[HN Gopher] NASA's helicopter survives first freezing night on Mars
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       NASA's helicopter survives first freezing night on Mars
        
       Author : imagine99
       Score  : 86 points
       Date   : 2021-04-05 20:16 UTC (2 hours ago)
        
 (HTM) web link (edition.cnn.com)
 (TXT) w3m dump (edition.cnn.com)
        
       | BitwiseFool wrote:
       | Does anyone know if Perseverance is capable of recording video? I
       | know it has several cameras but I can't figure out if it can
       | actually record footage of Ingenuity taking flight.
        
         | [deleted]
        
         | pohl wrote:
         | Yes, it is
         | 
         | https://mars.nasa.gov/mars2020/spacecraft/instruments/mastca...
        
           | BitwiseFool wrote:
           | Thank you, for some reason I had a lot of trouble with Google
           | when trying to find this answer. It kept returning results
           | about the video taken by the skycrane, not the rover itself.
        
             | mlyle wrote:
             | Note that most of that video is taken by the rover itself,
             | watching the skycrane fly off etc.
             | 
             | Indeed, we don't have any video from the skycrane after
             | touchdown, because I believe that data was fed over an
             | umbilical to the rover before being sent to the low orbit
             | (I'd typed LEO, but I guess I mean "LMO") satellites and
             | back to Earth.
        
           | aeternum wrote:
           | Have they posted any videos yet? Somewhat disappointing that
           | so far it's only been images with really poor UI/UX via the
           | NASA site. That's not how you capture the public's
           | imagination.
           | 
           | I also don't see why they are waiting so long to do the
           | flight, why risk even waiting until nightfall for the
           | batteries to get too cold or for dust to get into the
           | electronics/mechanics?
        
             | mlyle wrote:
             | > Have they posted any videos yet?
             | 
             | An amazing one. Most of driving along at 1MPH on a barren
             | landscape is incredibly boring, but...
             | 
             | https://youtu.be/4czjS9h4Fpg?t=10
             | 
             | > I also don't see why they are waiting so long to do the
             | flight
             | 
             | Because there's a couple dozen steps that are each
             | irrevocable involved in uncovering, unfolding, deploying,
             | and then flying this thing... and that they want to make
             | sure everything is perfect between each one and that comms
             | still worked before cutting umbilicals, etc, because you
             | can't just plug it back in.
        
             | ghaff wrote:
             | >I also don't see
             | 
             | Maybe, just maybe, the domain experts involved know
             | something you don't. Just a theory.
        
               | BitwiseFool wrote:
               | To be fair, maybe the OP was hoping they'd provide an
               | explanation as to why.
        
         | lgrebe wrote:
         | AFAIK it's possible and will save to an on-rover disk. The
         | current limit to seeing that footage here on earth is the
         | downlink bandwidth limit. So far it's been used for more
         | ,,interesting" data and still images.
        
       | [deleted]
        
       | londons_explore wrote:
       | Making electronics work at a very high or low temperature is a
       | challenge. You normally have to decide between custom-designing
       | all components to work at the extreme temperature, or to figure
       | out how to use off the shelf stuff, yet insulate them from the
       | environmental temperature.
       | 
       | More and more designs are choosing the latter, although notable
       | exceptions are LED light bulbs (which use special components
       | rated to operate for years at ~150 Celcuis)
        
       | maxwoj wrote:
       | "130 degrees Fahrenheit" - seriously? What else, pounds and feet?
        
         | js2 wrote:
         | The article is written for an American audience. We use
         | Fahrenheit here. That said, -130degF is so beyond what any
         | American can relate to, I agree the article should use C and
         | provide the -130degF in a parenthetical. Amusingly, the article
         | does just that later on:
         | 
         | > During the first flight, the helicopter will attempt to rise
         | about 10 feet (3 meters) in the air from the middle of its flat
         | 33-by-33-foot (10-by-10-meter) airfield...
         | 
         | p.s. -90degC
        
           | narrator wrote:
           | One way to relate to it is that -128.6F is the lowest
           | recorded temperature ever on earth.
           | 
           | https://en.wikipedia.org/wiki/Lowest_temperature_recorded_on.
           | ..
        
           | aksss wrote:
           | I think Americans would relate to -90C even less. Many
           | Americans are used to thinking about sub-zero temperatures,
           | it seems less of a burden to conceptualize a really low
           | temperature on the scale you're used to than to conceptualize
           | a really low temperature on a completely different measuring
           | system. The first question most Americans would ask is
           | "What's the equiv of -90 in F?".
        
             | Sharlin wrote:
             | Incidentally, -90degC/-130degF happens to be almost exactly
             | the lowest natural temperature measured on Earth
             | (-89.2degC, in Antarctica in 1982).
        
             | sleavey wrote:
             | Out of curiosity, what do Americans mean when they say
             | "sub-zero"? 0degC or 0degF?
        
               | AnimalMuppet wrote:
               | 0degF.
        
               | ceejayoz wrote:
               | 0degF. "Below freezing" would be below 0degC/32degF.
        
               | js2 wrote:
               | I've never lived anywhere in the U.S. that gets that
               | cold, but in my experience, I don't think Americans say
               | that much, but rather "below freezing" to mean below
               | 0degC/32degF.
               | 
               | I happen to easily remember that 20degC = 68degF and
               | usually use that when mapping the temperatures back and
               | forth which works for the usual ranges where I've had to
               | do so by just adding/subtracting 5/9 on each side.
               | 
               | I once translated literally on the run (running the
               | Boston marathon) for a foreigner who asked about the
               | temperature and got a Fahrenheit response.
               | 
               | When I've been in other countries that use C, I've always
               | had to translate from C back to F in my head to make
               | sense of the temperature. The longest I've ever been any
               | place outside the US is 10 days, and that hasn't been
               | enough time for me to get a feel of what temps are in C.
        
               | JoeAltmaier wrote:
               | 0F of course. We get pretty cold here.
               | 
               | When some youtuber is camping out in 'sub-zero' temps, I
               | smile. We call it 'warm' in Iowa when it gets above
               | freezing in winter.
        
               | js2 wrote:
               | I was hiking on the A.T. one time and it was just a bit
               | above freezing and rainy. My group (all from Florida) was
               | bundled up inside a cabin to get out of the rain. In
               | wandered some other college kids in shorts and tees,
               | soaking wet. They were from Minnesota. I really don't
               | know how they didn't have hypothermia, but I guess you
               | can acclimate to quite a range of temperatures... for a
               | while.
        
       | kshacker wrote:
       | "Survives first freezing night" == Is this just sensationalism?
       | Should NASA not have a good estimate of what the chances of
       | survival are? Maybe it is the media, maybe it is the need to fill
       | columns (like the old days) but I would probably make a list of
       | milestones and track "time to first flight" or something similar.
        
         | [deleted]
        
         | qchris wrote:
         | This is a technology demonstration of a novel robotics system
         | build using many off-the-shelf parts, on a planet with night-
         | time temperatures as low as -130F [1].
         | 
         |  _Ingenuity_ survived, literally, a first freezing night. That
         | is an accomplishment by itself, and is hardly sensationalist.
         | 
         | [1] As linked in the article:
         | https://mars.nasa.gov/technology/helicopter/status/288/its-c...
        
           | mseepgood wrote:
           | > on a planet with night-time temperatures as low as -130F
           | 
           | For anyone reading this: -130F is -90degC
        
         | galacticaactual wrote:
         | It is literally a milestone on a list of milestones.
         | 
         | https://www.jpl.nasa.gov/news/press_kits/mars_2020/launch/mi...
        
           | amelius wrote:
           | I find the order of milestones a little surprising.
           | 
           | Why didn't they test the survival of the freezing cold
           | _after_ testing the rotor blades, lift-off and perhaps a
           | short flight in the vicinity of the rover?
        
             | ceejayoz wrote:
             | They fully expect it to survive the night - it'll have
             | survived identical conditions in pre-launch testing - and
             | thus there's no need to rush through the other steps.
        
             | thelean12 wrote:
             | It's probably as simple as: they didn't have time. You have
             | to move slowly and carefully on Mars. One rushed mistake
             | and it's over.
        
               | amelius wrote:
               | Yes, but chances of getting useful data out of the
               | helicopter are much greater if you test the thing before
               | subjecting it to harsh conditions.
               | 
               | For example: if you know that lift-off works, then that's
               | a huge datapoint.
        
               | thelean12 wrote:
               | I bet they'd move faster if they could. I'm guessing for
               | takeoff there's a good amount of analysis to do
               | beforehand. Terrain, weather, system checks, whatever.
               | 
               | I don't know the actual list, but it's not hard to guess
               | why they couldn't do everything, including ejecting it
               | from the main rover and getting the main rover out of the
               | way, in the ~12-14 hours a day that they have to do
               | stuff.
        
             | jacobreg wrote:
             | They don't want to fly it with the rover nearby. It needs
             | to get to a safe distance before they can fly it.
        
           | whimsicalism wrote:
           | Wow, reading the first comment I would think that this was
           | planned. It literally is the third thing on a list of
           | "milestones."
        
         | ortusdux wrote:
         | 2/3rds of Ingenuity's stored energy goes towards keeping its
         | batteries and critical components warm each night. Only 1/3rd
         | is available for powered flight. It literally takes more energy
         | for this helicopter to survive the night than it takes to fly
         | on mars.
        
           | arrosenberg wrote:
           | That's pretty interesting. Maybe the next rover needs an
           | excavator tool so we can build an underground hidey-hole for
           | storing sensitive equipment at night.
        
           | namrog84 wrote:
           | I'm not sure how to really internalize this.
           | 
           | Does it take a ton of power to heat. Or does it take very
           | little power to fly?
           | 
           | I'd assume there is a ton of effort put into passive
           | insulation? Since my non intuitive gut seem like it should be
           | able to better insulate heat loss. I can't help but feel like
           | there is probably a ton of effort and science to insulate.
           | And this is even only possible because of that work. But is
           | it just a much harder problem than I probably realize?
        
             | danaliv wrote:
             | On the aerodynamic side, this aircraft has a mass of 1.8 kg
             | / 4 lbs, which is an equivalent weight of 0.7 kg / 1.5 lbs
             | on Mars. That is also the force required to maintain
             | altitude. Imagine picking up four or five apples; that's
             | what we're talking about as a minimum to stay in the air.
             | For comparison, a DJI Phantom weighs 3 lbs, and a Mavic
             | comes in at 2 lbs.
             | 
             | I can't find numbers on the power system or materials so I
             | can't speak to the thermal side or how much flight time
             | that affords.
             | 
             | EDIT: Apparently there's enough energy to fly for 90
             | seconds (!) per sol.
        
             | HPsquared wrote:
             | Mars is very cold, things like the battery can't handle
             | these temperatures. It's been thoroughly analysed, here is
             | a quote from the white paper [0]:
             | 
             | """H. Thermal System
             | 
             | The helicopter must survive the cold of the night on Mars
             | where temperatures can drop to -100 C or lower. The most
             | critical component is the battery which is kept above -15 C
             | through the night as it powers Kapton film heaters attached
             | to the battery cells. The avionics boards in the ECM
             | surround the battery and are also kept at an elevated
             | temperature by virtue of their proximity to the warm
             | battery assembly. Insulation around the avionics boards is
             | provided by a carbon-dioxide gap of 3 cm width. Additional
             | insulation can be provided by replacing the carbon-dioxide
             | gas with an Aerogel formulation. The outermost fuselage
             | thermal coating is from Sheldahl with Solar absorptivity a
             | = 0.8 and infra-red (IR) emissivity  = 0.1.
             | 
             | In addition to thermal losses through the gas gap (or
             | aerogel), additional losses occur due to conduction in the
             | mast as well as through the copper wiring that penetrate
             | the ECM from the mast. To minimize the latter, the wire
             | gauges are selected to be of the thinnest gauges that can
             | still support the current draw during operations without
             | overheating. Prior to flight, under the control of the
             | FPGA, the thermal system powers on heaters in the motor
             | control boards that have been exposed to the ambient
             | temperatures. The internal battery temperature is brought
             | up to 5 C to allow hi-power energy extraction from the
             | cells. During operation the ECM and battery warm up as a
             | result of avionics operations and battery self-heating.
             | However, the thermal inertia of the elements is such that
             | for the short flights of the helicopter, there is no
             | overheating."""
             | 
             | [0] "Mars Helicopter Technology Demonstrator" https://rotor
             | craft.arc.nasa.gov/Publications/files/Balaram_A...
             | 
             | EDIT: some detail on the battery capacity from section G:
             | 
             | "A de-rated end-of-life battery capacity of 35.75 Wh is
             | available for use. Of this capacity, 10.73 Wh (30%) is kept
             | as reserve, night-time survival energy usage is estimated
             | at 21 Wh for typical operation in the northern latitudes in
             | the spring season, and approximately 10 Wh is available for
             | flight. Assuming that 20% of the power is at the peak load
             | of 510 W and 80% is at a continuous load of 360 W,
             | approximately 90 sec of flight is possible. These energy
             | projections represent conservative worst-case end-of-
             | mission battery performance at 0 C initial temperature.
             | More moderate power loads will extend the flight time."
        
             | ortusdux wrote:
             | On top of what others have said, we need advancement it
             | batteries that can withstand low temperatures. Lithium ion
             | batteries generally need to be kept above freezing temps.
             | There have been some advances in capacitors that operate
             | down to -100C, but their energy density makes them a non-
             | ideal option for weight limited applications.
             | 
             | This video from Veritasium does a good job of covering the
             | helicopter power system:
             | https://www.youtube.com/watch?v=GhsZUZmJvaM&t=613s
        
             | InitialLastName wrote:
             | -130F/-90C is VERY cold, and this system is VERY weight-
             | sensitive. Presumably adding more insulation that always
             | needed to be carried was more weight than adding power
             | capacity that can serve a dual-use.
             | 
             | The power capacity metric isn't necessarily concurrent; one
             | could imagine the chopper using its power to fly (which
             | will generate heat as a byproduct) for a third of the
             | sunlight time, and then using the rest of the day to charge
             | for the night-time cold.
        
               | p1mrx wrote:
               | > one could imagine the chopper using its power to fly
               | (which will generate heat as a byproduct) for a third of
               | the sunlight time
               | 
               | This is impossible; the flight duration is ~ 90 seconds.
        
         | spuz wrote:
         | No it's not - firstly, you can go to JPL's version of the story
         | here and see how they lead with the same headline:
         | 
         | https://www.jpl.nasa.gov/news/nasas-mars-helicopter-survives...
         | 
         | But I prefer to hear it directly from the engineers involved:
         | 
         | > "What was it like seeing that first image of Ingenuity on
         | mars?"
         | 
         | > "Oh it was a dream come true. To see the culmination of the
         | entire team's hard work really pay off. Being dropped - that's
         | one huge milestone, but the _massive_ one for us over the last
         | few days has been realising not only did we drop, but we
         | actually survived the first night. That is huge. That was one
         | of the huge huge achievements that we 've been looking forward
         | to and now we can look forward to the rest of the mission. But
         | being able to drop under our own energy, sustain ourselves,
         | keep ourselves warm through the whole night and then wake up
         | and talk with Perseverance and say "yep we're here alive and
         | healthy" the team couldn't be happier."
         | 
         | https://youtu.be/PcpI8-S5ZE8?t=108
        
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