Who knew this is how exciting the future would be: Snapchat in space! Maybe they could make the claim of "First app used by a human in a vacuum and micro-gravity".
All the startups in Silicon Valley are vying for that. /s
So I assume the starliner has touch screens too, when I saw those on the Dragon Crew I thought "Gee how are they going to use those in gloves?" Sking and trying to use your phone is challenging this is just flying through space :-).
While not EVA suits they presumably work during a depressurization event so I wonder if they are candidates for mars suits.
They make ski under-gloves with touchscreen tips. I desperately needed under-gloves once and ended up buying the super-expensive kind from the store at the resort, they worked well with an iPhone.
Resistive touch screens still exist, and would probably still be preferable from a reliability point of view (I have all kinds of troubles with capacitive screens when there's sweat, humidity, low temperatures, etc)
Oddly I've found resistive touchscreens to be less reliable but anecdotes are not data so it could just be I'm unlucky.
One of the interesting things I also find is that using a touch screen on CalTrain while it bounces around is difficult, I can't imagine what it will be like to hit the correct control button on the touch screen of a rocket under boost.
I can think of at least one edge case where things might be different.
Emergency re-entry, time to put on your suit, but everyone else is dead.
But anyway, I'm just saying it would be interesting to know why certain design decisions were made, what trade-offs were considered, requirement constraints.
Saying something like you reckon they didn't think of that doesn't add to the conversation.
Sure they thought about... anyone knows the reason for that? I see 1 case in which it would be fast to dress up (emergency reentry, as TheSpiceLife said ..see [0]) and 2 to take it as fast as possible (toilet emergency and support system failure)..
Well, with all respect, a 1000 people thinking about a single point doesnt mean much.. we unfortunately saw catastrophic events caused by apparent single failures..
I think it's generally agreed upon that the Space Shuttle program was needlessly wasteful and more PR- than science-driven. A heavy space plane has zero advantages over a capsule for most work done in LEO. It's good to see this renewed focus on more practical designs.
(If that's incorrect and you're qualified to correct me please do.)
Having said that, the name Starliner writes a check that a manned capsule won't ever be able to cash. This is the first time I've heard of Boeing's Starliner and it got me really, really excited until I pulled up a picture of it. They really should have picked a less grandiose name.
Shuttle flew a decent number of missions for the National Reconnaissance Office, conducting secret experiments and deploying spy satellites. Most of the missions are still classified, but many folks have said the military needs drove the design of the Shuttle program. There are pretty obvious advantages to a spaceplane if your goals include capture of enemy satellites. http://www.space.com/34522-secret-shuttle-missions.html
It turns out a lot of science space research is heavily driven by military space presence. For example, Hubble has a 2.4m mirror because there was already a factory making that size for dozens of spy satellite. https://en.wikipedia.org/wiki/KH-11_Kennen
And ever heard of "The Dish" at Stanford? It's a 150-foot radio telescope the US Air Force funded during the Cold War to ostensibly "study the chemical composition of the atmosphere." Total BS. The Air Force built it to intercept signals from Soviet radar systems after they bounced off the moon.
(Thankfully Stanford got to keep it and it's been used for hundreds of projects since then.)
Retrieval of objects in space and bringing them back to Earth is about the only mission where the Space Shuttle was superior to capsule designs. This was also used in a handful of science missions for studying long-term exposure of various materials.
But the vast majority of the Shuttle's 130 flights would have been better served by an Apollo or Gemini derived design.
From what I've read, Shuttle also did quite a bit of satellite repair (like fixing Hubble). And the orbiter's cargo bay certainly was useful to transport many parts of the ISS.
The Department of Defense still actively uses a spaceplane-ish vehicle. It's just a much smaller unmanned one called the X-37b. Many folks speculate it's used to repair and refuel spy satellites, and potentially even rendezvous with and and hack enemy satellites. https://en.wikipedia.org/wiki/Boeing_X-37
Generally I totally agree though-- capsule design makes way more sense for anything leaving or reentering atmosphere. The upcoming Orion are clearly in that directly.
> From what I've read, Shuttle also did quite a bit of satellite repair (like fixing Hubble)
It did, but a capsule can do the job just fine too – for JWST, it is (or was) planned to do repairs using the Orion capsule and a mission module docked to it.
> And the orbiter's cargo bay certainly was useful to transport many parts of the ISS.
Kinda, yes. But an unmanned rocket could have done the same job, and likely cheaper than the Shuttle.
Most of the civilian Shuttle missions could have been easily served by other, much cheaper craft – but who knows what happened during the classified ones, it might actually have been cheaper to the taxpayer at large (if not NASA) to have one craft to serve both roles.
> The Department of Defense still actively uses a spaceplane-ish vehicle. It's just a much smaller unmanned one called the X-37b. Many folks speculate it's used to repair and refuel spy satellites, and potentially even rendezvous with and and hack enemy satellites. https://en.wikipedia.org/wiki/Boeing_X-37
We don't really know, but given how little fuel capacity it has and how long it stays in orbit, it's more likely that the DoD's stated purpose of long-endurance testing of new spy hardware is true.
If the rumor is that it's being used to refuel satellites, there are two considerations:
1. Can it get to many satellites? Yes, it has good delta V, though I think you're mixing the X-37's delta V with its boosters and the delta V of the Shuttle orbiter without its SRBs and external tank.
2. Can it carry fuel for those satellites? No, not much. The X-37 has a maximum total takeoff weight of 5000 kg, while the Shuttle can get 27000 kg to LEO. Unfortunately, only one X-37 will fit in the payload bay of the Shuttle, so we can't actually lift five X-37s in the Shuttle.
Many large satellites weigh more than the X-37's total mass. The biggest individual consumer, the ISS, requires about 7000 kg of fuel annually to stay in orbit. A KC-135 in-air refueling tanker is much faster than an oceangoing supertanker, but you wouldn't use the former to empty an oil rig!
The ISS needs that much fuel to boost it's altitude due to drag in LEO. But the refueling of satellites by the X-37 is hypothesized to be at much higher altitudes where there is very little drag.
These satellites don't need altitude boosts-- they use propellant for orbital changes (e.g. to "re-task" a spy satellite to a new region). But instead of chemical rockets they often use xenon gas ion engines.
The key thing with ion drives is their "specific impulse." High-thrust chemical rockets are needed to get out of the atmosphere and perform fast burns, but ion engines are often >10x more efficient once already in orbit. And because there isn't a chemical reaction, there is less corrosion and they can last for years.
Refueling xenon for the ion drives of spy satellites would double or triple their mission lifespan. They don't need much -- maybe just a couple hundred kg. And this could literally save billions of dollars since these satellites are so expensive to build.
Where have you gotten that from? The only numbers I can find for observed Δv changes are some 100m/s for USA-212, which is a third of the OMS' rated 300m/s with a full cargo bay.
For one thing, the X-37 Wikipedia page states that a design goal was 3.1 KM/s Delta-V. That's about as official a number as I'm finding online (blah blah Wikipedia source), but there are quite a few people who track these things in the sky. Each orbital inclination or altitude change requires a minimum delta V to execute, and we can observe the results of these maneuvers here on Earth. Online arguments about the X-37 delta-V are inconclusive, we'll leave it at that!
I'm pretty sure we're not going to send any capsule to repair the JWSP. It's going to be at L2 which is 1 million miles away from Earth, or about 3x furthest than mankind has ever traveled. It would take weeks to get there.
The shuttle was also great for anything that required an EVA, and could handle multiple EVAs on a single mission. It could also stay in orbit with a large crew for extended periods.
Those old boats had capabilities that I don't think we'll see for another two generations of manned spacecraft.
> The shuttle was also great for anything that required an EVA, and could handle multiple EVAs on a single mission.
Gemini, Vokshod, Apollo and Soyuz all demonstrated that ability as well. Apollo especially with multiple lunar EVAs per mission.
The Shuttle's biggest advantage over all those was being roomier, making EVA preparations less of a hassle, but all space craft currently in development are addressing that shortcoming.
> It could also stay in orbit with a large crew for extended periods.
Meh. Yes, it could… but should it? In that role, the Shuttle was still inferior to a real space station, while being as expensive. If it wasn't for political reasons (Shuttle was approved, but it was hard to fund anything else), NASA likely would have preferred using a space station for it (and largely did, once it could access Mir/ISS).
ISS isn't going away for a while yet, the industry is working on smaller private space stations that could be rented out for this purposes, and NASA is contemplating building smaller stations in deep space when/if necessary. We didn't actually lose any capability.
Important to note that the Shuttle did not require cabin depressurization to EVA, it had an airlock. None of those other vehicles could keep the cabin pressurized during an EVA (I'm not sure about Soyuz, for that matter).
There's a difference between the shuttle being used for certain missions and the shuttle being necessary for those missions.
(and then going up a level, whether those missions were necessary to establish those capabilities or if different missions would have been used in the absence of the shuttle)
Keep in mind it was NOT an all or nothing proposition for using the Shuttle. We launched satellites while the shuttle was running using Titan, Atlas, and Delta rockets. I would imagine if it was more cost efficient to use those rockets, they would have done so.
Regarding Hubble, the intelligence community knew of significant design flaws in Hubble based on their experience with similar hardware, and did not communicate the problems to the Hubble team, for security reasons. This was much more about solar array flex and the Southern Magnetic Anomaly (high radiation zone that is often transited by Hubble, and which tends to crash the processors running the scope); the mirror flaw wasn't known by the TLAs.
The book _The Hubble Wars_, which describes most of this, made me pretty angry that an important scientific instrument was nearly crippled by the "national security" mindset.
One thing that the Space Shuttle had going for it was that it could be used as a Canadarm[1] platform. Bringing the arm back home in one piece was handy, and the orbiter's huge mass probably made it easier to reason about the physics involved.
It's important to note the space shuttle was a poor design in large part because it added a lot of cargo on a man rated system. 1 failure to achieve orbit in 135 missions is an outstanding record, but very wasteful when sending cargo. A capsule seems better in large part because it does not.
Further, if the shuttle was only sending people to orbit it's design could be both reusable and vastly simpler because of vastly lower rentry temperatures and more redundancy.
Considering that the Buran program was much less active and only had a single launch, the ROI on that wastage seems like it would have been rather low.
> (If that's incorrect and you're qualified to correct me please do.)
You're not wrong but there are some nuances. The original design for the shuttle was very different from what was ultimately built because when the Shuttle program funding was in jeopardy the Air Force was brought in and they forced the design to change to meet their needs. The shuttle got bigger and added the external fuel tank, almost entirely crippling the shuttle's reusability.
By far the most negative impact on the shuttle was the massive reduction in space flights from the he original proposal due to budget cuts and Congressional politicking. The average cost per flight was something on the order of $1.8 billion but most of that was fixed overhead and a lot of that overhead was the consequence of the Air Force redesign. If the shuttle were funded independently as originally planned, it would have cost a lot less to fly and with enough flights it would have been significantly more cost effective. Whether NASA could make it as cheap as rockets is unclear but it's not impossible that they could have brought it within a factor of two.
However, it's also unclear to me whether we could have pulled off something like the Hubble telescope repair with a rocket and pods.
These are still not very cool. Why is there such a big disconnect between Hollywood movies, and these real space suits? I mean, even the shade of blue isn't particularly nice. If this was a toy, I don't think it would sell very well.
I know it doesn't really matter and the function is far more important than the aesthetics. But still... can they hire some of these Hollywood guys?
Because Hollywood movies are not generally based in, you know, reality. They're meant to be flashy and futuristic because that is what the audience expects in sci-fi movies. Real life isn't flashy and futuristic, though, and there's a lot of requirements to the suits which aren't super exciting.
So, yknow, good thing it's not a toy but a functional piece of clothing that's supposed to help astronauts do their job.
Design is completely subjective. Those Z series suits you linked look like a buzz light year costume.
I think these suits (Boeings) look fine, Boeing is just absolutely terrible at marketing. The giant image with "Tailored for Starliner" looks like it's from the 90's.
They don't say much about how well these suits can work. Are the just for protection or do they actually enable human functionality in space?
Zipper on the back? I sure hope they have a rope you can use to pull it up your back. This sounds like one of those design details that movies use as plot points.
For example, on a space station a disaster depressurizes a central capsule. A single astronaut is trapped with a suit on one end of the stations and because of a zipper at the back of the suit cannot be rescued.
The shoes are Reeboks, not Nikes. I'm not even kidding: http://www.boeing.com/space/starliner/ (scroll down to the suit and click the plus next to the shoe)
What is the benefit of having the helmet attached to the suit directly instead of detachable like the existing suits? If I was spending months in one of these aboard the space station, I think I would prefer to not have the helmet flopping around behind me all the time.
You don't need to wear a space suit aboard the space station. These suits are worn mostly just during launch and returning to the surface - a few hours or a couple of days at a time.
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[ 3.7 ms ] story [ 174 ms ] threadSo... has anyone rocked some snapchat during a spacewalk yet?
All the startups in Silicon Valley are vying for that. /s
While not EVA suits they presumably work during a depressurization event so I wonder if they are candidates for mars suits.
One of the interesting things I also find is that using a touch screen on CalTrain while it bounces around is difficult, I can't imagine what it will be like to hit the correct control button on the touch screen of a rocket under boost.
In which case the zipper is definitely in the least practical place.
Anyway, it's an interesting question that possibly has some story to it which would be interesting to hear.
Argh! How would we even know it's in the least practical place? Is it because you don't put on your coat that way?
These things are not designed with the same constraints. Getting into a space suit is a slow deliberate process, with people there to help.
Emergency re-entry, time to put on your suit, but everyone else is dead.
But anyway, I'm just saying it would be interesting to know why certain design decisions were made, what trade-offs were considered, requirement constraints.
Saying something like you reckon they didn't think of that doesn't add to the conversation.
[0] https://en.m.wikipedia.org/wiki/Soyuz_11
(If that's incorrect and you're qualified to correct me please do.)
Having said that, the name Starliner writes a check that a manned capsule won't ever be able to cash. This is the first time I've heard of Boeing's Starliner and it got me really, really excited until I pulled up a picture of it. They really should have picked a less grandiose name.
It turns out a lot of science space research is heavily driven by military space presence. For example, Hubble has a 2.4m mirror because there was already a factory making that size for dozens of spy satellite. https://en.wikipedia.org/wiki/KH-11_Kennen
And ever heard of "The Dish" at Stanford? It's a 150-foot radio telescope the US Air Force funded during the Cold War to ostensibly "study the chemical composition of the atmosphere." Total BS. The Air Force built it to intercept signals from Soviet radar systems after they bounced off the moon.
(Thankfully Stanford got to keep it and it's been used for hundreds of projects since then.)
But the vast majority of the Shuttle's 130 flights would have been better served by an Apollo or Gemini derived design.
The Department of Defense still actively uses a spaceplane-ish vehicle. It's just a much smaller unmanned one called the X-37b. Many folks speculate it's used to repair and refuel spy satellites, and potentially even rendezvous with and and hack enemy satellites. https://en.wikipedia.org/wiki/Boeing_X-37
Generally I totally agree though-- capsule design makes way more sense for anything leaving or reentering atmosphere. The upcoming Orion are clearly in that directly.
It did, but a capsule can do the job just fine too – for JWST, it is (or was) planned to do repairs using the Orion capsule and a mission module docked to it.
> And the orbiter's cargo bay certainly was useful to transport many parts of the ISS.
Kinda, yes. But an unmanned rocket could have done the same job, and likely cheaper than the Shuttle.
Most of the civilian Shuttle missions could have been easily served by other, much cheaper craft – but who knows what happened during the classified ones, it might actually have been cheaper to the taxpayer at large (if not NASA) to have one craft to serve both roles.
> The Department of Defense still actively uses a spaceplane-ish vehicle. It's just a much smaller unmanned one called the X-37b. Many folks speculate it's used to repair and refuel spy satellites, and potentially even rendezvous with and and hack enemy satellites. https://en.wikipedia.org/wiki/Boeing_X-37
We don't really know, but given how little fuel capacity it has and how long it stays in orbit, it's more likely that the DoD's stated purpose of long-endurance testing of new spy hardware is true.
1. Can it get to many satellites? Yes, it has good delta V, though I think you're mixing the X-37's delta V with its boosters and the delta V of the Shuttle orbiter without its SRBs and external tank.
2. Can it carry fuel for those satellites? No, not much. The X-37 has a maximum total takeoff weight of 5000 kg, while the Shuttle can get 27000 kg to LEO. Unfortunately, only one X-37 will fit in the payload bay of the Shuttle, so we can't actually lift five X-37s in the Shuttle.
Many large satellites weigh more than the X-37's total mass. The biggest individual consumer, the ISS, requires about 7000 kg of fuel annually to stay in orbit. A KC-135 in-air refueling tanker is much faster than an oceangoing supertanker, but you wouldn't use the former to empty an oil rig!
These satellites don't need altitude boosts-- they use propellant for orbital changes (e.g. to "re-task" a spy satellite to a new region). But instead of chemical rockets they often use xenon gas ion engines.
The key thing with ion drives is their "specific impulse." High-thrust chemical rockets are needed to get out of the atmosphere and perform fast burns, but ion engines are often >10x more efficient once already in orbit. And because there isn't a chemical reaction, there is less corrosion and they can last for years.
Refueling xenon for the ion drives of spy satellites would double or triple their mission lifespan. They don't need much -- maybe just a couple hundred kg. And this could literally save billions of dollars since these satellites are so expensive to build.
https://en.wikipedia.org/wiki/Specific_impulse#Examples
Those old boats had capabilities that I don't think we'll see for another two generations of manned spacecraft.
Gemini, Vokshod, Apollo and Soyuz all demonstrated that ability as well. Apollo especially with multiple lunar EVAs per mission.
The Shuttle's biggest advantage over all those was being roomier, making EVA preparations less of a hassle, but all space craft currently in development are addressing that shortcoming.
> It could also stay in orbit with a large crew for extended periods.
Meh. Yes, it could… but should it? In that role, the Shuttle was still inferior to a real space station, while being as expensive. If it wasn't for political reasons (Shuttle was approved, but it was hard to fund anything else), NASA likely would have preferred using a space station for it (and largely did, once it could access Mir/ISS).
ISS isn't going away for a while yet, the industry is working on smaller private space stations that could be rented out for this purposes, and NASA is contemplating building smaller stations in deep space when/if necessary. We didn't actually lose any capability.
(and then going up a level, whether those missions were necessary to establish those capabilities or if different missions would have been used in the absence of the shuttle)
https://en.wikipedia.org/wiki/List_of_Titan_launches and https://en.wikipedia.org/wiki/Delta_IV and https://en.wikipedia.org/wiki/Atlas_V
The book _The Hubble Wars_, which describes most of this, made me pretty angry that an important scientific instrument was nearly crippled by the "national security" mindset.
[1] https://en.wikipedia.org/wiki/Canadarm
Further, if the shuttle was only sending people to orbit it's design could be both reusable and vastly simpler because of vastly lower rentry temperatures and more redundancy.
Soviets decided to replicate it. So even if it was PR, it was a good PR - it managed to trick USSR to waste quite an effort.
You're not wrong but there are some nuances. The original design for the shuttle was very different from what was ultimately built because when the Shuttle program funding was in jeopardy the Air Force was brought in and they forced the design to change to meet their needs. The shuttle got bigger and added the external fuel tank, almost entirely crippling the shuttle's reusability.
By far the most negative impact on the shuttle was the massive reduction in space flights from the he original proposal due to budget cuts and Congressional politicking. The average cost per flight was something on the order of $1.8 billion but most of that was fixed overhead and a lot of that overhead was the consequence of the Air Force redesign. If the shuttle were funded independently as originally planned, it would have cost a lot less to fly and with enough flights it would have been significantly more cost effective. Whether NASA could make it as cheap as rockets is unclear but it's not impossible that they could have brought it within a factor of two.
However, it's also unclear to me whether we could have pulled off something like the Hubble telescope repair with a rocket and pods.
I know it doesn't really matter and the function is far more important than the aesthetics. But still... can they hire some of these Hollywood guys?
I think Elon Musk has the right idea: http://www.dailymail.co.uk/sciencetech/article-3573869/Elon-...
I do think these NASA suits are getting better, though: https://en.wikipedia.org/wiki/Z_series_space_suits
So, yknow, good thing it's not a toy but a functional piece of clothing that's supposed to help astronauts do their job.
Flashy lights and colors will most likely distract the astronauts in flight.
Why do you think there is big announcement, press event if not for PR?
I think these suits (Boeings) look fine, Boeing is just absolutely terrible at marketing. The giant image with "Tailored for Starliner" looks like it's from the 90's.
For the same reasons there's sound in space in movies but not in real life.
Zipper on the back? I sure hope they have a rope you can use to pull it up your back. This sounds like one of those design details that movies use as plot points.
For example, on a space station a disaster depressurizes a central capsule. A single astronaut is trapped with a suit on one end of the stations and because of a zipper at the back of the suit cannot be rescued.
That's more important than the color of the suit.