Author Topic: SpaceX Dragon 2 Updates and Discussion - Thread 3  (Read 965039 times)

Offline woods170

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #260 on: 08/28/2018 08:44 am »
Can someone explain this detail from the DM1 presentation? Landing Legs???

NASA, in these slides, used a generic, and out-of-date, SpaceX flow diagram for Crew Dragon.
People seem to be forgetting that landing legs were only deleted from NASA missions AFTER the design for Crew Dragon was almost completely done.

Offline kevinof

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #261 on: 08/28/2018 08:50 am »
My thoughts exactly.  Legs are long gone (and 99% chance they are never coming back).

Can someone explain this detail from the DM1 presentation? Landing Legs???

NASA, in these slides, used a generic, and out-of-date, SpaceX flow diagram for Crew Dragon.
People seem to be forgetting that landing legs were only deleted from NASA missions AFTER the design for Crew Dragon was almost completely done.

Offline woods170

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #262 on: 08/28/2018 12:19 pm »
Also I wonder whether "pilot(s)" will have some emergency buttons/joystick directly on the arm rest of their seats or will hold something in their hand as in Soyuz comander has now days. Some unexpected g-loads & vibrations might cause difficulty to rise their hand(s) up to the dash board and press or pull anything there.

Crew Dragon is highly automated. During the ascent phase the crew really isn't crew. They are passengers. The entire ascent to orbit is fully automated, including all the abort modes. No silly abort-mode switches or joysticks (a la Shuttle) or manual abort handles (a al Apollo). None of that stuff.
If a comsat can get to orbit fully autonomously on a regular F9 than why should Crew Dragon be different? By the time the crew finally realizes something is wrong with the rocket the computer has already executed the proper abort mode. Computers far out-perform humans in this regard. Why do you think ranges are switching over to AFTS for example?

The only manual intervention modes available are on-orbit, when you are not hampered by high G-loads. Like manually intervening in the approach to ISS or manually intervening in the final phases of docking. That why there are controls for the RCS engines. There is also an option to do a manual de-orbit. But the descent phase itself, including entry and the parachute stages is again fully autonomous.

Coming back to my own post because I finally found the Kathy Lueders (NASA program manager for CCP) quote on which my previous reply (see bolding above) was based:

https://www.nasa.gov/johnson/HWHAP/launch-america

Quote from: NASA
Host:  And this might get into the weeds a little bit, but how much-- so, these new spacecraft, are they going to be-- because, for example, the Russian Soyuz, largely automated, automated docking, you know, the crew has some tasks on board, mission control is largely monitoring.  Shuttle was a lot of, you know, onboard flying for the crew and stuff like that.  Where are these vehicles going to kind of fall and are they-- again, are they different?

Kathy Lueders:  So, I think both of them are fairly autonomous.  If you think about it, it kind of goes back to once again the commercial concept.  Right?  If you're a company that wants to have control over how your vehicle is operating and with the capabilities they have today, with computer-- the processing capability and everything else-- they're really developing very sophisticated autonomous rendezvous and docking and reentry capabilities.  And so, really crew is there as a monitoring function and back up in case some-- like something really goes wrong, but these, they're really-- both companies are designing their spacecraft to be two-fault tolerant to a failure.  All along the way.  Very robust, which is really our intent.  We wanted to have very robust vehicles.  Right?  Very robust vehicles.  We asked them to design their vehicles to be two-fault tolerant and to not have crew as a control.  So, we-- that was a-- kind of goes back to safe and reliability being kind of important tenets and the companies have really come through.

They have different strategies for how they do that and they'll be checking out that autonomous capability on their first demonstrations because they'll be uncrewed [phonetic].  They'll be uncrewed demonstrations to the ISS, so that will kind of prove out that autonomous capability.  I always tell people I'm-- I know we've got self-driving cars out there, but I'm really hoping that before they roll out their first commercial one, the first commercial self-driving crew vehicle that's being bought by the government is going to be a crew transportation vehicle that's going to the ISS and so--

In short: NASA asked the CCP providers for highly autonomous vehicles where the crew only interferes when all other options are exhausted. Hence my "the crew really isn't crew" remark.

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #263 on: 08/28/2018 08:35 pm »
ARTICLE: NAC provides Starliner, Dragon 2 update – Commercial Crew preps entering final leg to launch -

https://www.nasaspaceflight.com/2018/08/nac-starliner-dragon-2-preps-final-leg-launch/

- By Michael Baylor

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Offline Ludus

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #265 on: 08/29/2018 01:51 pm »
Just a little detail: Tesla Model X will carry first astronauts flying in SpaceX’s Dragon spacecraft to launch pad (Electrek.co)

The electrek story has this rendering of the Dragon2 on the pad with completed FSS covering.

Offline douglas100

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #266 on: 08/29/2018 03:07 pm »
The strongback is on the wrong side of the vehicle in the picture and the slide wire escape system doesn't appear to have been moved up to the CAA level.
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Offline Joffan

Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #267 on: 08/29/2018 03:18 pm »
The strongback is on the wrong side of the vehicle in the picture and the slide wire escape system doesn't appear to have been moved up to the CAA level.

Oh, fake photo criticism... apparently they're using child astronauts (scale of standing figure), who will have to walk along the top of the access arm and jump into the capsule from halfway along.
Getting through max-Q for humanity becoming fully spacefaring

Offline jpo234

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You want to be inspired by things. You want to wake up in the morning and think the future is going to be great. That's what being a spacefaring civilization is all about. It's about believing in the future and believing the future will be better than the past. And I can't think of anything more exciting than being out there among the stars.

Offline jpo234

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #269 on: 08/29/2018 03:54 pm »
The strongback is on the wrong side of the vehicle in the picture and the slide wire escape system doesn't appear to have been moved up to the CAA level.

The creator of the render was aware of that:

Quote
Yeah, that was clear to me. But I felt it important that people see the block V Falcon 9 in all its glory.
You want to be inspired by things. You want to wake up in the morning and think the future is going to be great. That's what being a spacefaring civilization is all about. It's about believing in the future and believing the future will be better than the past. And I can't think of anything more exciting than being out there among the stars.

Offline Draggendrop

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #270 on: 08/30/2018 04:39 am »
Just had a question..which probably borders on being silly....

For context, I was visualizing commercial crew up and running with a 7 person crew at ISS. If this where to entail 6 month rotations between CC and 6 month rotation between Soyuz and a mid stagger between  CC and Soyuz exchange....what would this do for contingency planning for emergencies such as medical or a capsule repair issue. I eventually talked myself into these scenarios being very rare but still ended up wondering...if an automated empty Dragon 2 was sent early to the ISS...

With Dragon 2 seating...would someone in a Boeing suit or an Orlan suit be able to at least sit in a Dragon 2 seat and be buckled in?

If they can be buckled in...would it be at least possible to use an adapter for the Dragon 2 umbilical to supply consumables to the other 2 suit types to enable getting someone home (under admittedly a far fetched scenario)?

 

Offline Roy_H

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #271 on: 08/30/2018 05:24 am »
Just had a question..which probably borders on being silly....

For context, I was visualizing commercial crew up and running with a 7 person crew at ISS. If this where to entail 6 month rotations between CC and 6 month rotation between Soyuz and a mid stagger between  CC and Soyuz exchange....what would this do for contingency planning for emergencies such as medical or a capsule repair issue. I eventually talked myself into these scenarios being very rare but still ended up wondering...if an automated empty Dragon 2 was sent early to the ISS...

With Dragon 2 seating...would someone in a Boeing suit or an Orlan suit be able to at least sit in a Dragon 2 seat and be buckled in?

If they can be buckled in...would it be at least possible to use an adapter for the Dragon 2 umbilical to supply consumables to the other 2 suit types to enable getting someone home (under admittedly a far fetched scenario)?

If a Dragon was to be sent up on and emergency mission, I think they would most likely send it up with SpaceX suits sized to fit anybody that did not have a SpaceX suit. If that was not possible (for time reasons) then the next best option would be to come down without a suit. The suits are only for emergency depressurization, a very unlikely scenario and I wouldn't be surprised if the astronauts would be fine with that after a few flights proving reliability of both Dragon and Starliner.
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Offline russianhalo117

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #272 on: 08/30/2018 06:15 am »
Just had a question..which probably borders on being silly....

For context, I was visualizing commercial crew up and running with a 7 person crew at ISS. If this where to entail 6 month rotations between CC and 6 month rotation between Soyuz and a mid stagger between  CC and Soyuz exchange....what would this do for contingency planning for emergencies such as medical or a capsule repair issue. I eventually talked myself into these scenarios being very rare but still ended up wondering...if an automated empty Dragon 2 was sent early to the ISS...

With Dragon 2 seating...would someone in a Boeing suit or an Orlan suit be able to at least sit in a Dragon 2 seat and be buckled in?

If they can be buckled in...would it be at least possible to use an adapter for the Dragon 2 umbilical to supply consumables to the other 2 suit types to enable getting someone home (under admittedly a far fetched scenario)?

If a Dragon was to be sent up on and emergency mission, I think they would most likely send it up with SpaceX suits sized to fit anybody that did not have a SpaceX suit. If that was not possible (for time reasons) then the next best option would be to come down without a suit. The suits are only for emergency depressurization, a very unlikely scenario and I wouldn't be surprised if the astronauts would be fine with that after a few flights proving reliability of both Dragon and Starliner.
Astronauts that rotated on shuttle had both ACES and Sokol suits on orbit.

Offline Draggendrop

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #273 on: 08/31/2018 01:15 am »
Thank you for answering, much appreciated...and sorry about Orlan typo, I was looking at my Sokol images and still typed Orlan...I have too much fun watching EVA's... :)

Offline su27k

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #274 on: 09/01/2018 05:21 pm »
Two DM-1 images captured from the new Commercial Crew video:


Offline Scylla

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #275 on: 09/06/2018 02:34 pm »
Inside SpaceX HQ and their new Dragon Capsule

Everyday Astronaut

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #276 on: 09/09/2018 05:54 am »
Inside SpaceX HQ and their new Dragon Capsule

Everyday Astronaut

They mentioned that the seats actually move to allow easy entrance and then again to allow easy access to the controls so you don't have to use the Soyuz poker stick. I hadn't seen that mentioned before, has anyone else?
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Offline nacnud

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #277 on: 09/09/2018 11:16 am »
Yep it was mentioned by the Everyday Astronaut a few weeks ago though I've not seen it mentioned elsewhere. I would think that moveable seats would make getting in and out on Earth much easier. 

Offline su27k

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #278 on: 09/12/2018 02:27 am »
Based on the Gwynne Shotwell quote from Jeff Foust's tweet:

Quote
Shotwell: decline in GEO business is not a “crushing blow” for us. Seeing strong growth in DOD business, but also later with commercial crew: “7 billion potential payloads”

Sounds like there will be space tourism flights using Crew Dragon. I wonder if the lunar flyby plan will be restored, just like how Gwynne saved FH from cancellation.

Offline speedevil

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #279 on: 09/12/2018 09:34 am »
Based on the Gwynne Shotwell quote from Jeff Foust's tweet:

Quote
Shotwell: decline in GEO business is not a “crushing blow” for us. Seeing strong growth in DOD business, but also later with commercial crew: “7 billion potential payloads”

Sounds like there will be space tourism flights using Crew Dragon. I wonder if the lunar flyby plan will be restored, just like how Gwynne saved FH from cancellation.

The 7 billion doesn't sound like it could be crew dragon. Mature BFR P2P could be loosely described as 'everyone' (neglecting many people can't hope to afford $1K). $1-10M really can't.

I think she's just loosely referring to tourism possibilities and not tying it to a platform in her mind.

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