Author Topic: SpaceX Dragon 2 Updates and Discussion - Thread 3  (Read 815064 times)

Offline cuddihy

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #540 on: 12/22/2018 09:39 pm »
Given that most the solar cells will be getting an incident angle <90 (because they’re on a cylinder), I wonder if they have done any optical lensing /layering tricks with the cells to maximize conversion at a suboptimal angle?

So I’ve forgotten a lot of trig but naively it should convert about the same area as a flat panel with width of the trunk diameter.

Offline Zed_Noir

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #541 on: 12/23/2018 08:39 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.

Would adding fixed fins on the Dragon do the same function as the trunk aerodynamically?

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.

Think onboard batteries is adequate for the suborbital flight of maybe 12 minutes or so. The Cargo Dragon have to run on batteries until separation from the upper stage on the CRS cargo runs to the ISS.

As for the heat generated by the electronics maybe installed a chilled water tank as a heatsink for the short flight duration between capsule separation and interface with the atmosphere.
.

Offline woods170

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #542 on: 12/23/2018 10:47 am »
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.

Emphasis mine.

From what I hear from sources: H*ll no those batteries are not short-lived. On a fully charged set Crew Dragon can go for nearly two days without them being recharged.
Theoretically Crew Dragon can go from launch to docking to the ISS without having the need for the solar cells at all.

Online clongton

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #543 on: 12/23/2018 12:44 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.

Emphasis mine.

From what I hear from sources: H*ll no those batteries are not short-lived. On a fully charged set Crew Dragon can go for nearly two days without them being recharged.
Theoretically Crew Dragon can go from launch to docking to the ISS without having the need for the solar cells at all.

I did not know that. Thank's Woods
« Last Edit: 12/23/2018 12:44 pm by clongton »
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Offline rockets4life97

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #544 on: 12/23/2018 01:10 pm »
I'm not surprised on the battery front. You would think the CEO of Tesla would know something about batteries.

Offline RonM

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #545 on: 12/23/2018 04:27 pm »
Would adding fixed fins on the Dragon do the same function as the trunk aerodynamically?

No, the center of pressure needs to be sufficiently aft of the center of gravity for the vehicle to be aerodynamically stable.

Offline DistantTemple

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #546 on: 12/23/2018 11:55 pm »
Would adding fixed fins on the Dragon do the same function as the trunk aerodynamically?

No, the center of pressure needs to be sufficiently aft of the center of gravity for the vehicle to be aerodynamically stable.
The trunk separates from Dragon after re-entry "burn" (RCS), but before atmospheric "interface", so the trunk has no aerodynamic function on re-entry. I assume any affect during launch can be mitigated.

Edit: The purpose of the trunk is, external storage, photovoltaic platform, and radiator platform, and mounting to second stage. No aerodynamic purpose I think.
« Last Edit: 12/23/2018 11:59 pm by DistantTemple »
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Offline IanThePineapple

Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #547 on: 12/24/2018 12:09 am »
Would adding fixed fins on the Dragon do the same function as the trunk aerodynamically?

No, the center of pressure needs to be sufficiently aft of the center of gravity for the vehicle to be aerodynamically stable.
The trunk separates from Dragon after re-entry "burn" (RCS), but before atmospheric "interface", so the trunk has no aerodynamic function on re-entry. I assume any affect during launch can be mitigated.

Edit: The purpose of the trunk is, external storage, photovoltaic platform, and radiator platform, and mounting to second stage. No aerodynamic purpose I think.

Its aerodynamic purpose is during an abort scenario, using its fins to keep the capsule facing forward until trunk jettison. If there's no abort, its aerodynamic purpose isn't used.

Offline Llian Rhydderch

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #548 on: 12/27/2018 12:28 am »

I agree it is a stretch at this point.  I was merely trying to come up with reasons for the existence for a manual abort switch/lever/button.  I am well past my instinct that there should be manual "flight controls" and just trying to poke the corners of the envelope to (dis)prove the need for some who seem to insist in favor of these manual controls.

Emphasis mine.

Neither the original design for Crew Dragon, nor the original design for Starliner, had manual abort capabilities. Manual abort capabilities were added because NASA asked the CCP providers to do so.


NASAs gotta have a few manual controls.  It helps to justify the fleet of NASA owned and maintained twin-engine supersonic T-38's for all the NASA pilot astronauts.

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Offline Lars-J

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #549 on: 12/27/2018 02:36 am »
The grip of the astronaut "pilot (sorry, need to stop here for a second and just say that I have to use stupid words to get my point across. I know that means I must have a weak argument, but that's why I use bad words)." over NASA human spaceflight is strong but loosening. Thankfully it will be gone soon.

Offline gongora

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #550 on: 12/27/2018 02:52 am »
The grip of the astronaut "pilot (sorry, need to stop here for a second and just say that I have to use stupid words to get my point across. I know that means I must have a weak argument, but that's why I use bad words)." over NASA human spaceflight is strong but loosening. Thankfully it will be gone soon.

What the... oh yeah, Chris put in that autocorrect for the M-word  ;D

Offline Lars-J

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #551 on: 12/27/2018 04:17 am »
The grip of the astronaut "pilot (sorry, need to stop here for a second and just say that I have to use stupid words to get my point across. I know that means I must have a weak argument, but that's why I use bad words)." over NASA human spaceflight is strong but loosening. Thankfully it will be gone soon.

What the... oh yeah, Chris put in that autocorrect for the M-word  ;D

Lol. I had no idea the dreaded M-word was banned here.

Offline zubenelgenubi

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #552 on: 12/27/2018 05:18 am »
Late to the party here...what's the M-word? :P

What does it rhyme with? ;)
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Offline su27k

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #553 on: 12/27/2018 09:42 am »
Late to the party here...what's the M-word? :P

What does it rhyme with? ;)

Criminal organization originated from Italy...

Anyway, NASA explains T-38 is needed to train astronauts to do technical work under stressful situations, I don't disagree.
« Last Edit: 12/27/2018 09:44 am by su27k »

Offline meekGee

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #554 on: 12/27/2018 05:11 pm »
Late to the party here...what's the M-word? :P

What does it rhyme with? ;)

Criminal organization originated from Italy...

Anyway, NASA explains T-38 is needed to train astronauts to do technical work under stressful situations, I don't disagree.

That's why bomb-squad personnel get them too.  And deep-sea divers.  And test pilots.   :)
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Offline woods170

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #555 on: 12/27/2018 05:46 pm »
Late to the party here...what's the M-word? :P

What does it rhyme with? ;)

Criminal organization originated from Italy...

M*ffia

* Replace with "a".

Offline Rocket Science

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #556 on: 12/27/2018 09:23 pm »

I agree it is a stretch at this point.  I was merely trying to come up with reasons for the existence for a manual abort switch/lever/button.  I am well past my instinct that there should be manual "flight controls" and just trying to poke the corners of the envelope to (dis)prove the need for some who seem to insist in favor of these manual controls.

Emphasis mine.

Neither the original design for Crew Dragon, nor the original design for Starliner, had manual abort capabilities. Manual abort capabilities were added because NASA asked the CCP providers to do so.


NASAs gotta have a few manual controls.  It helps to justify the fleet of NASA owned and maintained twin-engine supersonic T-38's for all the NASA pilot astronauts.

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Online clongton

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #557 on: 12/27/2018 09:23 pm »
Neither the original design for Crew Dragon, nor the original design for Starliner, had manual abort capabilities. Manual abort capabilities were added because NASA asked the CCP providers to do so.

Woods, any idea for the official rationale for that decision?
Are the manual abort controls actually functional?
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Offline Lar

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #558 on: 12/28/2018 12:28 pm »
I hear Staples can give you a good deal on an "Easy" button.

More seriously a "manual abort" really  means telling the computer to change plans, no? And what it does in response depends on where you are in the ascent profile?
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Offline woods170

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Re: SpaceX Dragon 2 Updates and Discussion - Thread 3
« Reply #559 on: 12/28/2018 01:50 pm »
I hear Staples can give you a good deal on an "Easy" button.

More seriously a "manual abort" really  means telling the computer to change plans, no? And what it does in response depends on where you are in the ascent profile?

Yup. This.

The abort handle in Crew Dragon basically tells the flight computer to take Crew Dragon back home the soonest possible way. So what that "soonest possible" actually is very much depends on where Crew Dragon is in the ascent profile.

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