Author Topic: NASA - Europa Clipper updates and discussion  (Read 405520 times)

Offline vjkane

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Re: Europa Clipper
« Reply #20 on: 03/13/2019 04:37 pm »
Yet to me not to expect discussion of the launchers on a forum mostly dedicated to such technology seems a odd stance to take.
Too often discussions of launchers in the science forums has gone the way of thinking about what ifs, "if we do multiple launches and stack elements in orbit..."  These are fine discussions and there are boards to vet and debate these kinds of issues.  However, they are outside the realm of options being considered by the project teams.  I believe that the discussions on the science board should be among the options being considered by the project teams.

So I support discussions of the implications of different commercial launches here, whether ice giant missions should have SEP stages, etc., in the science boards.

I write this knowing that the head of NASA has just suggested in orbit stacking of elements for the first Orion moon launch.  That now makes this legitimate to discuss on the Orion, SLS, and Falcon Heavy boards.


Offline Star One

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Re: Europa Clipper
« Reply #21 on: 03/14/2019 06:41 am »
Yet to me not to expect discussion of the launchers on a forum mostly dedicated to such technology seems a odd stance to take.
Too often discussions of launchers in the science forums has gone the way of thinking about what ifs, "if we do multiple launches and stack elements in orbit..."  These are fine discussions and there are boards to vet and debate these kinds of issues.  However, they are outside the realm of options being considered by the project teams.  I believe that the discussions on the science board should be among the options being considered by the project teams.

So I support discussions of the implications of different commercial launches here, whether ice giant missions should have SEP stages, etc., in the science boards.

I write this knowing that the head of NASA has just suggested in orbit stacking of elements for the first Orion moon launch.  That now makes this legitimate to discuss on the Orion, SLS, and Falcon Heavy boards.

My fear is it could drive the thread being split between science and launcher and discussion and I am not sure that’s particularly desirable.

Offline Kesarion

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Re: Europa Clipper
« Reply #22 on: 03/19/2019 12:02 pm »
https://www.lpi.usra.edu/opag/meetings/mar2019/Findings.pdf

Here’s a recent report from OPAG which also addresses the recent termination of ICEMAG. I’m surprised to find out that the cancellation of certain risky instruments seems to be new process and I am pleased to see others call for transparency regarding this new approach towards keeping science missions within their cost caps.

However, I’m not sure that alluding to possible sex-based discrimination is the most professional or wise thing to do when calling for said transperancy, especially when you consider that the current acting director of the planetary division is a woman. ???
« Last Edit: 03/19/2019 12:52 pm by Kesarion »

Offline su27k

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Re: Europa Clipper
« Reply #23 on: 03/20/2019 03:07 am »
More interesting to me is the fact that we have often been told in this section of the forum that a launch cost saving of $10M to $20M doesn't matter to science missions, since it's a tiny fraction of the total mission cost. Yet here we have an important instrument on a multi-billion dollar mission getting canned because it's $8M to $16M over budget. So the question is, does $10M to $20M matter to a science mission or not?

Offline Kesarion

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Re: Europa Clipper
« Reply #24 on: 03/20/2019 06:12 am »
More interesting to me is the fact that we have often been told in this section of the forum that a launch cost saving of $10M to $20M doesn't matter to science missions, since it's a tiny fraction of the total mission cost. Yet here we have an important instrument on a multi-billion dollar mission getting canned because it's $8M to $16M over budget. So the question is, does $10M to $20M matter to a science mission or not?


When it comes to flagships the answers seems to be no, because as far as I understand it, the problem was not just regarding the cost growth of the instrument.

https://spacenews.com/nasa-dealing-with-cost-growth-on-planetary-science-flagship-missions/

Quote
Glaze said that cost alone was not the reason for removing ICEMAG. “The emphasis is not so much on the overall cost growth but on the other risks that were inherent in the design and the approach that was going forward,” she said. “Most of the concern had to do with the future risks and the fact that instrument was not stabilizing.”

I have in no way shape or form any expertise regarding the construction of space probes, but this seems to be a case of flawed engineering which could potentially force a redisgn in other parts of the spacecraft and ultimately endanger the entire mission. Either that or they weren’t even sure that ICEMAG was capable of performing its baseline goals.

One of the purposes of flagships is to develop new instruments, but if the risks outweight the benefits, cancelling one in a phase were you could still replace it with a proven design is the responsible thing to do. After all, good science is still better than no science. The prospect of price ballooning when Europa Clipper lost its strongest congressional advocate (John Culberson) should be mitigated as much as possible.
« Last Edit: 03/20/2019 06:18 am by Kesarion »

Online ccdengr

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Re: Europa Clipper
« Reply #25 on: 03/20/2019 12:31 pm »
So the question is, does $10M to $20M matter to a science mission or not?
If I were going to be cynical, I'd say that it depends on who's getting the money.

Instruments are developed under separate subcontracts that are small fractions of the overall mission cost and typically cost-plus-fixed-fee with a budget cap.  Projects maintain some reserves in case of unexpected cost growth, typically not allocated by instrument, so if one instrument overruns, that comes out of reserves and means there's less to cover other instruments' problems.  If one instrument gets into a lot of trouble, it could use up all the reserve or potentially cause the whole mission to go over budget.

You could run these missions in a "cost is no object" mode (*cough*JWST*cough*) and just keep ratcheting the cost up and up, but if you don't want to do that, you have to compartmentalize spending and descope or delete elements that are going over budget.

Maybe it's paradoxical considering that these missions are flown for the instruments ultimately, but the instruments are usually on the bottom of the heap in terms of control.

Offline Kesarion

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Re: Europa Clipper
« Reply #26 on: 03/29/2019 03:55 pm »
Mission to Europa Gets New Instrument to Look for Signs of Habitability

Quote
Margaret Kivelson, a professor emerita at the University of California, Los Angeles, will lead the effort to develop a simplified magnetometer to replace ICEMAG. The instrument will measure Europa’s magnetic field and gather data on the ocean’s depth and salinity. Kivelson previously led the magnetometer team on the spacecraft Galileo, which orbited Jupiter in the 1990s. She is credited with discovering the ocean beneath Europa’s ice shell.
ICEMAG’s estimated cost had grown to $45 million—nearly three times its proposed price—according to NASA headquarters. Sophisticated internal sensors had vexed the ICEMAG science team and led to much of the extra expense. The new magnetometer will do away with those sensors, using simplified components instead. The downside is that the new sensors will likely lose calibration over time and drift in response to temperature variations. The team is now devising strategies to compensate for these effects.

Quote
“We are gearing up for one last review needed for confirmation of the mission by NASA,” Pappalardo says. “That is where NASA says that you are ready and cleared to go build the instruments and spacecraft.” In April, the project will go through its “delta preliminary design review” (PDR)—a reevaluation of certain elements of the spacecraft that had given NASA pause.

Quote
Once completed successfully, the project will go through another review at NASA headquarters called “key decision point C.” The agency will commit to the calendar and cost determined during the PDR, and the process of finalizing design and fabricating the hardware can begin.[...]After the April design review, Clipper will likely enter the final design and fabrication phase in August. If all goes well, it will lift its first inch from the launchpad in 2023.

Quote
When Culberson was defeated for reelection last year, things looked grim. He still had a few tricks up his sleeve, however. “Before I left,” he says, “I won the support of a number of my House colleagues to be sure that they would protect those missions.” And tying Clipper to SLS should help.

*Fingers crossed* that Culberson reached a hand to democrat members of the House of Represantatives so that the Europa Lander could at least continue as a technology development program.

Offline redliox

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Re: Europa Clipper
« Reply #27 on: 04/01/2019 08:27 pm »
While the magnetometer is getting tweaked, apparently the prototype to the main antenna is already receiving testing:  http://spaceref.com/europa-1/europa-clipper-high-gain-antenna-undergoes-testing.html

It also reminds me of a bronze Voyager antenna.
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Online zubenelgenubi

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Re: Europa Clipper
« Reply #28 on: 04/27/2019 06:20 pm »
Europa Clipper instrument change could affect mission science, dated April 26
Re: ICEMAG instrument replacement
Quote
In its place, NASA will fly a “facility magnetometer” that will collect some of the same magnetic field data as ICEMAG in the vicinity of Europa, an icy moon of Jupiter. The agency subsequently said Margaret Kivelson, a planetary scientist at UCLA who also is the new chair of the Space Studies Board, will lead the development of the magnetometer.
<snip>
Robert Pappalardo, project scientist for the mission, said in an April 23 presentation at an Outer Planets Assessment Group (OPAG) meeting here that challenges with the sensors’ fiber optic cables, which are sensitive to the temperature and radiation conditions at Jupiter, “essentially brought on its downfall.”
<snip>
The increased errors of the [replacement] fluxgate magnetometers, [Pappalardo] said, “does put at risk” some of the key, or Level 1, science requirements of the mission, notably estimating the thickness of Europa’s ice shell as well as the depth and salinity of the liquid water ocean beneath the ice. Other Level 1 science requirements aren’t affected, he emphasized.
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Re: Europa Clipper
« Reply #29 on: 04/27/2019 07:20 pm »
Further re: Europa Clipper launch options and launch windows for one of those options, from Europa Clipper instrument change could affect mission science, dated April 26
Quote
The project has been looking at a number of options for the non-SLS option. Speaking at a National Academies committee meeting in March, Barry Goldstein, Europa Clipper project manager, said one option under consideration would be a launch on a SpaceX Falcon Heavy equipped with a Star 48BV kick stage. That trajectory, known formally as Delta-V Earth Gravity Assist 3-Minus, involves a launch in November 2023 and an Earth flyby in October 2025 prior to arrival at Jupiter in September 2029.

The travel time of a little less than six years is only slightly shorter than some other alternatives previously studied. However, it has the advantage of not requiring any gravity assist flybys of Venus, with the spacecraft getting only slightly closer to the sun on its trajectory than the Earth. “That solves a world of problems on thermal management,” Goldstein said. “We no longer have the challenge of the thermal problems that we had getting close to Venus.”

A second advantage, he said, is that it offers a backup launch window roughly a year later, whereas with the Venus flyby trajectory the mission would have to wait until 2025 if it can’t launch in 2023. “We’re not 100 percent there yet, but things are looking very positive” for the new trajectory, he said.

Also, see slide embedded in the article.
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Offline Ultrafamicom

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Re: Europa Clipper
« Reply #30 on: 04/28/2019 04:42 pm »


a launch in November 2023 and an Earth flyby in October 2025 prior to arrival at Jupiter in September 2029.

Why does it take 4 years from EGA(not launch!) to Jupiter arrival? A transfer orbit with 5.5AU AP and 1AU PE has period of ~6 years, so even Hormman transfer will only take 3 years. Does it actually pass AP when encounter with Jupiter? But what's the purpose?

Offline redliox

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Re: Europa Clipper
« Reply #31 on: 04/29/2019 02:20 am »
Excellent find with the 'Clipper update zubenelgenubi  :)

It's good to see they gave Falcon Heavy as a calculated, if not official, option.  Although I had hopes for SLS, I'm sad to say it looks like it'll be falling out of favor fast.  It could be ready, and perhaps even more available if the Gateway payloads get offloaded to commercial alternatives, by 2023.  I'll be more than happy with a route that sees 'Clipper at Europa in less than a decade.  Now that we know what's available, which is the Atlas V, Delta IV, FH, and SLS (a momentary big if), the debate on what'll be used should be laid to rest.  The team and Congress will decide especially as '23 approaches.  Probably the budget will be the decider in the end.

If anyone wants extra credit though, perhaps it should be checked as to what asteroids 'Clipper could hypothetically flyby if it launches in '23.  ;)
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Offline redliox

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Re: Europa Clipper
« Reply #32 on: 04/29/2019 02:22 am »
https://www.lpi.usra.edu/opag/meetings/mar2019/Findings.pdf

Here’s a recent report from OPAG which also addresses the recent termination of ICEMAG. I’m surprised to find out that the cancellation of certain risky instruments seems to be new process and I am pleased to see others call for transparency regarding this new approach towards keeping science missions within their cost caps.

Has there been any further news from the OPAG meeting this month?  Aside from the ICEMAG and FH/EGA-trajectory options being unveiled?
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Offline vjkane

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Re: Europa Clipper
« Reply #33 on: 04/29/2019 03:37 am »
Has there been any further news from the OPAG meeting this month?  Aside from the ICEMAG and FH/EGA-trajectory options being unveiled?
The OPAG presentation was entirely focused on the impact on the magnetometer measurements.  The launch/trajectory options were from an earlier meeting this year (CAPS?).

Offline redliox

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Re: Europa Clipper
« Reply #34 on: 04/29/2019 04:25 am »
Has there been any further news from the OPAG meeting this month?  Aside from the ICEMAG and FH/EGA-trajectory options being unveiled?
The OPAG presentation was entirely focused on the impact on the magnetometer measurements.  The launch/trajectory options were from an earlier meeting this year (CAPS?).

And in regards to ICEMAG, basically the improved electronics and optronics turned out to be sadly vulnerable to Jupiter's radiation whereas another, presumably off-shelf or 'traditional', magnetometer could manage but only, slightly better at best, at Galileo's detection levels?  If that's the case, one only has to remember that Galileo was heavily plagued by issues and, even with the Europa campaign in its extended mission, the data was sporadic and far from global.  As I recall, the Galilean team was forced to choose between closeups and global views, with the former being chosen.  The poor old probe never fulfilled its full potential, and there never has been a global map of Europa, visually or magnetically.  'Clipper will basically finish the job Galileo never properly finished to begin with.

If the other instruments can be cobbled together without complication this would still be a win-win for mapping Europa.  I'd presume the radar instrument would be the biggest to worry about.  A wonky (yet functional) magnetometer would only imply there was an ocean below whereas the radar would solidly confirm it.

Although the obvious focus will be for Europa, I hope there are some thoughts to contribute to Jupiter or the likes of Callisto and Ganymede, although the later would receive extensive coverage from JUICE.
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Offline vjkane

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Re: Europa Clipper
« Reply #35 on: 04/29/2019 04:47 am »
And in regards to ICEMAG, basically the improved electronics and optronics turned out to be sadly vulnerable to Jupiter's radiation whereas another, presumably off-shelf or 'traditional', magnetometer could manage but only, slightly better at best, at Galileo's detection levels? 

'Clipper will basically finish the job Galileo never properly finished to begin with.

A wonky (yet functional) magnetometer would only imply there was an ocean below whereas the radar would solidly confirm it.
Per the recent OPAG presentation, my recollection is that the fiber optic cables caused the problems.

Clipper's capabilities go incredibly beyond those of Galileo.  The latter was late 1970's technology selected to study the entire Jovian system.  The former is mid 2010's technology selected specifically to study Europa.

I believe that the radar penetrates only a few kilometers into the ice shell.  Perhaps in places, that will allow it to probe the start of the ocean.  The magnetometer's goal is to study both the depth and the salinity of the ocean.  The new design may be unable to substantially improve on Galileo's results (a lot depends on the ocean's salinity).  However, I want to wait to see what really smart people are able to come up with the new design before it write it off as little improvement.

One key problem with Clipper is that it does only flybys.  Eventually, the study of Europa would benefit from a short-lived orbiter that performs magnetometer measurements throughout Europa's orbit around Jupiter, lidar measurements of the surface flux to study the depth and strength of the icy shell, and gravity studies.

Offline vjkane

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Re: Europa Clipper
« Reply #36 on: 04/29/2019 02:23 pm »
-You're going to hear some low level (i.e. not very public) grumbling about the overall capabilities of the mission and whether it will really provide the science that the community wants. Some of that was voiced at OPAG last week by people who wish that NASA was building an orbiter instead of a flyby mission. Some of these people are in denial, because there simply was not enough money to build the orbiter. But certainly some science was lost when going from orbiter to flyby.
There are three measurements that really require data from orbit:

Ice flexing by studying how height of the ice changes as Jupiter-caused tides change and flex the ice revealing its thickness.  You want repeat measurements of the same location.

Magnetic measurements from multiple points in Europa's orbit through Jupiter's magnetosphere

Gravity measurements

The Clipper team appears to have done a heroic job of trying to perform these studies from flybys instead of from orbit. 

However, an orbiter would not have the lifespan to replicate many of Clipper's remote sensing studies.  It could gather the data, but there isn't time to return the bulk of it to Earth.  Clipper will use most of the days between encounters to return the data from each flyby.

ESA has studids a simple Europa orbiter.  This was presented as a possible European contribution early in the Europa lander trade off studies.  However, it could be a standalone mission.  Since such a mission would carry just the magnetometer instrument (which would be only one that needs to be outside the spacecraft), a laser altimeter (lidar), and the radio experiment, almost all the electronics could be in a heavily shielded vault.  Data rates would be low.  If I remember the old Europa orbiter studies correctly, even a month in orbit would return the needed data.

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Re: Europa Clipper
« Reply #37 on: 04/29/2019 03:27 pm »
a launch in November 2023 and an Earth flyby in October 2025 prior to arrival at Jupiter in September 2029.

Why does it take 4 years from EGA(not launch!) to Jupiter arrival? A transfer orbit with 5.5AU AP and 1AU PE has period of ~6 years, so even Hormman transfer will only take 3 years. Does it actually pass AP when encounter with Jupiter? But what's the purpose?

SLS is the only launcher of the set under consideration that can lift a "heavy" planetary probe onto a trans-jovian direct trajectory (simplest example is a Hohmann transfer orbit).

None of the other, currently flying launch vehicle/upper stage systems can do this.  Thus, the resort to delta-V gravity assists.

EDIT 4/30
Excerpt from "If Only We Had Taller Been" by Ray Bradbury
Quote
Short man, Large dream/
I send my rockets forth between my ears/
Hoping an inch of Good is worth a pound of years
« Last Edit: 04/30/2019 03:52 pm by zubenelgenubi »
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Offline ugordan

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Re: Europa Clipper
« Reply #38 on: 04/29/2019 04:15 pm »


a launch in November 2023 and an Earth flyby in October 2025 prior to arrival at Jupiter in September 2029.

Why does it take 4 years from EGA(not launch!) to Jupiter arrival? A transfer orbit with 5.5AU AP and 1AU PE has period of ~6 years, so even Hormman transfer will only take 3 years. Does it actually pass AP when encounter with Jupiter? But what's the purpose?

Either the slide is in error and the Earth flyby actually occurs in Oct 2026, not 2025 or it's just too illegible on the low-res slide so it makes the "6" look like a "5".

Reason for this conclusion: like you say, a Hohmann transfer takes roughly 3 years. However, this trajectory design is dubbed "3-Minus" and the 3 is stated to mean the spacecraft is injected into roughly a 3:1 resonant orbit with Earth. Therefore, it has a 3 year period so the flyby has to happen roughly 3 years after launch, leaving another 2.9 years for the typical Hohmann transfer to Jupiter after that.

This is different from the Juno mission profile which was a 2:1 resonant orbit, but it required a lot of delta-V for DSMs. The higher aphelion for Clipper might be the reason for the Star 48B kick stage baselined, essentially pushing the spacecraft as far out as possible to conserve propellant otherwise required for cruise DSMs for the actual Jupiter tour.

Offline Jim

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Re: Europa Clipper
« Reply #39 on: 04/30/2019 03:49 pm »
.perhaps even more available if the Gateway payloads get offloaded to commercial alternatives, by 2023.

It is the other way around.

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