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STS-113 Space Shuttle Processing Q & A
Before
the KSC Direct! webcast of the STS-113 launch, space enthusiasts from
all over the world submitted questions for our Shuttle expert, Shawn Greenwell.
The questions were answered during the show. In case you missed the webcast,
or would like to review each of the questions and answers, we have provided
the STS-113 Space Shuttle Processing Q&A in its entirety below.
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J.Maki
from Japan,Niihama
When I was watching NASA-TV broadcasting Soyuz docking with
ISS, I wondered what language do they use on the ISS? Can Russian
cosmonauts speak English? |
|
And I think the overall answer is that they use both languages,
English and Russian. Certainly when they're orbiting the Earth
they have the opportunity to talk to mission controllers in
Houston and they have the opportunity to talk to some folks
in Moscow as well. If the Russians are communicating, more often
they're talking in Russian, it's more comfortable for them.
If they're talking to the JSC folks, they're speaking in English.
I know from talking to some of the Russians that they do speak
English, and I know that our astronauts also take Russian lessons,
so I think they're probably equally versed in both languages.
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Mark
from Chicago
How does the orbiter get mounted on the flatbed orbiter transporter,
and how long does it take to do this? |
| When
we have the orbiter inside the OPF (Orbiter Processing Facility),
it's essentially jacked down, on its own wheels and tires. When
it's time to finish up processing and transfer the orbiter over
to the Vehicle Assembly Building (VAB), we jack it up using
some floor jacks inside the OPF, and then the orbiter transporter
is brought underneath the orbiter, and then the floor jacks
are gently let down to allow the orbiter to interface with three
points (ONSIDE THE OTS). And at that point, the main landing
gear are retracted and essentially the orbiter is ready to roll
over to the VAB. We do this because we used to roll the orbiter
over on its own main landing gear tires, but we found out if
we rolled it from the OPF to the VAB, we were picking up a lot
of debris on the main landing gear tires. We had the orbiter
transporters that were out in California and they became available
to us so we decided it would be a better idea if when we were
in the OPF, we took the main landing gear up for flight and
rolled over and were ready to go by the time the orbiter got
into the VAB. |
Scott
from Melbourne
Why does it take so long to get Shuttles ready for a launch? |
| It
takes a long time, Scott, because of all the things we're doing
to try and make sure that the Shuttle is ready to go support
the next flight. Although there are a lot of redundant systems
on the orbiter, we really don't like to get on orbit and then
have to take advantage of that redundancy. So we try to make
sure that the orbiter is the best it can be. So all the systems
- the SSMEs (Space Shuttle Main Engines) are changed out, the
orbiter mechanisms for up in the payload bay, the ET doors,
all the ECS Systems (Environmental Control Systems) that provide
cooling and air for the astronauts and crew, all the data processing
systems... they're all thoroughly checked out before flight.
One of the things that also is a real time-consuming thing for
Shuttle processing is a need to change payloads. Because the
orbiter is so flexible, and we can fly multiple types of payloads.
One mission you may be flying a deployable payload and in the
next mission it's possible that you're flying a payload that
you're bringing back. So you need to reconfigure the payload
bay. So really the flexibility of the system unfortunately adds
to the time of getting it turned around. |
Miguel
from Madrid
What is MECO? Thank you very much. |
| Well
Miguel, MECO is an acronym - you probably know that NASA is
really big into using acronyms - and MECO is an acronym for
Main Engine Cutoff. And what it actually signifies, what it
means, is when the orbiter is going through ascent, and we've
used all the liquid hydrogen and liquid oxygen inside of the
External Tank, or used enough to get us to where we need to
be in the ascent profile, the engines are shut down and the
MECO call from Houston signifies that the main engines are cut
off and it signals to the crew that the main engines are done
for flight. |
Emilio
Pérez from Lugo-Spain
When the Shuttle blasts off, why do you transfer the Shuttle
control to the Mission Control Center (Houston)? |
| Emilio,
the answer to that question is that the two centers, KSC (Kennedy
Space Center) and JSC (Johnson Space Center), really have different
missions. The mission of the Kennedy Space Center is to get
the orbiters, SRBs (Solid Rocket Boosters) and ETs (External
Tanks) ready for flight. And the mission of JSC is really to
train the crew and to help the crew to manage the on-orbit operations.
So KSC is really managing the countdown up until T-0 time, and
after T-0 time, the JSC folks take over control and manage the
flight operations. That role reverses as soon as we land and
the orbiter comes to a stop and the crew is actually exiting
the vehicle. JSC gives command and control of the vehicle back
to to the KSC folks. |
Emilio Pérez from Lugo-Spain
Why will mission sts-113 blast off to an altitude about 122
nautical miles, when the ISS is in orbit about 400 kilometers? |
| Okay!
The answer to that is actually complicated in a lot more than
I can actually go into, or am prepared to go into. But the short
answer is because the orbiter has to catch up to the Space Station
and the Space Station is in a fixed orbit around the Earth.
The way we do that is we either have to move faster or slower
in order to catch up to the Space Station. Going in a lower
orbit allows you to circumnavigate the Earth quicker so you're
actually closing the gap to the Space Station. After T-0 they
don't actually dock until launch plus three days or launch plus
four days. It's just a matter of where the dynamics work in
and what time we launched inside the launch window and how quickly
we can get to the Space Station. It's a matter of trying to
work out the dynamics on orbit to get to the Space Station when
you want to. |
Cleteus
from Bithlo
How long does it take the shuttle to orbit
the Earth once? |
|
It takes approximately 90 minutes for the orbiter to go
around the Earth one time, moving at 17,500 miles per hour. |
Jon
from Jacksonville
What is the purpose of the orange "bars" we sometimes
see attached to the payload bay doors of the Shuttle on the
pad or in transit to the pad? |
| I
think you're probably talking about the torque tubes we install
once we get the vehicle out to the pad. The payload bay doors
are fairly delicate and they don't support operations in 1-G
real well. So when we get to the pad we install what we call
torque tubes on the outside of the payload bay doors, and the
torque tubes allow the payload bay doors to stay rigid so that
when we do payload bay door opening and closing after we put
a payload in, we can maintain the integrity of the payload bay
doors and not have to worry about damaging the doors. For horizontal
operations, we actually have a STRONGVEX we install, now because
the orientation of the orbiter has changed from being horizontal
to vertical at the pad, when we're horizontal, we use a set
of STRONG BACKs. They're a lot like the torque tubes, they're
just a little bit thicker. And then we have a zero-G system
that's installed in all the OPFs. So whenever we're opening
and closing payload bay doors, we have a large set of counterweights
that we have installed, so the doors physically go through about
the same loads on Earth in 1-G that they actually always go
through on orbit in zero-G. |
nate
from florence
I was wondering what the time frame is for post landing processing
of the orbiter before heading back for "overhaul"?
For example, purging of lines of any gases, post flight checks
of motors, etc. Thanks, a curious jet mechanic. |
| Nate,
your question is a little interesting because you have to answer
it probably two different ways. If we're talking about what
we do after landing in order to get the orbiter back to the
OPF, from what we're hooking up for purge, and how we're making
sure the lines are clear before we get into the OPF. It only
takes about 3 and a half hours from wheel stop, and depending
on the payload you have, the nominal Space Station payloads
take about 3 and a half hours to download the extra science
that we have onboard, and get the orbiters turned around into
the OPF. Now if you're talking about when we're in the OPF and
how long it takes us to get the orbiter processed to get ready
to fly again, that can be a matter of months. |
orion
from ninrveh
What are some of the activities that take place during turnaround,
and can you give me a thorough explanation of the activities? |
| i
can certainly give you a taste of what some of the activities
are. Certainly when we get back to the OPF we need to take care
of the main engines and the main engines are changed out because
they have to go back for some fairly detailed inspection at
the main engine shop here at Kennedy Space Center. So the engines
are one of the items that we take all three of the engines off,
and we normally have another set of engines that are ready to
get installed again. We also do checkout, as I mentioned before
our (BODY) orbiter components like the orbiter payload bay doors,
the ET doors are checked out, the wheels and tires are inspected
and the main landing gear tires are changed out and those landing
gear tires if they're acceptable are flown again. All the DPS
folks that handle data processing on the orbiter have checkouts
to go do, the folks that manage the OMS RCS system (Orbital
Maneuvering System - Reaction Control System) have to check
out those systems, so every individual system component on the
orbiter gets a thorough checkout before launch. |
Jeremy
Hartings from New Orleans, LA
What are the windows in the space shuttle
made out of? |
| The
windows on the Space Shuttle are actually made out of aluminum
silicate glass and fused silica glass. The orbiter windows are
actually three different panes, there's an interior pressure
pane because the pressure inside the orbiter is a lot higher
than it is in the vacuum of space. We also have an optical pane
that's installed in the middle that's about three and a half
inches thick and on the outside, there's a thermal pane that
protects the inside of the cockpit from the high heats of ascent
and reentry. There are six forward-looking windows, three on
the CDR (Commander) side and three on the PLT (Pilot) side.
There are two overhead windows that the crew out of especially
when docking to the Space Station they're using those windows
to watch the orbiter approach the Space Station. And then there
are two windows on the aft that look into the payload bay, and
depending on our hatch configuration on the inside, there can
be anywhere from one to two additional windows, they're small
holes that are installed inside the hatches so you can look
through hatch windows. And the side hatch, the emergency egress
hatch, has a small hatch window as well. They're all made of
the same materials. The forward windows - the ones that the
crew actually uses for ascent and entry - are the ones we have
to take really good care of in order to maintain the optical
quality of them. |
James
from Millersport
What kind of fuel is used in the RCS and OMS Systems? |
| The
RCS and OMS systems use monomethyl hydrazine and nitrogen tetroxide.
It's a system that doesn't require oxygen to be combustible,
so that you can mix those two components in the proper ratios
and end up being able to maneuver the orbiter on orbit. |
Julia
from Canberra
What materials are used to protect shuttles
during re-entry? |
|
Julia, we use a number of different
materials to protect the orbiter from re-entry heat, and for
ascent heating as well. If you look at the nose cap of the orbiter,
the very front of the orbiter, and what coating is on the wings,
it's a reinforced carbon-carbon material. If you looked on the
bottom of the orbiter it's covered with black tiles which are
actually a silicate made of glass, and if you looked on the
top of the wings we actually have a few silica blankets and
those cover the payload bay doors as well. So depending on what
area of the orbiter we're trying to protect, and what temperatures
that area of the orbiter is exposed to, we have a certain prescribed
type of thermal protection system that we keep applied to those
areas. |
Jeff
from Hopkinsville
The tiles and thermal blankets are glued to the orbiter, right?
The glue used has to be really strong to stand up to the aero
pressures that are put on the vehicle during flight. So how
do you remove a damaged tile or thermal blanket when it is damaged
and must be replaced? |
| Well
Jeff, if we come back from orbit or from orbiter processing
operations and have to to go in and replace a tile, if it's
one of the hard tile that's on the bottom of the orbiter, one
of the white tile, we normally have to destructively remove
it. You have to use a little pick and begin chipping through
the hard outer coating of the tile and that exposes the very
soft inner portion of the tile and you can just kind of chip
it out of the cavity, and then you've got a strain isolation
pad that the actual tile rides on, since it doesn't interface
directly with the orbiter, metal structure, and you can just
scrape that off with a non-metallic scraper. And if we're talking
about one of the blankets installed on the wing or up on top
of the payload bay doors, it's a simple matter of getting a
non-metallic scraper in there and opening up a little hole where
you can start scraping out and just pull back the blanket. And
you just scrape it off and prepare the surface and you're ready
to go bond another tile in place. We have tiles and blankets
because originally when the orbiters came in they had a lot
more tiles, somewhere around 33,000 or 34,000 tiles. Right now
we have about 23,000 tiles. What we did was, through processing,
we realized that there were areas on the orbiter where you could
actually tolerate some lower heat, like on top of the payload
bay doors and up on top of the wings. The blankets cover a larger
area, so there's not so much maintenance associated with them,
and actually they're lighter and easier to work with than the
tile, and they take a lot more abuse than the tiles do as well.
|
Jim
from Grand Junction
What are the actual number of TPS heat
shield tiles used on each orbiter today? |
| About
23,000, and certainly every orbiter differs a little bit, but
it's somewhere around 23,000 tiles. |
Emilio
Pérez from Lugo-Spain
When the Shuttle blasts off, why do you transfer the Shuttle
control to the Mission Control Center (Houston)? |
| The
solid rocket boosters have about 2.6 million pounds of thrust
apiece. They weight about a million pounds in the propellant
side and produce about 2.6 million pounds of thrust. The amount
of thrust actually varies, we're using the solid rocket motors
and you cannot go in and change the propellant in real time,
or you can't turn the thrust up or down in real time, and when
the Thiokol folks in Utah cast the motors for us, they actually
cast the forward grain in a little different shape, it actually
has a star pattern on the inside. So at T-0 when we send the
command for the solid rocket motor igniter to ignite the rest
of the grain, the star pattern enables the solid rocket motors
to burn a little hotter and provide a little more thrust in
the beginning of the countdown and in order to get you off the
pad and then as we're going through ascent, we may want to decrease
the thrust when we're going through Max Q, the grain is also
tailor-made to take that into account. And then as you're going
up the hill it becomes a steady profile and then you just burn
out your propellant and essentially get ready to have SRB separation. |
james
kelley from cananduagia
How long does it take to retrieve the solid rocket boosters
and get them ready for another launch? |
| James,
it takes approximately two days if we're looking at from the
time the boosters enter the water until the time they get back
to Hangar AF. It takes about two days for the two retrieval
ships to go back and retrieve each booster, left-hand and right-hand.
Once they're back to Hangar AF, the boosters are taken out of
the water and put onto modified rail cars and are able to turn
the boosters and they're given a thorough post-flight inspection.
After post-flight inspection is done and everyone is convinced
and ready to give permission to begin separating the segments.
The segments are separated individually at Hangar AF, the forward
skirt is demated and the aft skirt is demated as well, and the
components are shipped out to respective sites. The forward
skirts and the aft skirts stay here where we process them here
at Kennedy Space Cente with a subcontractor, and the actual
solid rocket motor casings for them are sent back Thiokol on
rail cars. Now once they get back, the Thiokol folks have to
clean them, reinspect them and go back and refill the solid
rocket motors. So it can be anywhere from six months to years
before we see that same segment come back to KSC and be ready
for use again. |
John
L from Santa Barbara
What is the life expectency of #1 or #2 crawler? |
| John,
we started using the crawlers in the 1960s. And we've had to
keep using the crawlers, when we went from Apollo to the Shuttle.
And the plan is to keep using the crawlers. We take good care
of them and they're in great shape, and we constantly work to
make them better and make sure that they're supporting all the
way until we move on to the next phase of the program. |
Michelle
from Augusta
How can you achieve more than 100% power
during launch? What is the g force exerted on an astronaut at
launch? |
| Michelle,
the first part of your question is, we get more than 100% thrust
out of the engines when we say we're up at 100% that's at the
thrust at sea level. And as the engines go through the atmosphere
and the atmosphere becomes thinner, the main engines actually
get more efficient, so eventually you can achieve more than
100% thrust because of what you're doing in the ascent profile.
And we actually get to 104% of rated thrust. And for the second
part of your question, the astronauts feel somewhere around
three G's when they're in the ascent profile, and somewhere
around three G's when they're coming back for descent is about
the worst G case that they feel. |
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