistic processing schedules
weren't exactly the order of the day.
The ODS didn't become a 'permanent' part of the orbiter until ISS
construction was well underway. Until it was installed 'permanently',
it could be (and was) changed out as easily as any other payload.
D.
--
Touch-twice life. Eat. Drink. Laugh.
http://derekl1963.livejournal.com/
-Resolved: To be more temperate in my postings.
Oct 5th, 2004 JDL |
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| Guest |
Posted: Thu Mar 13, 2008 2:34 am |
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On Mar 13, 2:21 am, fairwa...@gmail.com (Derek Lyons) wrote:
Quote:
The ODS didn't become a 'permanent' part of the orbiter until ISS
construction was well underway. Until it was installed 'permanently',
it could be (and was) changed out as easily as any other payload.
It was never easy. They tried to schedule the orbiters to allow it to
stay in |
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| Jorge R. Frank |
Posted: Thu Mar 13, 2008 3:14 am |
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Brian Thorn wrote:
Quote: On Tue, 11 Mar 2008 21:27:31 -0500, "Jorge R. Frank"
jrfrank@ibm-pc.borg> wrote:
It is relevant, because even though the capability was intended from the
start, it was not part of the original vehicle design. It wound up being
upgraded later,
Jenkins 3rd Ed., Page 190 shows pretty much today's docking system
(part of the Spacelab tunnel) in the Orbiter proposed in November
1973. This is very soon after the current Orbiter design basics were
settled uponm so it does not appear on the surface to have been an
afterthought. Earlier concepts seem to have the docking adapter in the
nose, but these are also Orbiter concepts that have abort motors and
air-breathing engines. I guess it depends on what your definition of
"original vehicle design" is. I'm not at all sure there was *one*.
in a rather kludgy way that makes no sense from an
overall system perspective but makes perfect sense once you know that it
was grafted on.
Actually, it makes perfect sense. I suspect this was a design decision
made when the Shuttle had to become an all-purpose launch vehicle and
not just a Station Shuttle. Moving the docking adapter to the cargo
bay meant the Shuttle only needed to carry it on missions that needed
it (Station missions) in turn meaning more payload could be carried on
missions that didn't need to dock (Spysat launches.)
OK, I can see by your reply and Derek's that I completely failed to
specify what I was talking about.
I'm not referring to the docking mechanism itself - it was clear even in
the 70's that docking was not going to happen on every flight, so the
docking mechanism would be best done as a "kit" installable in the
payload bay.
What I'm referring to is the docking sensor and associated GNC software.
The sensor (TCS) was first implemented as a payload, and the GNC
software implemented on a laptop computer. That was fine for the initial
rapid-prototyping phase during Shuttle-Mir, but during the "operational"
ISS phase, both should have been fully integrated into the orbiter's
GNC system. The shuttle program's failure to do so has led to
reliability problems, of which today's approach and docking was a
perfect example, for those who were paying close attention. |
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| Jan Vorbrüggen |
Posted: Thu Mar 13, 2008 10:32 am |
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Quote: The shuttle program's failure to do so has led to
reliability problems, of which today's approach and docking was a
perfect example, for those who were paying close attention.
Hmmm, I couldn't pay attention, as I couldn't watch...so what happened?
The laptop crashed in Winwoes at an inopportune moment?
Jan |
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| Jeff Findley |
Posted: Thu Mar 13, 2008 12:49 pm |
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"Derek Lyons" <fairwater@gmail.com> wrote in message
news:47da6cc8.1410989078@news.supernews.com...
Quote: "Jeff Findley" <jeff.findley@ugs.nojunk.com> wrote:
Thanks for a great explanation of how a docking is actually flown. I'd
forgotten that the aft station allows the CDR to fly the shuttle.
AOL>Me too</AOL> I kept thinking 'the CDRs window is in front of the
CDRs seat'.
I wonder if this was covered in the "Space Shuttle Operator's Manual" that I
bought in the early 80's. It's not a great book, but it was good for a
teenager interested in the space shuttle. :-)
Jeff
--
A clever person solves a problem.
A wise person avoids it. -- Einstein |
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| Jorge R. Frank |
Posted: Fri Mar 14, 2008 12:31 am |
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Jeff Findley wrote:
Quote: "Derek Lyons" <fairwater@gmail.com> wrote in message
news:47da6cc8.1410989078@news.supernews.com...
"Jeff Findley" <jeff.findley@ugs.nojunk.com> wrote:
Thanks for a great explanation of how a docking is actually flown. I'd
forgotten that the aft station allows the CDR to fly the shuttle.
AOL>Me too</AOL> I kept thinking 'the CDRs window is in front of the
CDRs seat'.
I wonder if this was covered in the "Space Shuttle Operator's Manual" that I
bought in the early 80's. It's not a great book, but it was good for a
teenager interested in the space shuttle.
Pages 3.2 and 3.3 (yes, I still have my copy...). Unfortunately, that
book came along before the shuttle had ever performed a rendezvous, let
alone a docking, so there are very few operational details, but it does
show a diagram of the aft flight station, including both hand controllers. |
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