Author Topic: SpaceX Dragon XL  (Read 405052 times)

Offline jadebenn

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Re: SpaceX Dragon XL
« Reply #520 on: 03/23/2021 11:20 am »
I don't know if this is true but it would make sense:

https://twitter.com/artemis360_moon/status/1372292826977902594

Quote
Dragon XL will be used to resupply Gateway, a lunar outpost for Artemis astronauts. This resupply ship will also include a toilet and beds to provide extra space in HALO for science.
This would explain the "1 year docked" requirement a lot of us were scratching our heads at in the original GLS procurement.

Offline DreamyPickle

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Re: SpaceX Dragon XL
« Reply #521 on: 03/23/2021 02:24 pm »
A dragon-derived Hydrazine tug has been speculated about before and it could be used for a great number of things, among them as a third stage for Falcon Heavy and even Starship.

Is it more than just speculation? There does not appear to be any budget for it.

SpaceX does not currently have a vacuum-optimized hydrazine engine and using SuperDracos (as frequently proposed) would have worse ISP than the AJ10 on the Orion service module. Doing a hydrazine tug "properly" would likely require a new engine.

Offline Lars-J

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Re: SpaceX Dragon XL
« Reply #522 on: 03/23/2021 03:46 pm »
SpaceX does not currently have a vacuum-optimized hydrazine engine and using SuperDracos (as frequently proposed) would have worse ISP than the AJ10 on the Orion service module. Doing a hydrazine tug "properly" would likely require a new engine.

What about Draco engines? Stick a full nozzle on them, and they should qualify. But maybe you mean something with more thrust, like the Orion main engine?

Offline baldusi

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Re: SpaceX Dragon XL
« Reply #523 on: 03/23/2021 07:35 pm »
A dragon-derived Hydrazine tug has been speculated about before and it could be used for a great number of things, among them as a third stage for Falcon Heavy and even Starship.

Is it more than just speculation? There does not appear to be any budget for it.

SpaceX does not currently have a vacuum-optimized hydrazine engine and using SuperDracos (as frequently proposed) would have worse ISP than the AJ10 on the Orion service module. Doing a hydrazine tug "properly" would likely require a new engine.

You probably meant a storable propellant tug, right? Hydrazine is a monopropellant. Tugs usually use a something like MMH/N2O2. Yes, variations of hydrazine, but a different set.
I will only say three things:
1) Not all space-certified storables are as toxic as the hidrazine based ones. There are some new one that were just demonstrated non toxic, and SpaceX is planning on using methalox for multiyear missions.
2) If one company has demonstrated an amazing capability at developing new engines, it is SpaceX. If they needed a storable vac optimized engine, they will develop it very quickly. Specially with all the internal experience they have.
3) I don't see why you can't use an electric tug.

Offline DistantTemple

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Re: SpaceX Dragon XL
« Reply #524 on: 03/23/2021 08:00 pm »


It might be better to think of it as a self- propelled outhouse.
That's it, you've forever ruined an entire spacecraft for me  :D

Even better - a self propelled outhouse you can sleep in with your three closest friends! :D
It would make a pretty good police box... its not blue, and its not a cuboid, but once inside it fulfils your most pressing needs, and transports you to boot. Who was that doctor character... he was releasing SX intellectual property... he was using a future version with upgraded engines to get that time displacement effect.
« Last Edit: 03/23/2021 08:00 pm by DistantTemple »
We can always grow new new dendrites. Reach out and make connections and your world will burst with new insights. Then repose in consciousness.

Online spacenut

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Re: SpaceX Dragon XL
« Reply #525 on: 03/23/2021 10:27 pm »
Can Dragon XL be made into a tug to transfer other modules, landers, or supplies to the Artemis orbit? 

Offline Slarty1080

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Re: SpaceX Dragon XL
« Reply #526 on: 03/24/2021 09:06 pm »
I don't know if this is true but it would make sense:

https://twitter.com/artemis360_moon/status/1372292826977902594

Quote
Dragon XL will be used to resupply Gateway, a lunar outpost for Artemis astronauts. This resupply ship will also include a toilet and beds to provide extra space in HALO for science.
Does it make sense? A disposable cargo container is becoming more of a full fledged habitat module with a very short service life.

If dragon was bringing those to the station and leaving them behind maybe that would make sense. (Future crews could relocate them back into subsequent dragon vehicles)

Otherwise it's a recurring weight and cost to each dragon XL mission. Plus there is likely more stringent requirements on dragon if it is planned to be occupied like a habitat vs. infrequently accessed like a cargo craft.

Or maybe this is just on the first dragon XL before the ESA habitat module is available... That could make sense.
It might be better to think of it as a self- propelled outhouse. Dragon XL will be bringing waste back from the station, so having the toilet be on board to directly interface with the waste tanks makes a certian amount of sence and reduces contamination on the rest of the station.
And no ECCLSS in the outhouse so it might get a bit ripe in there. I suppose they will just have to hold their breath.  ;D
My optimistic hope is that it will become cool to really think about things... rather than just doing reactive bullsh*t based on no knowledge (Brian Cox)

Offline wannamoonbase

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Re: SpaceX Dragon XL
« Reply #527 on: 03/24/2021 09:12 pm »
I don't know if this is true but it would make sense:

https://twitter.com/artemis360_moon/status/1372292826977902594

Quote
Dragon XL will be used to resupply Gateway, a lunar outpost for Artemis astronauts. This resupply ship will also include a toilet and beds to provide extra space in HALO for science.
Does it make sense? A disposable cargo container is becoming more of a full fledged habitat module with a very short service life.

If dragon was bringing those to the station and leaving them behind maybe that would make sense. (Future crews could relocate them back into subsequent dragon vehicles)

Otherwise it's a recurring weight and cost to each dragon XL mission. Plus there is likely more stringent requirements on dragon if it is planned to be occupied like a habitat vs. infrequently accessed like a cargo craft.

Or maybe this is just on the first dragon XL before the ESA habitat module is available... That could make sense.
It might be better to think of it as a self- propelled outhouse. Dragon XL will be bringing waste back from the station, so having the toilet be on board to directly interface with the waste tanks makes a certian amount of sence and reduces contamination on the rest of the station.
And no ECCLSS in the outhouse so it might get a bit ripe in there. I suppose they will just have to hold their breath.  ;D

After a few days in space the sense of smell diminishes, at least it did with Apollo. 
We very much need orbiter missions to Neptune and Uranus.  The cruise will be long, so we best get started.

Offline jarmumd

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Re: SpaceX Dragon XL
« Reply #528 on: 03/24/2021 10:29 pm »
No different than with Dragon 2 at ISS.  The ECLSS isn't on when docked to the ISS, there is a ventilation pipe which provides circulation for the air.  Would imagine gateway would be the same...

Offline woods170

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Re: SpaceX Dragon XL
« Reply #529 on: 03/25/2021 07:40 am »
Can Dragon XL be made into a tug to transfer other modules, landers, or supplies to the Artemis orbit? 

Dragon XL-based tug would be launched with the module already docked to it. The module would be where the pressurized section is on Dragon XL. So, launch on FH as a 'whole package'

FH upper stage would push the combination into lunar transfer orbit.
Dragon XL-based tug does the final job: enter NRHO, approach to Lunar Gateway and perform the docking.

After the module has been removed from Dragon XL-based tug, and relocated to its permanent position on Gateway (by means of Canadarm 3), the Dragon XL-based tug would undock and send itself into a disposal orbit.

Dragon XL is already in development for sending supplies to the Lunar Gateway. So will be a modified version of HTV-X.

Landers will get to Gateway under their own power. National Team has a Cygnus derivative for that, which serves as a transfer stage for the their lander.
Dynetics uses in-space refueling and its own engines.
So will lunar Starship: in-space refueling and its own engines.

Dragon XL-based tug is there mostly for getting modules, without their own propulsion system, to the Gateway (including the docking).
« Last Edit: 03/25/2021 07:44 am by woods170 »

Offline woods170

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Re: SpaceX Dragon XL
« Reply #530 on: 03/25/2021 07:43 am »
No different than with Dragon 2 at ISS.  The ECLSS isn't on when docked to the ISS, there is a ventilation pipe which provides circulation for the air.  Would imagine gateway would be the same...

Naturally, the toilet will only be in use when people are there. Which also happens to be the time that the ECLSS is running, including the air filtering system.
And yes, ventilation hoses will be applied between the modules. Exactly like how its done on ISS now.

Offline guckyfan

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Re: SpaceX Dragon XL
« Reply #531 on: 03/25/2021 08:00 am »
After the module has been removed from Dragon XL-based tug, and relocated to its permanent position on Gateway (by means of Canadarm 3), the Dragon XL-based tug would undock and send itself into a disposal orbit.

If I recall correctly, you said early on that the disposal will be into the Earth atmosphere on a slow low delta-v trajectory. Is this still the plan?

Offline woods170

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Re: SpaceX Dragon XL
« Reply #532 on: 03/25/2021 06:22 pm »
After the module has been removed from Dragon XL-based tug, and relocated to its permanent position on Gateway (by means of Canadarm 3), the Dragon XL-based tug would undock and send itself into a disposal orbit.

If I recall correctly, you said early on that the disposal will be into the Earth atmosphere on a slow low delta-v trajectory. Is this still the plan?

That's for Dragon XL. I haven't had it confirmed that Dragon XL-based tug would do the same.

Offline Johnnyhinbos

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Re: SpaceX Dragon XL
« Reply #533 on: 03/25/2021 06:42 pm »
Can Dragon XL be made into a tug to transfer other modules, landers, or supplies to the Artemis orbit? 

Dragon XL-based tug would be launched with the module already docked to it. The module would be where the pressurized section is on Dragon XL. So, launch on FH as a 'whole package'

FH upper stage would push the combination into lunar transfer orbit.
Dragon XL-based tug does the final job: enter NRHO, approach to Lunar Gateway and perform the docking.

After the module has been removed from Dragon XL-based tug, and relocated to its permanent position on Gateway (by means of Canadarm 3), the Dragon XL-based tug would undock and send itself into a disposal orbit.

Dragon XL is already in development for sending supplies to the Lunar Gateway. So will be a modified version of HTV-X.

Landers will get to Gateway under their own power. National Team has a Cygnus derivative for that, which serves as a transfer stage for the their lander.
Dynetics uses in-space refueling and its own engines.
So will lunar Starship: in-space refueling and its own engines.

Dragon XL-based tug is there mostly for getting modules, without their own propulsion system, to the Gateway (including the docking).
The solar panels are currently on the pressurized end of XL, so that would have to change for the tug concept, unless XL relies on power from its payload?
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Offline woods170

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Re: SpaceX Dragon XL
« Reply #534 on: 03/26/2021 08:52 am »
Can Dragon XL be made into a tug to transfer other modules, landers, or supplies to the Artemis orbit? 

Dragon XL-based tug would be launched with the module already docked to it. The module would be where the pressurized section is on Dragon XL. So, launch on FH as a 'whole package'

FH upper stage would push the combination into lunar transfer orbit.
Dragon XL-based tug does the final job: enter NRHO, approach to Lunar Gateway and perform the docking.

After the module has been removed from Dragon XL-based tug, and relocated to its permanent position on Gateway (by means of Canadarm 3), the Dragon XL-based tug would undock and send itself into a disposal orbit.

Dragon XL is already in development for sending supplies to the Lunar Gateway. So will be a modified version of HTV-X.

Landers will get to Gateway under their own power. National Team has a Cygnus derivative for that, which serves as a transfer stage for the their lander.
Dynetics uses in-space refueling and its own engines.
So will lunar Starship: in-space refueling and its own engines.

Dragon XL-based tug is there mostly for getting modules, without their own propulsion system, to the Gateway (including the docking).
The solar panels are currently on the pressurized end of XL, so that would have to change for the tug concept, unless XL relies on power from its payload?

Solar panels would be moved to the tug itself.

Offline yg1968

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Re: SpaceX Dragon XL
« Reply #535 on: 03/26/2021 11:55 am »
Can Dragon XL be made into a tug to transfer other modules, landers, or supplies to the Artemis orbit? 

Dragon XL-based tug would be launched with the module already docked to it. The module would be where the pressurized section is on Dragon XL. So, launch on FH as a 'whole package'

FH upper stage would push the combination into lunar transfer orbit.
Dragon XL-based tug does the final job: enter NRHO, approach to Lunar Gateway and perform the docking.

After the module has been removed from Dragon XL-based tug, and relocated to its permanent position on Gateway (by means of Canadarm 3), the Dragon XL-based tug would undock and send itself into a disposal orbit.

Dragon XL is already in development for sending supplies to the Lunar Gateway. So will be a modified version of HTV-X.

Landers will get to Gateway under their own power. National Team has a Cygnus derivative for that, which serves as a transfer stage for the their lander.
Dynetics uses in-space refueling and its own engines.
So will lunar Starship: in-space refueling and its own engines.

Dragon XL-based tug is there mostly for getting modules, without their own propulsion system, to the Gateway (including the docking).

Is there any plans for a Dragon-XL based tug?

Offline woods170

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Re: SpaceX Dragon XL
« Reply #536 on: 03/26/2021 02:34 pm »
Can Dragon XL be made into a tug to transfer other modules, landers, or supplies to the Artemis orbit? 

Dragon XL-based tug would be launched with the module already docked to it. The module would be where the pressurized section is on Dragon XL. So, launch on FH as a 'whole package'

FH upper stage would push the combination into lunar transfer orbit.
Dragon XL-based tug does the final job: enter NRHO, approach to Lunar Gateway and perform the docking.

After the module has been removed from Dragon XL-based tug, and relocated to its permanent position on Gateway (by means of Canadarm 3), the Dragon XL-based tug would undock and send itself into a disposal orbit.

Dragon XL is already in development for sending supplies to the Lunar Gateway. So will be a modified version of HTV-X.

Landers will get to Gateway under their own power. National Team has a Cygnus derivative for that, which serves as a transfer stage for the their lander.
Dynetics uses in-space refueling and its own engines.
So will lunar Starship: in-space refueling and its own engines.

Dragon XL-based tug is there mostly for getting modules, without their own propulsion system, to the Gateway (including the docking).

Is there any plans for a Dragon-XL based tug?

No, not 'plans'. As part of the Dragon XL contract studies are being performed to look at other roles that Dragon XL derivatives might fulfill. One of those study subjects is a Dragon XL derived tug.

So, it's not a plan. It's a study subject.

Offline yg1968

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Re: SpaceX Dragon XL
« Reply #537 on: 03/27/2021 03:06 pm »
I don't know if this is true but it would make sense:

https://twitter.com/artemis360_moon/status/1372292826977902594

Quote
Dragon XL will be used to resupply Gateway, a lunar outpost for Artemis astronauts. This resupply ship will also include a toilet and beds to provide extra space in HALO for science.
This would explain the "1 year docked" requirement a lot of us were scratching our heads at in the original GLS procurement.

In the proposed RFP, they had a 3 year docked requirement but it got reduced to one year in the final RFP.

https://forum.nasaspaceflight.com/index.php?topic=48353.msg1956785#msg1956785

https://forum.nasaspaceflight.com/index.php?topic=48353.msg2018139#msg2018139
« Last Edit: 03/27/2021 04:16 pm by yg1968 »

Offline yg1968

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Re: SpaceX Dragon XL
« Reply #538 on: 03/27/2021 03:57 pm »
It appears that SpaceX is interested in developing a commercial LEO free flying habitat (see below). I wonder if such a habitat would be based on its Dragon XL:

Interesting that SpaceX is among the companies interested in the upcoming commercial LEO free flying habitats procurement:

https://twitter.com/thesheetztweetz/status/1375799375742525440
« Last Edit: 03/27/2021 04:15 pm by yg1968 »

Offline hplan

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Re: SpaceX Dragon XL
« Reply #539 on: 03/27/2021 04:30 pm »
It appears that SpaceX is interested in developing a commercial LEO free flying habitat (see below). I wonder if such a habitat would be based on its Dragon XL:

This Dragon II platform is proving versatile and potentially useful for a variety of purposes.

Put on the capsule--HLS.

Put on the pressurized cylinder--cargo delivery to lunar orbit, Gateway module. Maybe a free flying space station.

Take off the modules--space tug.

Almost like legos!

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