Author Topic: SpaceX Dragon 2 Updates and Discussion - Thread 3  (Read 815117 times)

Offline John Santos

  • Full Member
  • **
  • Posts: 256
  • Liked: 243
  • Likes Given: 148
Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #520 on: 12/21/2018 10:03 pm »
In the picture from inside the building at 39A: assuming the more or less rectangular panel on the side of the Dragon is the hatch, there doesn't appear to be any method for opening it from the outside.  There is a smaller square panel in the center right side of the big panel, that appears to be held on by 4 bolts.  Is that a cover for the handle to open the hatch?  Or is this not the hatch at all but some other cover and the hatch is on the other side of the Dragon?  Or is it a temporary hatch for DM-1 and the real hatch will be installed on DM-2?
I think, given the lessons of Apollo 1, it is very important to have a hatch that can be opened quickly from either the inside or the outside.

(Edited for clarity)
« Last Edit: 12/21/2018 10:05 pm by John Santos »

Offline whitelancer64

Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #521 on: 12/21/2018 10:08 pm »
In the picture from inside the building at 39A: assuming the more or less rectangular panel on the side of the Dragon is the hatch, there doesn't appear to be any method for opening it from the outside.  There is a smaller square panel in the center right side of the big panel, that appears to be held on by 4 bolts.  Is that a cover for the handle to open the hatch?  Or is this not the hatch at all but some other cover and the hatch is on the other side of the Dragon?  Or is it a temporary hatch for DM-1 and the real hatch will be installed on DM-2?
I think, given the lessons of Apollo 1, it is very important to have a hatch that can be opened quickly from either the inside or the outside.

(Edited for clarity)

It is NOT the flight hatch that will be on the Dragon v2 with crew. This hatch is meant to be used only for the DM-1 mission (and probably IFA).

The Crew hatch will have an external handle to open it, along with (presumably) rescue instructions.
"One bit of advice: it is important to view knowledge as sort of a semantic tree -- make sure you understand the fundamental principles, ie the trunk and big branches, before you get into the leaves/details or there is nothing for them to hang on to." - Elon Musk
"There are lies, damned lies, and launch schedules." - Larry J

Offline Johnnyhinbos

  • Senior Member
  • *****
  • Posts: 3864
  • Boston, MA
  • Liked: 8095
  • Likes Given: 946
Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #522 on: 12/21/2018 10:22 pm »
Sorry to interrupt this propulsive landing /  NASA money vs SpaceX  / dead horse beating thread by asking about an update on Dragon 2.    :(

So, can someone explain the white covers that are over the black solar cells on the Trunk as seen in a photo a few posts up?  Protective until shortly before launch, or  will be there at launch and discarded sometime after Max-Q? Or is one side (180 degrees)  covered in solar cells and the other not?
One side of the trunk is white(ish) radiators, the other is covered with (wonderfully shiny black) solar cells.

And please - no beating dead horses references. I have a hard time letting go of the Dostoevsky imagery...
John Hanzl. Author, action / adventure www.johnhanzl.com

Online clongton

  • Expert
  • Senior Member
  • *****
  • Posts: 12111
  • Connecticut
    • Direct Launcher
  • Liked: 7508
  • Likes Given: 3817
Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #523 on: 12/21/2018 10:36 pm »
Sorry to interrupt this propulsive landing /  NASA money vs SpaceX  / dead horse beating thread by asking about an update on Dragon 2.    :(

So, can someone explain the white covers that are over the black solar cells on the Trunk as seen in a photo a few posts up?  Protective until shortly before launch, or  will be there at launch and discarded sometime after Max-Q? Or is one side (180 degrees)  covered in solar cells and the other not?

The white half of the trunk are radiators.

And the black half (obviously) are solar cells.
I don't add this comment to try and be funny, but to ask a specific question.
Apollo was rotated on its longitudinal axis during its missions to prevent overheating of any one side.
Will Dragon be similarly rotated for the same reason?
And if so how will this affect the environmental systems when the radiators are facing the sun?
Chuck - DIRECT co-founder
I started my career on the Saturn-V F-1A engine

Offline Comga

  • Senior Member
  • *****
  • Posts: 6503
  • Liked: 4624
  • Likes Given: 5359
Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #524 on: 12/21/2018 11:04 pm »
Sorry to interrupt this propulsive landing /  NASA money vs SpaceX  / dead horse beating thread by asking about an update on Dragon 2.    :(

So, can someone explain the white covers that are over the black solar cells on the Trunk as seen in a photo a few posts up?  Protective until shortly before launch, or  will be there at launch and discarded sometime after Max-Q? Or is one side (180 degrees)  covered in solar cells and the other not?

The white half of the trunk are radiators.

And the black half (obviously) are solar cells.
I don't add this comment to try and be funny, but to ask a specific question.
Apollo was rotated on its longitudinal axis during its missions to prevent overheating of any one side.
Will Dragon be similarly rotated for the same reason?
And if so how will this affect the environmental systems when the radiators are facing the sun?

It's pretty unlikely SpaceX will replicate the "barbeque roll" for thermal equalization, but they probably don't have to.
I think the roll was done transiting between LEO and lunar orbit or on the return trip, where there were extended periods of continuous sunlight.
The Dragon should remain in LEO, particularly now that all deep space missions are planned with BFS.
The ISS has gone for decades without rolling, staying mostly in a fixed Local Vertical Local Horizontal (LVLH) orientation.
Dragon couldn't do a roll when docked to the ISS for six months.  It has to be able to handle full sunlight for 45 minutes, and longer at times of high beta angles.

Which does bring up the question of why SpaceX went with the body mounted solar cells, and didn't just add four fins to the Cargo Dragon trunk.  I can guess (eliminating the possibility of the solar panel pods ripping off, a la Skylab, during a Max-Q abort) but guessing only gets me so far.
What kind of wastrels would dump a perfectly good booster in the ocean after just one use?

Offline Alexphysics

  • Full Member
  • ****
  • Posts: 1625
  • Spain
  • Liked: 6027
  • Likes Given: 952
Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #525 on: 12/21/2018 11:11 pm »
The ISS has gone for decades without rolling, staying mostly in a fixed Local Vertical Local Horizontal (LVLH) orientation.

However... they do move the station when there are times of high solar beta angles to protect the main radiators and the ones on the russian segment. They can't work properly if they are constantly illuminated and there are times where the ISS doesn't see a sunset in days.

But that is obviously info related with the ISS and not with Dragon 2, so sorry for that, but just wanted to give some perspective on this particular example that was given.

Offline Jim

  • Night Gator
  • Senior Member
  • *****
  • Posts: 37831
  • Cape Canaveral Spaceport
  • Liked: 22071
  • Likes Given: 430
Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #526 on: 12/21/2018 11:18 pm »

Apollo was rotated on its longitudinal axis during its missions to prevent overheating of any one side.


But not when docked to Skylab.

Offline docmordrid

  • Senior Member
  • *****
  • Posts: 6351
  • Michigan
  • Liked: 4223
  • Likes Given: 2
Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #527 on: 12/21/2018 11:27 pm »
>
Which does bring up the question of why SpaceX went with the body mounted solar cells, and didn't just add four fins to the Cargo Dragon trunk.  .

I would assume to eliminate the numerous "solar wing" deployment mechanisms and events, starting with the covers. KISS.
« Last Edit: 12/21/2018 11:30 pm by docmordrid »
DM

Offline Lar

  • Fan boy at large
  • Global Moderator
  • Senior Member
  • *****
  • Posts: 13469
  • Saw Gemini live on TV
  • A large LEGO storage facility ... in Michigan
  • Liked: 11869
  • Likes Given: 11116
Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #528 on: 12/21/2018 11:56 pm »
>
Which does bring up the question of why SpaceX went with the body mounted solar cells, and didn't just add four fins to the Cargo Dragon trunk.  .

I would assume to eliminate the numerous "solar wing" deployment mechanisms and events, starting with the covers. KISS.
IIRC on the very first Dragon there was some excitement about deployment not working quite as expected but I don't think they've ever failed to deploy. Bodymounted cells, though, as long as they remain attached, CAN'T fail to deploy.
"I think it would be great to be born on Earth and to die on Mars. Just hopefully not at the point of impact." -Elon Musk
"We're a little bit like the dog who caught the bus" - Musk after CRS-8 S1 successfully landed on ASDS OCISLY

Offline QuantumG

  • Senior Member
  • *****
  • Posts: 9266
  • Australia
  • Liked: 4489
  • Likes Given: 1126
Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #529 on: 12/22/2018 12:04 am »
From SpaceX's perspective, the purpose of the commercial crew program is to get NASA, Congress and the public used to SpaceX launching humans into space. That's it. If they can't do that, they have no chance of sending anyone to Mars, and even less chance of getting Congress to contribute to the cost. Considering that the whole project rests on winning this battle, they're willing to put up with just about anything.

Human spaceflight is basically just LARPing now.

Offline Zed_Noir

  • Senior Member
  • *****
  • Posts: 5490
  • Canada
  • Liked: 1811
  • Likes Given: 1302
Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #530 on: 12/22/2018 01:06 am »
So let's start a different unanswerable debate about Dragon 2
Please point out corrections where these assumptions are wrong.
SpaceX is building a new Dragon 2 for each manned/crewed flight to the ISS under Commercial Crew.
Eventually NASA will allow these to fly, next spring, next fall, before Boeing's CST-100, after Boeing, whatever.
They plan on refurbishing capsules and reusing them for CRS-II cargo flights.
SpaceX may do one crew rotation per year, and perhaps three cargo flights, as one of three providers, four if we count the modest amount of cargo that can ride with the four passengers on CST-100.
Because Dragon is never flown as expendable, SpaceX will start accumulating used Dragons.
I would presume that BFS will take a bit longer than some of Musk's predictions to get built, work out the ground system, fly low altitude, low speed tests, build to high speed and altitude, practice the acrobatics of converting from reentry to landing, and fly some test orbits, which will be needed before the DearMoon flight.
Given they will have used first stages and capsules complete with proven life support systems, the marginal cost of an independent crew flight to orbit is mostly the second stage and trunk.  This is not trivial, but not huge on the scale of SpaceX projects, or even the Boring Company projects.

Why wouldn't someone try to arrange a private flight to LEO?
Why wouldn't SpaceX agree to make that happen?
NASA will have "real astronauts" doing Real Astronaut Stuff (R) on the real space station, so they might not care.
SpaceX can "walk and chew gum at the same time". 
I think this will indeed happen, perhaps in 2021 or 2022.

I also hope it does.

SpaceX's attitude has generally been, "if someone is willing to pay us, we'll do it," so I would say such a tourist flight(s) would be plausible.

That said, they will probably also be re-using crew dragons for flights to Bigelow's space station, whenever they get around to launching it.

Skip the second stage for an interesting suborbital flight. Only throwing away the trunk. Should be relatively inexpensive with reusable booster and capsule.

If the Dragon is out of the atmosphere does it need a trunk at all?

Attached the Dragon to a modified intrastage fairing directly. Actively stablized the Dragon for the short time aloft with the Dracos.

Of course you might need down range recovery assets.

Offline Comga

  • Senior Member
  • *****
  • Posts: 6503
  • Liked: 4624
  • Likes Given: 5359
Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #531 on: 12/22/2018 01:24 am »
Forget Bigelow (Anyone still work there?)
Forget custom, one-off configurations. (Custom trunks, crew from  AFB,...)
With all the parts available, how can SpaceX resist?

Edit: spelling
« Last Edit: 12/22/2018 01:25 am by Comga »
What kind of wastrels would dump a perfectly good booster in the ocean after just one use?

Offline RonM

  • Senior Member
  • *****
  • Posts: 3340
  • Atlanta, Georgia USA
  • Liked: 2233
  • Likes Given: 1584
Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #532 on: 12/22/2018 02:27 am »
So let's start a different unanswerable debate about Dragon 2
Please point out corrections where these assumptions are wrong.
SpaceX is building a new Dragon 2 for each manned/crewed flight to the ISS under Commercial Crew.
Eventually NASA will allow these to fly, next spring, next fall, before Boeing's CST-100, after Boeing, whatever.
They plan on refurbishing capsules and reusing them for CRS-II cargo flights.
SpaceX may do one crew rotation per year, and perhaps three cargo flights, as one of three providers, four if we count the modest amount of cargo that can ride with the four passengers on CST-100.
Because Dragon is never flown as expendable, SpaceX will start accumulating used Dragons.
I would presume that BFS will take a bit longer than some of Musk's predictions to get built, work out the ground system, fly low altitude, low speed tests, build to high speed and altitude, practice the acrobatics of converting from reentry to landing, and fly some test orbits, which will be needed before the DearMoon flight.
Given they will have used first stages and capsules complete with proven life support systems, the marginal cost of an independent crew flight to orbit is mostly the second stage and trunk.  This is not trivial, but not huge on the scale of SpaceX projects, or even the Boring Company projects.

Why wouldn't someone try to arrange a private flight to LEO?
Why wouldn't SpaceX agree to make that happen?
NASA will have "real astronauts" doing Real Astronaut Stuff (R) on the real space station, so they might not care.
SpaceX can "walk and chew gum at the same time". 
I think this will indeed happen, perhaps in 2021 or 2022.

I also hope it does.

SpaceX's attitude has generally been, "if someone is willing to pay us, we'll do it," so I would say such a tourist flight(s) would be plausible.

That said, they will probably also be re-using crew dragons for flights to Bigelow's space station, whenever they get around to launching it.

Skip the second stage for an interesting suborbital flight. Only throwing away the trunk. Should be relatively inexpensive with reusable booster and capsule.

If the Dragon is out of the atmosphere does it need a trunk at all?

Attached the Dragon to a modified intrastage fairing directly. Actively stablized the Dragon for the short time aloft with the Dracos.

Of course you might need down range recovery assets.

Dragon 2 needs a trunk for abort scenarios. No need to put solar cells on the trunk. Short flight should work with internal batteries.

Online LouScheffer

  • Senior Member
  • *****
  • Posts: 3453
  • Liked: 6263
  • Likes Given: 883
Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #533 on: 12/22/2018 03:38 am »
And if so how will this affect the environmental systems when the radiators are facing the sun?
The radiators should still work when facing the sun.  Presumably, the paint they use is the type that is white (reflective) in the visible, so absorbs little radiation from the sun.  But it's black in the infra-red, so it can still radiate heat.  See, for example Spacecraft Thermal Control Systems, page 11.

Offline Comga

  • Senior Member
  • *****
  • Posts: 6503
  • Liked: 4624
  • Likes Given: 5359
Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #534 on: 12/22/2018 06:31 am »
And if so how will this affect the environmental systems when the radiators are facing the sun?
The radiators should still work when facing the sun.  Presumably, the paint they use is the type that is white (reflective) in the visible, so absorbs little radiation from the sun.  But it's black in the infra-red, so it can still radiate heat.  See, for example Spacecraft Thermal Control Systems, page 11.
That may work in theory, but in practice it’s not possible to get a durable paint that’s sufficiently reflective to radiate heat from reasonable temperature coolants while being illuminated by the Sun.
The white paint can, though, be reflective enough that the system won’t overheat, boil the coolant, discolor the paint, warp the radiators, during limited exposures.
My guess is that Dragon will dock so that the radiators avoid extended illumination by the Sun.
There are practical considerations to this, too. Facing the radiators downward, to the warm Earth and atmosphere, will reduce their capacity to dump heat, relative to what they can dump to cold space. This will place limits on how much power Dragon can dissipate while docked, or why the radiators have to be so big, or both.
PS I have collaborated on thermal radiators for deep space and LEO instruments.
What kind of wastrels would dump a perfectly good booster in the ocean after just one use?

Offline woods170

  • IRAS fan
  • Senior Member
  • *****
  • Posts: 12196
  • IRAS fan
  • The Netherlands
  • Liked: 18496
  • Likes Given: 12573
Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #535 on: 12/22/2018 11:10 am »
Sorry to interrupt this propulsive landing /  NASA money vs SpaceX  / dead horse beating thread by asking about an update on Dragon 2.    :(

So, can someone explain the white covers that are over the black solar cells on the Trunk as seen in a photo a few posts up?  Protective until shortly before launch, or  will be there at launch and discarded sometime after Max-Q? Or is one side (180 degrees)  covered in solar cells and the other not?

The white half of the trunk are radiators.

And the black half (obviously) are solar cells.
I don't add this comment to try and be funny, but to ask a specific question.
Apollo was rotated on its longitudinal axis during its missions to prevent overheating of any one side.
Will Dragon be similarly rotated for the same reason?
And if so how will this affect the environmental systems when the radiators are facing the sun?

It's pretty unlikely SpaceX will replicate the "barbeque roll" for thermal equalization, but they probably don't have to.
I think the roll was done transiting between LEO and lunar orbit or on the return trip, where there were extended periods of continuous sunlight.
The Dragon should remain in LEO, particularly now that all deep space missions are planned with BFS.
The ISS has gone for decades without rolling, staying mostly in a fixed Local Vertical Local Horizontal (LVLH) orientation.
Dragon couldn't do a roll when docked to the ISS for six months.  It has to be able to handle full sunlight for 45 minutes, and longer at times of high beta angles.


That is the correct answer.

Crew Dragon is flying in LEO. Meaning it is in sunlight for only 45 minutes at the time, followed by 45 minutes of being out of sunlight. No chance for the vehicle to overheat:
- Soyuz doesn't do a barbecue roll.
- Shuttle didn't do a barbecue roll.
- Apollo didn't due barbecue roll on it LEO-bound missions (Apollo 7, Apollo 9, Skylab and ASTP).

Crew Dragon, when in sunlight, will be pointing the side with the solar cells towards the sun. That automatically means that the radiators are pointing away from the sun, which is a nearly ideal situation for the radiators.

Barbecue roll is one possible mitigation of heating effects when the spacecraft is in continuous sunlight, such as during transit to the Moon or interplanetary travel. Another is adding sufficient thermal insulation on the side that is pointing to the sun. That's why, currently, no barbecue roll is envisioned for BFS.

Offline woods170

  • IRAS fan
  • Senior Member
  • *****
  • Posts: 12196
  • IRAS fan
  • The Netherlands
  • Liked: 18496
  • Likes Given: 12573
Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #536 on: 12/22/2018 11:12 am »

Apollo was rotated on its longitudinal axis during its missions to prevent overheating of any one side.


But not when docked to Skylab.

Indeed. And that is why substantial parts of the Skylab CSM's were painted white on the side that was facing the sun.

Offline Phillip Clark

  • Senior Member
  • *****
  • Posts: 2616
  • Hastings, England
  • Liked: 557
  • Likes Given: 1078
Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #537 on: 12/22/2018 05:37 pm »
Since there doesn't appear to be a thread for the Dragon-2 DM1 mission (yet), is this still on schedule for NASA's target of January 7th (2019) launch?
I've always been crazy but it's kept me from going insane - WJ.

Offline cppetrie

  • Full Member
  • ****
  • Posts: 792
  • Liked: 552
  • Likes Given: 3
Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #538 on: 12/22/2018 05:55 pm »
Since there doesn't appear to be a thread for the Dragon-2 DM1 mission (yet), is this still on schedule for NASA's target of January 7th (2019) launch?

See here:
SpaceX Falcon 9 / Dragon 2 : SpX-DM1 : NET Jan 17, 2019 : General Thread
https://forum.nasaspaceflight.com/index.php?topic=36966.0

Edit to add: no it is now targeting the 17th instead. Explanation for slide right is in the linked thread.
« Last Edit: 12/22/2018 05:56 pm by cppetrie »

Online clongton

  • Expert
  • Senior Member
  • *****
  • Posts: 12111
  • Connecticut
    • Direct Launcher
  • Liked: 7508
  • Likes Given: 3817
Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #539 on: 12/22/2018 06:20 pm »
If the Dragon is out of the atmosphere does it need a trunk at all?

The onboard batteries are very short-lived. Power is normally supplied by the solar cells on half the trunk body. Cooling for the onboard electronics is supplied by the radiators on the other half of the trunk body.
« Last Edit: 12/22/2018 06:25 pm by clongton »
Chuck - DIRECT co-founder
I started my career on the Saturn-V F-1A engine

Tags:
 

Advertisement NovaTech
Advertisement Northrop Grumman
Advertisement
Advertisement Margaritaville Beach Resort South Padre Island
Advertisement Brady Kenniston
Advertisement NextSpaceflight
Advertisement Nathan Barker Photography
0