Quote from: docmordrid on 06/09/2014 03:23 amIf you look closely at the outer rim of pic #3 there's what looks like a white O-ring type seal, and I'd bet that thick black band is part of an inflatable pressure seal. Seen those before in isolation and biohazard labs. 'Inflatable seal (or gasket) door'. Also dynamic seal. IIRC they can also be used in water-tight hatches for marine applications. In this application those are likely the passive side seals with the inflatable active side seals in the door frame. Easier to plumb the gas supply there.Once those seals inflate it's going absolutely nowhere, locked tight as a drum - with or without locking pawls. Ditto for any gas flow.I've used inflatable seals for both underwater robots and pressure suit entry mechanisms. They work well if you can continually pressurize them, but are a potential source of leaks. They also aren't all that solid if loaded in shear, since they are made of elastomers. Even assuming they're using an 8.3 psi cabin pressure, it's still about 3500 pounds of force trying to open the door. I definitely think you would absolutely want mechanical latches, even with an inflatable seal.
If you look closely at the outer rim of pic #3 there's what looks like a white O-ring type seal, and I'd bet that thick black band is part of an inflatable pressure seal. Seen those before in isolation and biohazard labs. 'Inflatable seal (or gasket) door'. Also dynamic seal. IIRC they can also be used in water-tight hatches for marine applications. In this application those are likely the passive side seals with the inflatable active side seals in the door frame. Easier to plumb the gas supply there.Once those seals inflate it's going absolutely nowhere, locked tight as a drum - with or without locking pawls. Ditto for any gas flow.
Quote from: justineet on 06/08/2014 01:19 amAnother reason they [Orion team] stated was touch screen would be difficult to use with space glove on. Would like to see how well astronauts can operate the screen via simulation to find out the real deal.Easy. There is no reason that space gloves can't have inductive fingertips.I have seen people wearing such gloved fingertips, to keep fingerprints off the screen.They work great.Legacy equipment mindset looses another one.
Another reason they [Orion team] stated was touch screen would be difficult to use with space glove on. Would like to see how well astronauts can operate the screen via simulation to find out the real deal.
Quote from: justineet on 06/08/2014 01:19 amAnother reason they [Orion team] stated was touch screen would be difficult to use with space glove on. Would like to see how well astronauts can operate the screen via simulation to find out the real deal.And what about a situation like the Apollo 12 "Try SCE to aux"? It is true there are some mechanical emergency switches, but what if something like that happens? Would an astronaut be able to quickly and correctly press a switch, or a sequence of switches, with the cabin under high vibration or high-g accelerations, also if bare handed?Just a question. Obviously they must have considered this situation.
There are manual emergency switches for all vital systems.
Operational hatch handle will likely resemble aircraft exterior doors, like this:
So, ok: time passed and system engineering is much more refined today. But I wonder how they will manage the copious unpredictable procedures that may be required through a touch-screen in high stress situations.Again, obviously they must have managed this. I wonder HOW.
Even in my experience from the 1980s, there were a number of technologies to chose from for touch technology including multi-layer contact based film systems, acoustic (sound based), capacitive/resistive (based on changes in electrical properties on a grid), and IR based (breaking the beams which required a deep frame around the panels).
Quote from: Garrett on 06/03/2014 08:23 amAlso, it's bad practice, in my opinion, to have the O2 and CO2 levels indicated on 0 - 100% scales. A quick search on the web shows that, from a health perspective, O2 should be between 19% and 24% and CO2 should be less than 0.6%. The indicators should be scaled accordingly.O2 and CO2 figures listed are in the ranges you indicated as normal.
Also, it's bad practice, in my opinion, to have the O2 and CO2 levels indicated on 0 - 100% scales. A quick search on the web shows that, from a health perspective, O2 should be between 19% and 24% and CO2 should be less than 0.6%. The indicators should be scaled accordingly.
...(Oh, and the "deep frame" is only about 1/8". Here's a picture -- note that the touchscreen part is *not* the white bezel, it's the black (IR filter) plastic between that and the screen.)
Quote from: Elmar Moelzer on 06/09/2014 04:16 pmThere are manual emergency switches for all vital systems.Thanks Elmar. Yes, I know (and I wrote that) there are manual switches. But was for example the SCE switch on the CM considered vital at the time? I don't think so, and in fact neither Pete Conrad or anyone else in the MC or on board except Aaron and Bean remembered about that: the abort switch was the actual "emergency switch", at least for that situation.So, ok: time passed and system engineering is much more refined today. But I wonder how they will manage the copious unpredictable procedures that may be required through a touch-screen in high stress situations.Again, obviously they must have managed this. I wonder HOW.
Oh ye of little faith; hast thou not viewed process control from a modern software engineering paradigm?Go now an contemplate the appropriate button for the blue screen of woe and have faith in the systems engineers.
What you prefer? Metal on metal seals?
He said "Most of what you see here is flight hardware." (emphasis mine). Do we really have to have 18 pages filled with pointless speculation on things like pressure seals being absent from the hatch of a mostly flight hardware new Dragon V2?
In my previous job we brought a children's laptop with an IR-based touchscreen to production. IR-based touchscreens went through some exciting technology development recently; some versions of the kindle use them, for example. They are very good for gloved/ungloved use, and with various size "touch points". In our application it was also a plus that they are very robust in the face of kids using them with sticky fingers, splashing stuff on the screens, etc. They are also easy to integrate because the touch sensing mechanism doesn't have to be transparent and sandwiched in front of the visual display.
Testing, obviously. Even "unpredictable" situations are usually a combination of known procedures. They have astronauts on staff, who probably spend a lot of time running simulated failures of various kinds. Consider that the procedures checklist on shuttle often involved typing inscrutable digit combinations into a manual keypad. It's not too different from hitting different buttons on an on-screen display. The important thing is *practice* and muscle-memory, so that the behavior is automatic. The cognitive load isn't all that different.
Will the touchscreen monitors survived and be touchable during vacuum environment at very low temp if they had to open the hatch to go EVA from the Dragon V2 in the distant future?
Quote from: Jdeshetler on 06/10/2014 12:52 amWill the touchscreen monitors survived and be touchable during vacuum environment at very low temp if they had to open the hatch to go EVA from the Dragon V2 in the distant future?Why do you think the temperature on the cockpit should go so low under vacuum in normal operating conditions?
A piece of bare metal in space, under constant sunlight can get as hot as two-hundred-sixty (260) degrees Celsius. And yet, in the shade, an object will cool down to below -100 degrees Celsius.http://www.universetoday.com/77070/how-cold-is-space/
You worked on OLPC[2]? That's AWESOME.
cscott, do you think that obviously you can reproduce any fault that requires split seconds intervention and save the mission by pressing one of the 30 (I counted them) buttons available in the V2 main console without having to push the "abort" one (if exists) at the first real malfunction in a critical situation?
Quote from: Lar on 06/09/2014 11:22 pmYou worked on OLPC[2]? That's AWESOME.Yup. @jg is hanging around these parts, he's an OLPC alumnus as well.Quote from: Jdeshetler on 06/10/2014 12:52 amWill the touchscreen monitors survived and be touchable during vacuum environment at very low temp if they had to open the hatch to go EVA from the Dragon V2 in the distant future?No physical reason why they cannot be. Assuming they are LED (not LCD), it's all just solid state transistors and some transparent plastics. (For our part, we only rated our machines down to "walking to school in outer Mongolia" temperatures.)Quote from: pagheca on 06/10/2014 01:53 amcscott, do you think that obviously you can reproduce any fault that requires split seconds intervention and save the mission by pressing one of the 30 (I counted them) buttons available in the V2 main console without having to push the "abort" one (if exists) at the first real malfunction in a critical situation? I'm not sure what point you're trying to make. Finding the "right" switch in the maze of of a 787 -vs- drilling down on a touchscreen right in front of you? Comparing the severity of "touchscreen failure" in a Dragon v2 -vs- in a F-35? Or are you just upset that the computer is likely to be better at reacting to and flying failure modes than a human pilot?
I'm not sure what point you're trying to make. Finding the "right" switch in the maze of of a 787 -vs- drilling down on a touchscreen right in front of you? Comparing the severity of "touchscreen failure" in a Dragon v2 -vs- in a F-35? Or are you just upset that the computer is likely to be better at reacting to and flying failure modes than a human pilot?