Is Shuttle "slipped" into crosswinds?
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George Orwell - 23 Aug 2007 22:46 GMT The old taildraggers were cross-controlled (slipped) in crosswinds. This keeps the upwind wing low and the fuselage aligned straight with the runway on touchdown. After touchdown the stick is advanced towards the upwind wing to help keep it down and avoid the dreaded groundloop.
I believe tricycle gear airplanes can be slipped also, though the slip is not used to steepen the approach; instead, flaps are used. The slip is still used to get it out of a crab, though you have to really mishandle a trike gear plane to groundloop since it tends to self-straighten when the mains touch.
I once asked an airliner pilot if he slipped the 737 because it appears the wing engine might scrape if he did. The answer I got was slipping isn't much needed, but if he did, there isn't much chance of the engine contacting the ground before the wingtip. Does anybody out there fly 737s who can confirm this?
So, the questions is: Is the Shuttle slipped into the wind when on final, just like any other airplane?
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Danny Deger - 23 Aug 2007 23:39 GMT > The old taildraggers were cross-controlled (slipped) in crosswinds. This > keeps the upwind wing low and the fuselage aligned straight with the [quoted text clipped - 25 lines] > Per maggiori informazioni |For more info > https://www.mixmaster.it The shuttle is put into a crab and lands in the crab. It is not slipped. The pilot never touches the rudders while in the air. They are only used for control while on the ground.
Danny Deger
Danny Deger
John - 23 Aug 2007 23:44 GMT > > The old taildraggers were cross-controlled (slipped) in crosswinds. This > > keeps the upwind wing low and the fuselage aligned straight with the [quoted text clipped - 35 lines] > > - Show quoted text - Really . . . the orbiter is a feet on the floor "airplane," like a Piper Cherokee?
I have also heard that the DC-9 is the same, at least with both engines running although that is an unconfirmed memory.
take care . . .
John
Danny Deger - 24 Aug 2007 16:14 GMT snip
> Really . . . the orbiter is a feet on the floor "airplane," like a > Piper Cherokee? Yep, feet on the floor until on the runway. The rudder is moved automatically by the computer to "center the ball".
Danny Deger
> I have also heard that the DC-9 is the same, at least with both > engines running although that is an unconfirmed memory. > > take care . . . > > John MichaelJP - 24 Aug 2007 09:38 GMT >> The old taildraggers were cross-controlled (slipped) in crosswinds. This >> keeps the upwind wing low and the fuselage aligned straight with the [quoted text clipped - 32 lines] > > Danny Deger Interesting you should say that, as the video of the landing showed the shuttle landing on its into-wind left mainwheels just as a light aircraft landing in a forward slip would do. Maybe it's just at the final seconds.
- Michael
John - 23 Aug 2007 23:46 GMT > The old taildraggers were cross-controlled (slipped) in crosswinds. This > keeps the upwind wing low and the fuselage aligned straight with the runway [quoted text clipped - 22 lines] > Per maggiori informazioni |For more info > https://www.mixmaster.it George,
I was re-taught slips when I was getting checked out in sailplanes so approachs could be steepened as well. Not something that would be needed when landing an orbiter.
Take care . . .
John
Brian Gaff - 24 Aug 2007 09:35 GMT I'd have thought that the orbiter was so sluggish that unless a really big gust at a crucial point occured, then it would self straighten at main gear touch. Brian
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>> The old taildraggers were cross-controlled (slipped) in crosswinds. This >> keeps the upwind wing low and the fuselage aligned straight with the [quoted text clipped - 36 lines] > > John Gene Seibel - 24 Aug 2007 18:25 GMT > The old taildraggers were cross-controlled (slipped) in crosswinds. This > keeps the upwind wing low and the fuselage aligned straight with the runway > on touchdown. After touchdown the stick is advanced towards the upwind > wing to help keep it down and avoid the dreaded groundloop. I use a slip, or a crab with a last second transition to a slip in my Cherokee. Of course, the same principles apply to the Shuttle, however with it's much faster landing speed, the crosswind is a much lower percentage of it's forward speed, therefore relatively little correction is needed to get it's alignment close enough to land. And with the main gear so far back, it tends to straighten out very nicely once the gear touches. -- Gene Seibel Hangar 131 - http://pad39a.com/gene/plane.html Because I fly, I envy no one.
dan@tw.com - 26 Aug 2007 18:23 GMT Here's the official line from the Shuttle Ascent, Entry Landing Flight procedure handbook:
b. Crosswind after T/D It is a good practice to consider every landing a crosswind landing. Even when the crosswind component is small, the pilot who is prepared for this makes a more controlled T/D and rollout. T/D is made in a pure crab, with no lateral drift; therefore, the nose is pointed upwind. During rollout, prior to derotation, the vehicle's response to crosswind is to roll and yaw away from the wind. The wings are held level with lateral RHC and lateral drift is held at zero with rudder into the wind as required.
>> The old taildraggers were cross-controlled (slipped) in crosswinds. This >> keeps the upwind wing low and the fuselage aligned straight with the runway [quoted text clipped - 8 lines] >with the main gear so far back, it tends to straighten out very nicely >once the gear touches. Jim in Houston - 26 Aug 2007 18:57 GMT >Here's the official line from the Shuttle Ascent, Entry Landing Flight >procedure handbook: [quoted text clipped - 9 lines] >level with lateral RHC and lateral drift is >held at zero with rudder into the wind as required. I felt sure that the rudder had to be used, as with any slip a rudder is required. I'm just a private pilot but I have never slipped, or heard of a slip without a rudder. A rudder is required to maintain runway heading while aileron is used for lateral movement. At least that's what I thought. Why would the shuttle be equipped with a rudder if the rudder is not used? Jim in Houston.
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Danny Deger - 30 Aug 2007 16:56 GMT >>Here's the official line from the Shuttle Ascent, Entry Landing Flight >>procedure handbook: [quoted text clipped - 16 lines] > that's what I thought. Why would the shuttle be equipped with a rudder > if the rudder is not used? The rudder is used by the autopilot while in the air. The pilot/CDR NEVER touches the rudder while airborn. After landing it is used to maintain alignment on the runway.
Danny Deger
Jim in Houston - 31 Aug 2007 03:09 GMT >"Jim in Houston" <nospamjamesgoodum@sbcglobal.netnospam> wrote in message >> [quoted text clipped - 10 lines] > >Danny Deger Now I get it. I didn't understand how that worked. But... I thought the nose wheel steering was used to maintain alignment on the runway. I remember that prior to nw steering they were using differential braking which often resulted in blown tires. Jim in Houston.
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tdadamemd-spamblock-@excite.com - 31 Aug 2007 08:23 GMT >From Jim in Houston: > On Thu, 30 Aug 2007 10:56:04 -0500, "Danny Deger" [quoted text clipped - 12 lines] > >touches the rudder while airborn. After landing it is used to maintain > >alignment on the runway.
> Now I get it. I didn't understand how that worked. But... I thought > the nose wheel steering was used to maintain alignment on the runway. > I remember that prior to nw steering they were using differential > braking which often resulted in blown tires. Ok, the level of inaccuracy on this thread has just exceeded my threshold for observation only...
Particularly, this notion of the shuttle blowing tires "often". That goes totally against my understanding of the shuttle program history.
And for Danny, I have this point of feedback: the rudder is used even when the autopilot is not engaged!
(And I find it curious that no one has straightened out the inaccuracies that have been posted on that Crosswind DTO thread as well.)
~ CT
Jim in Houston - 31 Aug 2007 10:25 GMT
>> Now I get it. I didn't understand how that worked. But... I thought >> the nose wheel steering was used to maintain alignment on the runway. [quoted text clipped - 15 lines] > >~ CT I probably shouldn't have used the word often. But I know for a fact, and it is documented on the NASA web site, that nose wheel steering was added. One of the reasons stated for adding the nw steering was the wear on the brake system, and blown out tires. I will provide the link when time allows. I suspected the rudder was available to the CDR and PLT but am not sure, I would like someone to clear that up. As for the chute DTO please feel free to clear that up for us. Jim in Houston.
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tdadamemd-spamblock-@excite.com - 31 Aug 2007 18:27 GMT >From Jim in Houston: > >> Now I get it. I didn't understand how that worked. But... I thought [quoted text clipped - 14 lines] > >inaccuracies that have been posted on that Crosswind DTO thread as > >well.)
> I probably shouldn't have used the word often. But I know for a fact, > and it is documented on the NASA web site, that nose wheel steering [quoted text clipped - 4 lines] > sure, I would like someone to clear that up. > As for the chute DTO please feel free to clear that up for us. I would be interested to hear from Danny before elaborating, because I know that he is well aware of the answers.
But Jim, you might find some satisfaction to hear that there ARE astronauts who know how to fly with the rudder on the Space Shuttle! Basic piloting skill like Danny learned in the Air Force.
...as for the Xwind DTO, the correction belongs on that thread.
~ CT
Jim in Houston - 31 Aug 2007 22:19 GMT
>I would be interested to hear from Danny before elaborating, because I >know that he is well aware of the answers. [quoted text clipped - 6 lines] > >~ CT Well I would be interested in reading what you are alluding to concerning the DTO in whatever thread. I understand that the crosswind limit for the shuttle is 15 knots, IIRC the crosswind component was 17 knots at the time of the landing. I would think that the late chute is related to the slightly excessive cw component. I know that there is a list of DTO's that they invoke when opportunities arise. I just felt confident that with the call about the DTO and the higher cw that they had a DTO opportunity that they took. I know from my own flying experience (limited to Cessna, Piper, and Grumman tricycle type aircraft), that the rudder, while not essential, makes flying much safer and easier. It would seem that the Shuttle, being a glider, would require pilot controlled rudder to maneuver. I understand that the airbrake feature would change the characteristic of the rudder, but rudder would still be needed. I need to research this further.
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Danny Deger - 01 Sep 2007 21:41 GMT On Aug 31, 5:19 pm, Jim in Houston <nospamjamesgoo...@sbcglobal.netnospam> wrote:
> On Fri, 31 Aug 2007 10:27:38 -0700, tdadamemd-spamblo...@excite.com > wrote: [quoted text clipped - 25 lines] > of the rudder, but rudder would still be needed. I need to research > this further. The Digital Auto Pilot uses the rudder below Mach 5 to "center the ball", even if the pilot doesn't touch the pedals. I have never heard of a pilot moving the pedals while airborn.
Danny Deger
> -- > Posted via a free Usenet account fromhttp://www.teranews.com Danny Deger - 01 Sep 2007 21:38 GMT On Aug 31, 1:27 pm, tdadamemd-spamblo...@excite.com wrote:
> >From Jim in Houston: > > >> Now I get it. I didn't understand how that worked. But... I thought [quoted text clipped - 10 lines] > > >And for Danny, I have this point of feedback: the rudder is used even > > >when the autopilot is not engaged! There might be some confusion on the use of the term "autopilot". In most planes when the pilot is manupulating the controls, the autopilot is off. In the shuttle the Digital Autopilot Pilot (DAP) is ALWAYS flying the shuttle. If the pilot wishes, he can take Controlled Stick Steering (CSS) and manipulate the controls. If the pilot is not manipulating the controls, DAP takes its commands from a piece of software called "guidance".
> > >(And I find it curious that no one has straightened out the > > >inaccuracies that have been posted on that Crosswind DTO thread as [quoted text clipped - 10 lines] > I would be interested to hear from Danny before elaborating, because I > know that he is well aware of the answers. I started work for NASA in 1990, so I can't say for sure what the early shuttles had. I don't recall anyone telling me the early shuttle's didn't have nosewheel steering, but maybe they didn't.
Danny Deger
tdadamemd-spamblock-@excite.com - 01 Sep 2007 17:32 GMT >From Jim in Houston: > On Fri, 31 Aug 2007 00:23:08 -0700, tdadamemd-spamblo...@excite.com > wrote:
> >> I remember that prior to nw steering they were using differential > >> braking which often resulted in blown tires. [quoted text clipped - 4 lines] > >Particularly, this notion of the shuttle blowing tires "often". That > >goes totally against my understanding of the shuttle program history.
> I probably shouldn't have used the word often. But I know for a fact, > and it is documented on the NASA web site, that nose wheel steering [quoted text clipped - 3 lines] > I suspected the rudder was available to the CDR and PLT but am not > sure, I would like someone to clear that up. Let's be clear that there has only been one blown tire in the history of the shuttle program. That was Karol Bobko on 51-D (with Jake Garn). They experienced somewhere around 8 knots of crosswind. Near the end of their rollout, a brake failed, locked up, and the right inboard main tire blew. This served as a primary driver for getting NWS capability.
(ref - http://members.aol.com/WSNTWOYOU/STS16MR.HTM)
But for all I know, it could have been piloting technique that caused the problem. I would guess that if Bobko had used sufficient rudder aero forces to maintain directional tracking down the runway instead of differential braking as the primary means, then there would have been no problem at all. I have not seen the traces of his inputs, but if he did not blend up to maximum rudder input during that rollout, then the pilot contributed to the problem.
Bobko did go on to fly one more mission (51-J), but those were the days of one-a-month/two-a-month flight rates. He did not fly at all post-51L like his contemporaries like Dan Brandenstein and Vance Brand.
Some might believe that approval of the NWS mod served to vindicate Bobko, but there are many examples of where the pilot made a mistake and an engineering solution was incorporated just to make it easier on the pilots.
~ CT
Jim in Houston - 02 Sep 2007 16:19 GMT
>But for all I know, it could have been piloting technique that caused >the problem. I would guess that if Bobko had used sufficient rudder [quoted text clipped - 15 lines] > >~ CT I have heard it mentioned, and know that to many pilots it is very important to land or, in the case of the Shuttle, to stop with the nose wheel on the center line of the runway. In my limited experience with light aircraft, I am happy to be on the runway at all!! Concerning the tires and CDR Bobko, I accept that his flight was the only one to actually blow a tire. I know for a fact however, that there was great concern about tire wear prior to the advent of NWS and perhaps still is. But it was this wear issue, and the blown tire, that sealed the deal on the NWS. I recall seeing pictures of tires worn down to the cords due to the differential braking and the obsession with stopping on the centerline. AFAIK Bobko is held in high esteem in the astronaut community. Regards, Jim in Houston.
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tdadamemd-spamblock-@excite.com - 02 Sep 2007 22:50 GMT >From Jim in Houston: > AFAIK Bobko is held in high esteem in the astronaut community. He is the first Air Force Academy graduate to ever fly in space.
...and he is also the first Air Force Academy graduate to blow a tire on a spaceship! Ha! I'm sure that he and his peers all get a good laugh about it these days.
~ CT
Jim in Houston - 03 Sep 2007 02:42 GMT >>From Jim in Houston: >> AFAIK Bobko is held in high esteem in the astronaut community. [quoted text clipped - 6 lines] > >~ CT That would evoke a chuckle wouldn't it? Irony is so ironic!!! Jim in Houston.
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Danny Deger - 01 Sep 2007 21:31 GMT On Aug 30, 10:09 pm, Jim in Houston <nospamjamesgoo...@sbcglobal.netnospam> wrote:
> On Thu, 30 Aug 2007 10:56:04 -0500, "Danny Deger" > [quoted text clipped - 19 lines] > braking which often resulted in blown tires. > Jim in Houston. snip
Yes. Nosewheel steering is used, but the pilots control the nosewheel steering via the rudder pedals. They will also use the pedals after touchdown but befor the nose is on the ground. In this way they are using the rudder. Before main wheel touchdown, the rudder pedals are never used -- at least for anything I know about and I used to teach this phase of fligh to the astronuats.
Danny Deger
Jim in Houston - 01 Sep 2007 23:13 GMT
>Yes. Nosewheel steering is used, but the pilots control the nosewheel >steering via the rudder pedals. They will also use the pedals after [quoted text clipped - 4 lines] > >Danny Deger If I ever suggested that you didn't know what you were talking about I sincerely apologize. I never meant to imply that. I am a pilot with limited experience (less than 200 hours). The way the rudder on the Shuttle works is very intriguing to me; simple as that. I still can't get my little brain to understand how a rudder, with a built in speed brake that splits it in half, can be effective as a rudder. But it all seems to work just fine. In my searching for rudder info on the shuttle I found some very interesting information about the actuator for the rudder, and that on some pre Columbia accident flights, some parts of the actuators used on, IIRC, all the shuttles were put in backwards! How those flights got away without that causing a catastrophic accident is just a miracle. Jim in Houston.
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Danny Deger - 03 Sep 2007 01:06 GMT On Sep 1, 6:13 pm, Jim in Houston <nospamjamesgoo...@sbcglobal.netnospam> wrote:
> On Sat, 01 Sep 2007 13:31:21 -0700, Danny Deger > [quoted text clipped - 15 lines] > brake that splits it in half, can be effective as a rudder. But it all > seems to work just fine. When the speed brake is out and let's say a right rudder command is issued, the left panel closes a bit and the right panel opens a bit.
Danny Deger
tdadamemd-spamblock-@excite.com - 02 Sep 2007 02:26 GMT Thanks for clarifying your "autopilot" statement, Danny. I need to clarify mine: Rudder is still used when CSS is engaged.
>From Danny Deger: > Yes. Nosewheel steering is used, but the pilots control the nosewheel [quoted text clipped - 3 lines] > never used -- at least for anything I know about and I used to teach > this phase of fligh to the astronuats. I am surprised to see you take the hard line about the rudder never being used. If you were to say that no pilot in the history of the program has ever touched the rudder while airborne, that would not surprise me. But with all of your "never"s, it gives the impression that there is no scenario where you would see fit for the rudder to be used. I can think of at least three. Yes, all three are off- nominal. But if you tell me that in all of your years of instructing astronauts on how to land, I will be *shocked* if you tell me that you _never_ told any pilots that using the rudder on approach is a good thing to do in certain situations.
And I will be even more shocked if you say that you never saw a shuttle pilot fly with the rudder in the sim. You must know that heavy use of rudder is *standard* procedure for a common maneuver that astronauts do on final approach.
As I stated earlier, the reason for using rudder like this falls back to basic pilot skills.
~ CT
Jim in Houston - 02 Sep 2007 14:33 GMT
>And I will be even more shocked if you say that you never saw a >shuttle pilot fly with the rudder in the sim. You must know that [quoted text clipped - 5 lines] > >~ CT Why so cryptic? You afraid of disclosing that the shuttle is in fact slipped in sometimes on final. Or that an occasional wing wiggle is done to say hello on the way in? I think you just enjoy faking the notion that you have inside information that no one else is privy to. I don't know what you know or even who you are. You obviously have a keen knowledge of Shuttle ops. But you obviously don't have the balls to come out and say what you mean or who you are. You could take a lesson from Jorge or even Danny. Folks like me read the posts to learn and keep informed, 90% of the people who use the Internet don't know what Usenet is, or how to access it. I just don't understand the cloak and dagger routine. Jim in Houston.
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tdadamemd-spamblock-@excite.com - 02 Sep 2007 16:57 GMT >From Jim in Houston: > Why so cryptic? You afraid of disclosing that the shuttle is in fact [quoted text clipped - 9 lines] > what Usenet is, or how to access it. I just don't understand the cloak > and dagger routine. I am not wearing any cloak. And I bear no daggers.
You may have seen on that other thread where Jorge made a statement about ISS-Shuttle undock that any person who has passed freshman physics could see as inaccurate, yet such statements go unquestioned.
That is not knowledge "that no one else is privy to".
On this thread, a former F-4 pilot has made it sound like there is no time when a shuttle pilot would use rudder prior to touchdown. Any person with basic piloting knowledge would question that, as you have.
Once again, knowing smart ways to use a rudder is not knowledge that no one else is privy to. You yourself, Jim, have already stated one of the three scenarios as to when the rudder comes in handy for the shuttle. And the second one is obvious too. I'm sure you can tell us yourself. The third one is not quite as obvious. But anyone who has flown an aircraft with a HUD should know.
These types of corrections are no big deal. "I forgot that the rudder is an extremely useful tool for energy management." Or, "I forgot that the rudder is an extremely useful tool for improving roll performance."
Or, "I forgot that momentum is the product of mass TIMES velocity."
But it becomes a bigger deal when people who should know better blow off the basics, like oxygen tanks being specifically designed with blow-out rupture discs and stuff that have cost astronaut's lives.
The idea that scares me is the notion that these people *actually don't know*. Jorge has let days go by without providing any indication that he knows the difference between momentum and velocity. Jim Oberg was part of that discussion as well, and he has been silent. I've had direct discussions with Sy Liebergot about Apollo 13, reminding him that the oxygen tanks were designed so they would not explode, and he has yet to acknowledge this fact. He seems perfectly comfortable with calling the incident an explosion.
As for this thread here, I KNOW that Danny knows how to use a rudder to his advantage. If he didn't learn this in F-4s then I don't know how he made it through AF UPT. It would then follow that he knows how to use the rudder in the space shuttle. Yet he says the things he has said here.
Part of the reason why I haven't posted it myself as yet is because I am baffled. I am being accused of cloak&daggering. If there are any daggers involved, you might want to consider the possibility that it is the poster falling on their own dagger.
I do understand that me posting corrections runs the risk of embarrassing someone (myself included). But say that on the very next shuttle flight, the crew ends up in an ECAL abort with very high energy on final. Say that they manually take the speed brake to full open but do nothing with the rudder, because no one in DT ever taught them to use the rudder. Say that the shuttle then lands long, rolls off the end of the runway, snaps the nose gear, blows the FWD RCS tanks and the crew dies.
Improbable, sure. But possible. We here have the opportunity, however small, to potentially help improve the training of shuttle pilots. Or we can sit back in silence, let it slide so as not to embarrass anyone and hope that this is not the mistake that proves fatal.
~ CT
Jim in Houston - 02 Sep 2007 19:45 GMT On Sun, 02 Sep 2007 08:57:58 -0700, tdadamemd-spamblock-@excite.com wrote: Say that the shuttle then lands long, rolls
>off the end of the runway, snaps the nose gear, blows the FWD RCS >tanks and the crew dies. [quoted text clipped - 6 lines] > >~ CT Point - set - match. You win. Prior to reading this post I didn't get your drift. But I, with my very limited piloting experience, and zero engineering training experience was not aware of the third rudder energy management scenearo. I agree that if Danny was teaching people how to fly the machine without this knowledge... well I just don't know what to say. I appreciate your explanation, and your patience with my ignorance. I apologize for any inappropriate comments. Just one point, if I may, wouldn't they dump the RCS prop prior to landing? Thanks again. I guess I should go back to lurk mode and let people who know what they are talking about have the floor. Jim in Houston.
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Jorge R. Frank - 02 Sep 2007 20:22 GMT >> Say that the shuttle then lands long, rolls >> off the end of the runway, snaps the nose gear, blows the FWD RCS [quoted text clipped - 4 lines] > Just one point, if I may, wouldn't they dump the RCS prop prior to > landing? The forward RCS prop is burned to depletion prior to entry. They literally burn until the forward thrusters are starved of propellant and start annunciating "fail off". There will be some unusable propellant trapped in the lines, but definitely not enough to blow the tanks even in a worst-case landing scenario.
You can take back at least one of your points. Resume match...
tdadamemd-spamblock-@excite.com - 02 Sep 2007 23:08 GMT >From Jorge:
> > Just one point, if I may, wouldn't they dump the RCS prop prior to > > landing? [quoted text clipped - 4 lines] > trapped in the lines, but definitely not enough to blow the tanks even > in a worst-case landing scenario. It was a pilot astronaut who told me about this very scenario of why driving off the runway can be expected to be fatal for the entire crew. But I am totally open to the possibility that they were speaking from a position of ignorance and that Jorge's version of the risk is accurate.
We are all ignorant to one degree or another. That includes astronauts, engineers and Cessna pilots. I don't see that as a reason for any of us to hold back from contributing or asking questions. It is all a grand collective effort to help us draw back that veil of ignorance by just a little bit with each successive generation.
One of my most rewarding ways to learn is when one of my children teaches me something. It happened just yesterday while mowing the yard with them. I approached it with the attitude that I would be teaching them something, but the flow of learning was two-way.
~ CT
tdadamemd-spamblock-@excite.com - 02 Sep 2007 23:39 GMT >From Jim in Houston: > Prior to reading this post I didn't get your drift. But I, with my > very limited piloting experience, and zero engineering training > experience was not aware of the third rudder energy management > scenearo. Ok, I need to be explicit here...
Only one scenario is for energy management. If you want to dissipate a lot of energy, you can kick in the rudder so that the entire airframe acts as one big speedbrake. That is the classic slip that has already been mentioned early on in this thread. The method works great on the space shuttle as with other aircraft. It is not the first method that I would resort to for dissipating excess energy while on final in the shuttle, but it certainly belongs in a good glider pilot's bag of tricks.
The second scenario is the need to increase roll performance. For any aircraft that has either swept leading edges for its wings or a dihedral (wings canted upward from root to tip), a beta slip angle will have the second-order effect of causing that aircraft to roll in the direction of the slip. So if you want to increase your roll performance, instead of just using aileron you can kick in some rudder in the direction of roll. Where shuttle pilots do this is when they are goofing off in the sim and flying aileron rolls down final. The roll can be done just fine with feet on the floor, but it is more effective to use the rudder. Astronauts teach this use of rudder. For whatever reason, Danny apparently doesn't. And it stands to reason that on an actual shuttle landing, if an abrupt roll maneuver was required for some off nominal situation (like breaking out of the clouds with a bad nav state) then a smart astronaut will consider using rudder to help out with those abrupt rolls.
Now the third scenario has nothing to do with energy management or performance. It has to do with the limitations of the Heads Up Display. The HUD presents critical flight information in a relatively narrow field of view. In a situation with a large crosswind, it is possible that the flight vector symbol will get pegged to the edge of that field of view and then you are stuck at guessing where that symbol is actually pointing. The solution to this, as most HUD pilots know, is to kick the rudder enough to bring that symbol back within the field of view and you can know exactly where it is pointing.
That's all of the reasons that I know of for using the shuttle's rudder prior to touchdown. There may be others.
...oh yeah, like wanting to stretch out your legs and inadvertantly wiggling them. Or flying a Rudder Doublet DTO. Or...
But I myself would be very cautious about making absolute statements like the rudder is "never used".
~ CT
tdadamemd-spamblock-@excite.com - 03 Sep 2007 00:35 GMT Ok, I just thought of one more scenario, albeit more extreme than the others. It is the most obvious scenario because it is the title of this thread...
Just because the shuttle isn't slipped wing-low, doesn't mean that it *can't* be. It is conceivable that some emergency puts the orbiter in a situation where it is headed toward a runway where the crosswinds are way out of limits. Two choices that the commander would then face are to expect to blow one or more main gear tires (potentially fatal) or to command a bailout in lieu of attempting to land in the excess xwind.
Now the third option that a smart commander would consider is to prevent blowing the tires by cross controlling the landing (induce a beta angle in order to line the tires up more straight to the concrete).
Now that is an extremely unlikely scenario and I don't see any reason to train for it, but it is a basic skill that any pilot should know how to do.
~ CT
Danny Deger - 03 Sep 2007 01:13 GMT On Sep 2, 11:57 am, tdadamemd-spamblo...@excite.com wrote:
> >From Jim in Houston: > > Why so cryptic? You afraid of disclosing that the shuttle is in fact [quoted text clipped - 33 lines] > that the rudder is an extremely useful tool for improving roll > performance." The shuttle's autopilot moves the rudder if the pilot commands a roll, but the rudder pedals are not moved.
Danny Deger
Danny Deger - 03 Sep 2007 01:10 GMT On Sep 1, 9:26 pm, tdadamemd-spamblo...@excite.com wrote:
> Thanks for clarifying your "autopilot" statement, Danny. I need to > clarify mine: Rudder is still used when CSS is engaged. [quoted text clipped - 27 lines] > > ~ CT As far as I know, the rudder pedals have never been touched while in the air (an early DTO?), and I can say with great confindence I taught there is no reason to touch the pedals while airborne. Keep in mind I am the owner of a small taildragger and in this plane, rudder is used all the time.
Danny Deger
tdadamemd-spamblock-@excite.com - 03 Sep 2007 02:44 GMT >From Danny Deger: > As far as I know, the rudder pedals have never been touched while in > the air (an early DTO?), and I can say with great confindence I taught > there is no reason to touch the pedals while airborne. Keep in mind I > am the owner of a small taildragger and in this plane, rudder is used > all the time. I would agree that the shuttle can be flown perfectly well with no rudder in nominal conditions. But the four scenarios specified were discussing way off-nominal conditions that I expect that you trained for. So it appears that you are saying that you would teach a pilot to not touch the rudders even if they find themselves in any of these four: hi energy, roll perf, HUD xwind and xwind out of limits.
Curious. But I would agree that it is not *necessary* to use rudder. This leads to a follow up: If a pilot *did* use the rudder to help themselves out in such a situation, would you ding them for doing so?
~ CT
Danny Deger - 03 Sep 2007 21:20 GMT On Sep 2, 9:44 pm, tdadamemd-spamblo...@excite.com wrote:
> >From Danny Deger: > > As far as I know, the rudder pedals have never been touched while in [quoted text clipped - 15 lines] > > ~ CT I would ding him for say a massive slip using massive amounts of rudder to generate a slip -- if he didn't try the manuever out in the sim first. I would also need to make sure the simulator didn't go outside of the limits of the aerodata base -- and the aerodata base has a small limit on sideslip angle. If you are flying outside the limits of the aerodata base, the sim response is not correct.
One last point, I got out of training in 1995, perhaps using rudders for the cases you mentioned have been added to the training flow. In the second to the last flight, the CDR was briefed to expect HUD saturation due to cross winds at 10K feet, but no mention of using the rudders to unstaturate the HUD. I agree the rudders might fix the problem here, but I have no recall of the technique being used earlier than 1995.
Danny Deger
tdadamemd-spamblock-@excite.com - 03 Sep 2007 22:07 GMT >From Danny Deger: > On Sep 2, 9:44 pm, tdadamemd-spamblo...@excite.com wrote: > > If a pilot *did* use the rudder to help > > themselves out in such a situation, would you ding them for doing so?
> I would ding him for say a massive slip using massive amounts of > rudder to generate a slip -- if he didn't try the manuever out in the > sim first. Yeah, it is definitely necessary to try out these tricks in the sim so that you can learn what works and what doesn't. And to find out what point 'some' becomes 'too much'.
Thanks again, Danny. And as always, I wish you the best in your future pursuits.
~ CT
MichaelJP - 05 Sep 2007 17:08 GMT > >From Danny Deger: >> On Sep 2, 9:44 pm, tdadamemd-spamblo...@excite.com wrote: [quoted text clipped - 13 lines] > > ~ CT Very interesting discussion to read this from the basic light aircraft pilot's point of view.
Watching the HUD videos and the north end camera view from the STS-118 landing, the shuttle does roll slightly to the left about 1 second before touchdown and in fact the left mainwheels touch down first. Looks to have a touch of right rudder also but its hard to tell on the lo-res video.
Is the pilot de-crabbing at this point?
- Michael
tdadamemd-spamblock-@excite.com - 05 Sep 2007 23:53 GMT >From MichaelJP: > Watching the HUD videos and the north end camera view from the STS-118 [quoted text clipped - 3 lines] > > Is the pilot de-crabbing at this point? Perhaps we have not been clear enough. To restate: There is no need, under nominal conditions, for the pilot to ever touch the rudder prior to touchdown. That would include high crosswinds up to limits.
For whatever crab angle you have at touchdown, the side-forces on the main gear tires work to straighten out the nose down the runway. Rudder inputs after touchdown are primarily to achieve tracking toward the centerline. There isn't much need to use rudder inputs to straighten the nose down the runway because the tires do a good job of taking care of that.
~ CT
Jim in Houston - 06 Sep 2007 04:10 GMT
>Perhaps we have not been clear enough. To restate: There is no need, >under nominal conditions, for the pilot to ever touch the rudder prior [quoted text clipped - 8 lines] > >~ CT No doubt that what you have stated is true and correct. However, IIRC the CW was 17KT at touchdown. The CW was hitting the Orbiter from the port side IIRC. With the massive cross section of the Orbiter, a CW component of 17KT would have a large influence on the lateral movement. Also IIRC the crosswind limit is 15KT, so to add insult to injury we are 2KT over the limit. My experience is strictly limited to GA aircraft where we would apply left aileron into the CW and rudder to align the nose to the runway centerline. This would result in touchdown on the left main, with the right main dropping onto the ground shortly there after. The rudder is then the only aerodynamic surface used to affect any of the planes axes after landing. (Cessna's do have a bungee connected from the rudder to the NW, a form of NWS, but I don't know about other light GA aircraft) Not wishing to beat a dead horse any more than which we have already beat it, we did see the CDR land left wing slightly down, and touch down on the left main just like in my GA experience. IIRC in this thread, the DAP, not the CDR, would command the rudder to align the longitudinal axis of the Orbiter with the runway. The CDR would be controlling the elevon, lowering the left wing, to arrest the right lateral deviation caused by the CW? Then using the NW steering or rudder the CDR would maintain centerline until wheels stop? IS that correct? One other question, if I may, do the landing gear trucks swivel on the Shuttle ( like on the C5 for instance). That would account for crabbing without using the rudder to recover. Thanks for your patience Jim in Houston.
Contrary to popular opinion RN does not mean Real Nerd! Teddy Roosevelt's mother said: "Fill what is empty, empty what is full, and scratch where it itches"
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tdadamemd-spamblock-@excite.com - 06 Sep 2007 04:37 GMT >From Jim in Houston: > With the massive cross section of the Orbiter, a CW > component of 17KT would have a large influence on the lateral > movement. Also IIRC the crosswind limit is 15KT, so to add insult to > injury we are 2KT over the limit. You might want to recheck your facts there. Crosswind for STS-118 was nowhere near the limit. I heard numbers closer to 7kts. They did Not accomplish the Xwind DTO (which requires 10kts).
> My experience is strictly limited to GA aircraft where we would apply > left aileron into the CW and rudder to align the nose to the runway [quoted text clipped - 16 lines] > Shuttle ( like on the C5 for instance). That would account for > crabbing without using the rudder to recover. Whoa! The horse is far from dead if you guys are making statements like that!
Repeating for clarity: The shuttle is Not cross controlled on final. It is not done by pilots. It is not done by flight software.
Rudder inputs done by the computer are to coordinate turns. As Danny said, to "center the ball". This keeps any beta sideslip to a minimum, therefore maintaining the crab angle at touchdown. Nominally, there is no effort made by anyone to remove the crab prior to touchdown.
Just because one wheel touches before the other does not mean that the vehicle flew a wing-low cross-controlled approach. With zero beta, all one wheel touching down before the other means is that the vehicle was in a slight *turn* at touchdown. A coordinated turn.
It may have been more helpful if the question from the very first post of this thread had gotten nipped in the bud:
"So, the questions is: Is the Shuttle slipped into the wind when on final, just like any other airplane?"
No. The shuttle is not slipped. And it is totally inaccurate to hold that "any other airplane" is slipped on final. There are plenty of airplanes designed to land in a crab. That goes for just about every modern fighter jet. It also holds true for the NASA T-38s. I have never heard of a T-38 being cross-controlled on final. For many aircraft, there is simply no need to. The space shuttle is one.
Ok, now if anyone sees the horse twitch, please let us know.
~ CT
MichaelJP - 06 Sep 2007 10:26 GMT > >From Jim in Houston: >> With the massive cross section of the Orbiter, a CW [quoted text clipped - 59 lines] > > Ok, now if anyone sees the horse twitch, please let us know. I think you've killed it. Thanks for the additional info.
A related question, anyone know the highest crosswind the shuttle has ever had to land in? Presumably it can be landed above the crosswind limit to allow for an unexpected windspeed increase on final.
tdadamemd-spamblock-@excite.com - 06 Sep 2007 22:49 GMT >From MichaelJP: > A related question, anyone know the highest crosswind the shuttle has ever > had to land in? Presumably it can be landed above the crosswind limit to > allow for an unexpected windspeed increase on final. I have never heard of any crosswind landings higher than single digit. If this strikes you as abnormally low, the rationale is simple: if the crosswind prediction is too high, then they will just wave off the deorbit burn and look for a more benign opportunity.
As for unexpected increases, they take the possibility of wind increases into account when they make the deorbit decision. This is the primary reason why the Xwind DTO has yet to be accomplished. However badly engineers may want that 10kt Xwind data point, the Flight Directors want just as badly to *avoid* it.
~ CT
Jim in Houston - 06 Sep 2007 11:38 GMT >>From Jim in Houston: >> With the massive cross section of the Orbiter, a CW [quoted text clipped - 5 lines] >nowhere near the limit. I heard numbers closer to 7kts. They did Not >accomplish the Xwind DTO (which requires 10kts). I have hearing that is just a bit better than Brian's seeing, so it is quite probable that I heard seven as seventeen. I could've sworn though, and would pass a polygraph, that the final wind call was 17KT. I concede the point. Do I have the CW limit correct? Now if you all will excuse me, I have a horse to bury. Jim in Houston.
Contrary to popular opinion RN does not mean Real Nerd! Teddy Roosevelt's mother said: "Fill what is empty, empty what is full, and scratch where it itches"
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tdadamemd-spamblock-@excite.com - 06 Sep 2007 22:57 GMT >From Jim in Houston: > >> With the massive cross section of the Orbiter, a CW [quoted text clipped - 10 lines] > though, and would pass a polygraph, that the final wind call was 17KT. > I concede the point. Do I have the CW limit correct? Basically, yes. The crosswind limit is typically 15kts.
But there are other factors where they make the rules more conservative, like pilot fatigue for being on orbit more days than normal, or landing at night, or with an APU malfunction (limiting hydraulic flow available to flight controls) and other factors that you might imagine. Even different set of rules for aborts. There are abort situations where they will be less conservative.
But keep in mind that these rules are only the rules, subject to judgement calls and waivers. And more importantly like MJP points out above, the decision to bring the shuttle down is based only on this prediction. The ultimate answer is that...
You land with whatever crosswind you find when you get there. I don't know of anyone who would bailout because winds are "out of limits" rather than give it their best go.
~ CT
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