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#71
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Oberg: "The real significance of the ISS thruster test failure"
Pat Flannery wrote: Again, on the Intermountain Railways model....with the implied proviso "get ****in real". (anyone who hasn't built that model hasn't gotten any real idea exactly _how_ big the original ISS proposal was intended to be. I've got a Mir; I've got two Salyuts: I've got a Skylab.... that SOB is gigantic.) Following that up, NASA's biggest mistake was always showing the scale of the ISS in regards to a docking Shuttle instead of an EVAing astronaut. It's ****in' HUGE, as in Saturn V first stage huge. You know; "how big?" ..reply being "around a city block across". Pat |
#72
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Oberg: "The real significance of the ISS thruster test failure"
Pat Flannery wrote in
: Jorge R. Frank wrote: Yeah, I kind of thought so with all the modules sticking out at the front end. It's not the modules that make up the bulk of the area; it's the solar arrays and radiators. No, looking at the huge model (one of my favorites) you can feather the solar arrays so that the present minimal drag to the ISS as she travels forward through space, and the radiators are put in her drag shadow. The station can't fly like that all the time; the solar arrays have to be feathered face-on (and the radiators edge-on) to the sun during orbital day. *As I said before*, the ballistic number I quoted was an "average" value over an orbital day, to account for solar array/radiator area. Of course, that the final configuration actually is seems to change from month-to-month. The only major difference in frontal area between the config I quoted above and the "current" config is the deletion of the Russian Science Power Platform. Again, on the Intermountain Railways model....with the implied proviso "get ****in real". I have that model... in fact, I have two of them, one at home and one at work. I've even done a bit of scratch-build on both of them to properly depict the current config (the IMR instructions only describe how to build the "assembly complete" config). Clarifying my earlier statement, I should have wrote "current planned assembly complete config", not "current config in orbit right now". -- JRF Reply-to address spam-proofed - to reply by E-mail, check "Organization" (I am not assimilated) and think one step ahead of IBM. |
#73
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Oberg: "The real significance of the ISS thruster test failure"
JRS: In article , dated Sat, 13
May 2006 19:05:46 remote, seen in news:sci.space.station, Jorge R. Frank posted : "Jorge R. Frank" wrote in : The ballistic number of the current config is 166.0 kg/m^2 while flying in XVV (normal low-beta) attitude. That's a mass/area ratio; the higher the number, the *less* draggy the station is. The ballistic number of the station at assembly complete will be 70.02 kg/m^2, which is considerably less draggy than the current config. Oops - got that backward; the final config is more draggy. What does the drag amount to in actual Newtons and pounds-of-force, for a typical or mean attitude? It can hardly be 166 kgf/m^2. -- © John Stockton, Surrey, UK. Turnpike v4.00 MIME. © Web URL:http://www.merlyn.demon.co.uk/ - FAQqish topics, acronyms & links; Astro stuff via astron-1.htm, gravity0.htm ; quotings.htm, pascal.htm, etc. No Encoding. Quotes before replies. Snip well. Write clearly. Don't Mail News. |
#74
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Oberg: "The real significance of the ISS thruster test failure"
Dr John Stockton wrote in news:$n9DF9AxAObEFwW9
@merlyn.demon.co.uk: JRS: In article , dated Sat, 13 May 2006 19:05:46 remote, seen in news:sci.space.station, Jorge R. Frank posted : "Jorge R. Frank" wrote in : The ballistic number of the current config is 166.0 kg/m^2 while flying in XVV (normal low-beta) attitude. That's a mass/area ratio; the higher the number, the *less* draggy the station is. The ballistic number of the station at assembly complete will be 70.02 kg/m^2, which is considerably less draggy than the current config. Oops - got that backward; the final config is more draggy. What does the drag amount to in actual Newtons and pounds-of-force, for a typical or mean attitude? It can hardly be 166 kgf/m^2. Right, the ballistic number is not pressure (force per unit area) but rather mass per unit area. So 166 kg/m^2 means the station has 166 kg of mass for every square meter of projected area. Drag force is F = 0.5*rho*v^2*Cd*A, drag deceleration is a = F/m. The ballistic number is BN = m/(Cd*A) so drag simplifies to a = 0.5*rho*v^2/BN or F = 0.5*rho*v^2*m/BN. m is around 185,000 kg, v is around 7700 m/s. I don't have my atmosphere models handy so plug in your favorite value for rho and chug away. -- JRF Reply-to address spam-proofed - to reply by E-mail, check "Organization" (I am not assimilated) and think one step ahead of IBM. |
#75
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Oberg: "The real significance of the ISS thruster test failure"
In article ,
Jorge R. Frank wrote: No, looking at the huge model (one of my favorites) you can feather the solar arrays ... The station can't fly like that all the time; the solar arrays have to be feathered face-on (and the radiators edge-on) to the sun during orbital day. There's always an orientation which puts the radiators edge-on to both the Sun and the air, although perhaps it might be one that ISS can't use because of something like gimbal limits. To keep the solar arrays edge-on to the air, alas, you'd have to accept less-than-ideal Sun angles much of the time, and a penalty on power output as a result. (Mind you, it might have been preferable to just make the arrays somewhat bigger and plan to operate this way, to save reboost fuel; there was a nice little paper by Landis&Yu in 1991 suggesting this.) -- spsystems.net is temporarily off the air; | Henry Spencer mail to henry at zoo.utoronto.ca instead. | |
#76
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Oberg: "The real significance of the ISS thruster test failure"
Mind you, it might have been preferable to just make the arrays
somewhat bigger and plan to operate this way, to save reboost fuel; there was a nice little paper by Landis&Yu in 1991 suggesting this. They still could do this, couldn't they? At least assuming the next few assembly flights occur, they'll have more power than they know what to do with, at least for a while. Or is there something about the radiator design or something which precludes it? |
#77
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Oberg: "The real significance of the ISS thruster test failure"
Jorge R. Frank wrote: Again, on the Intermountain Railways model....with the implied proviso "get ****in real". I have that model... in fact, I have two of them, one at home and one at work. I've even done a bit of scratch-build on both of them to properly depict the current config (the IMR instructions only describe how to build the "assembly complete" config). That's a pretty challenging model to build; particularly as to how you put it down during construction with all that gobblety gook sticking out of it. It comes in a surprisingly small box given its finished size. I wonder if that was the only commercial kit ever produced at taxpayer expense? (NASA funded the design of the kit so that their contractors on the ISS could have a model to go by to keep everything straight.) Pat |
#78
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Oberg: "The real significance of the ISS thruster test failure"
Pat Flannery wrote in
: Jorge R. Frank wrote: Again, on the Intermountain Railways model....with the implied proviso "get ****in real". I have that model... in fact, I have two of them, one at home and one at work. I've even done a bit of scratch-build on both of them to properly depict the current config (the IMR instructions only describe how to build the "assembly complete" config). That's a pretty challenging model to build; particularly as to how you put it down during construction with all that gobblety gook sticking out of it. One technique is not to religiously follow the instructions: go ahead and glue each module from its parts, and test-fit the modules together (sanding the connecting pegs as necessary), but don't permanently glue the modules together. That not only allows you to build different station configurations, it also makes it easier to put the thing down without breaking it, since you don't have to keep the more fragile modules attached while you're assembling the rest of it. Another technique is to improvise display stands for the intermediate configs. The IMR stand is really only suitable for the assembly complete config, since the struts are so far apart. I scrounged together some parts from a children's construction set toy (don't remember the brand name, but it's kind of like plastic Tinkertoys in 3D - the hubs are spherical rather than discs) and built some bases out of those; the pegs that the IMR model uses to join the modules fit nicely into the holes in the hubs. It comes in a surprisingly small box given its finished size. I'm impressed by the engineering behind it (which was done at Johnson Engineering rather than IMR). The modules really do fit together well with just light sanding on the connecting pegs, and the pegs are strong enough to carry the loads of the completed config without glue. And I'm sure you've noticed that the model includes the parts for an Orbiter Docking System (though the instructions don't mention it) that has a slot cut in the bottom to accommodate the ribbed payload bay in Revell's 1:144 orbiter model. The kicker is that the ODS will snap into the payload bay without glue (provided you didn't already glue in the Spacelab module that comes with the Revell kit) and that the ISS model is strong enough for you to hang the orbiter model off of it. I wonder if that was the only commercial kit ever produced at taxpayer expense? (NASA funded the design of the kit so that their contractors on the ISS could have a model to go by to keep everything straight.) Didn't know that, but it doesn't particularly surprise me given that no one was exactly stepping up to build a purely commercial model (the last SSF/ISS model I'm aware of was Revell's model of Boeing's SOC station concept from 1982 or so). And it was almost certainly less expensive than commissioning JSC's in-house model shop; they probably would have cost about as much per-model as the entire design and setup cost for the IMR kit. -- JRF Reply-to address spam-proofed - to reply by E-mail, check "Organization" (I am not assimilated) and think one step ahead of IBM. |
#79
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Oberg: "The real significance of the ISS thruster test failure"
Jorge R. Frank wrote: One technique is not to religiously follow the instructions: go ahead and glue each module from its parts, and test-fit the modules together (sanding the connecting pegs as necessary), Oh yes, those pegs... it sure would have been nice if all of them and their mounting holes were the same size. Looking at them, you assume that is the case; it is not the case. I'm impressed by the engineering behind it (which was done at Johnson Engineering rather than IMR). It's a tough little honker, that's for sure; and it's made out of very high quality plasic as well. the really impressive engineering is on the big Canadian remote manipulator arm- that's a little work of art in itself. The modules really do fit together well with just light sanding on the connecting pegs, and the pegs are strong enough to carry the loads of the completed config without glue. And I'm sure you've noticed that the model includes the parts for an Orbiter Docking System (though the instructions don't mention it) that has a slot cut in the bottom to accommodate the ribbed payload bay in Revell's 1:144 orbiter model. The kicker is that the ODS will snap into the payload bay without glue (provided you didn't already glue in the Spacelab module that comes with the Revell kit) and that the ISS model is strong enough for you to hang the orbiter model off of it. I have a 1/144th scale Shuttle, but it's attached to its ET and SRBs as it sits between the Saturn V and N-1 in front of me. You know what would have been nice for the ISS kit? A couple of EVA'ing astronauts to give it scale. I wonder if that was the only commercial kit ever produced at taxpayer expense? (NASA funded the design of the kit so that their contractors on the ISS could have a model to go by to keep everything straight.) Didn't know that, but it doesn't particularly surprise me given that no one was exactly stepping up to build a purely commercial model (the last SSF/ISS model I'm aware of was Revell's model of Boeing's SOC station concept from 1982 or so). Revell of Germany also makes a ISS in 1/144th: http://www.starshipmodeler.com/real/jc_iss.htm http://www.explorermagazin.de/modelle/miriss.htm I like their cutaway truss structure; although this doesn't look as tough as the IR one which was designed to be disassembled for easy transport. The Revell one is also cheaper than the IR one. http://www.spacetoys.com/proddetail.php?prod=MST11 Pat And it was almost certainly less expensive than commissioning JSC's in-house model shop; they probably would have cost about as much per-model as the entire design and setup cost for the IMR kit. |
#80
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Oberg: "The real significance of the ISS thruster test failure"
Pat Flannery wrote in
: Jorge R. Frank wrote: One technique is not to religiously follow the instructions: go ahead and glue each module from its parts, and test-fit the modules together (sanding the connecting pegs as necessary), Oh yes, those pegs... it sure would have been nice if all of them and their mounting holes were the same size. Looking at them, you assume that is the case; it is not the case. All things being equal, I'd agree. At least they generally erred on the side of making the pegs too big; it's a lot easier to sand them down than to putty them up. I'm impressed by the engineering behind it (which was done at Johnson Engineering rather than IMR). It's a tough little honker, that's for sure; and it's made out of very high quality plasic as well. Yes. Give credit to IMR; it's the type of plastic you typically see on model railroads rather than model airplanes. And it's a clean injection molding; no "flash" on the sprues. the really impressive engineering is on the big Canadian remote manipulator arm- that's a little work of art in itself. I was impressed that all seven joints work. It makes me annoyed that none of the shuttle model manufacturers have ever bothered to make an SRMS that works half as well, even at 1:72 scale. Perhaps you've also noticed that the sprues are almost exactly the right diameter to fit into the SSRMS end effectors, just in case you need to improvise "load-bearing" grapple fixtures as opposed to the decorative ones that come with the overpriced "enhancement kit". :-) I have a 1/144th scale Shuttle, but it's attached to its ET and SRBs as it sits between the Saturn V and N-1 in front of me. You know what would have been nice for the ISS kit? A couple of EVA'ing astronauts to give it scale. I scavenged one from my Boeing SOC model... :-) I wonder if that was the only commercial kit ever produced at taxpayer expense? (NASA funded the design of the kit so that their contractors on the ISS could have a model to go by to keep everything straight.) Didn't know that, but it doesn't particularly surprise me given that no one was exactly stepping up to build a purely commercial model (the last SSF/ISS model I'm aware of was Revell's model of Boeing's SOC station concept from 1982 or so). Revell of Germany also makes a ISS in 1/144th: http://www.starshipmodeler.com/real/jc_iss.htm http://www.explorermagazin.de/modelle/miriss.htm Right, but that one wasn't available at the time NASA contracted with Johnson/IMR. It also has some annoying inaccuracies, such as a Soyuz docked to Zarya *zenith* - when Zarya doesn't even *have* a docking port on the zenith side. They can't use "changes in the station configuration" as an excuse for that one; Zarya was *in space* before this model was produced! I like their cutaway truss structure; although this doesn't look as tough as the IR one which was designed to be disassembled for easy transport. Although more intricate, it's also less accurate; most of the truss is covered with thermal blankets. Though the IMR model isn't completely accurate either - it has thermal blankets even on the front panels of P1, S0, and S1, while the real ISS has open trusswork there. http://spaceflight.nasa.gov/gallery/images/shuttle/sts- 114/html/s114e6378.html If I had the patience, I'd paint the truss: aluminum girders, leave the thermal blanket white, and paint the front of the truss black where the open trusswork is supposed to be. And easy transport isn't the only reason the IMR model is designed to be disassembled; it also makes it capable of intermediate assembly configurations. It even includes extra endcaps for the truss segments (for example, the trapezoidal caps for the S1/P1 for the current configuration). Though again, annoyingly enough, none of this is mentioned in the instructions. If you build the model per the instructions, you'll wind up with an "assembly complete" config and a bunch of leftover parts in the box that the instructions don't mention. -- JRF Reply-to address spam-proofed - to reply by E-mail, check "Organization" (I am not assimilated) and think one step ahead of IBM. |
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