Author Topic: Commercial Crew - Discussion Thread 3  (Read 345246 times)

Offline envy887

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Re: Commercial Crew - Discussion Thread 3
« Reply #260 on: 05/15/2020 02:59 pm »
In a similar vein:

twitter.com/thesheetztweetz/status/1260638187640193024

Quote
NASA's Phil McAlister notes that the Commercial Crew program represents "the largest fixed-price contracts for spacecraft development in the history of the Agency" and yet are "still within 5% of the contract baseline."
https://www.cnbc.com/2020/05/13/nasa-estimates-having-spacex-and-boeing-build-spacecraft-for-astronauts-saved-up-to-30-billion.html

Note that this was for a six person Lunar capable spacecraft with over 1 km/s delta-V and an all new launch vehicle. NASA could have developed a smaller vehicle with limited delta-V and used a commercial launch vehicle....

Dragon was baselined for high energy reentry and 7 crew, and still has about 800 m/s of delta-v and the same internal volume as Orion. So the "but Orion is much more capable" disclaimer to account for the 10x greater cost isn't particularly convincing. The cost to NASA to develop and validate Dragon (and F9) including the uncrewed test flight should be about $1.5B (taking the total $3.1B value for all SpaceX commercial crew contracts and removing 28 seats at the $55M/seat baseline price per NASA OIG).

Developing a version able to do the Orion mission, and certifying FH for the crew launch, would add some cost... but probably not multiple billions. I think SpaceX would bid between $1B and $1.5B to enhance Dragon for Gateway crew delivery, including an uncrewed test flight to the Gateway and back, if the dev contract included several guaranteed crew flights much like CCtCap.

Offline dglow

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Re: Commercial Crew - Discussion Thread 3
« Reply #261 on: 05/15/2020 03:06 pm »
Developing a version able to do the Orion mission, and certifying FH for the crew launch, would add some cost... but probably not multiple billions. I think SpaceX would bid between $1B and $1.5B to enhance Dragon for Gateway crew delivery, including an uncrewed test flight to the Gateway and back, if the dev contract included several guaranteed crew flights much like CCtCap.

If Elon gets his way and Lunar Starship returns to Earth orbit, they won't even need to do that.

Offline abaddon

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Re: Commercial Crew - Discussion Thread 3
« Reply #262 on: 05/15/2020 04:34 pm »
The pity is that Boeing pushed right in, taking a slot in Commercial Crew that could have – and, IIRC, was whispered up until the very last moment would have – gone to SNC and DreamChaser. Let's be real: DC as a cargo-only vehicle is a depressing waste of potential.
Based on more recent information that Gerst was very seriously considering a sole selection of Boeing, that whispering seems likely to have been based more on wish fulfillment than credible information.

Offline abaddon

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Re: Commercial Crew - Discussion Thread 3
« Reply #263 on: 05/15/2020 05:36 pm »
With the benefit of hindsight, thanks to multiple and varying delays to both SpaceX and Boeing for various reasons, SNC may have been able to catch up to the other (which likely would have been Boeing anyway) by now and we'd probably still be about where we are now.
Or, more likely, SNC would also have had multiple and varying delays too.  At a minimum, they would have been just as underfunded as SpaceX and Boeing actually were in the early years, with a corresponding impact on their certification timeline.

Offline ncb1397

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Re: Commercial Crew - Discussion Thread 3
« Reply #264 on: 05/15/2020 07:37 pm »

Dragon was baselined for high energy reentry and 7 crew, and still has about 800 m/s of delta-v and the same internal volume as Orion.

Not really the same internal volume. ~20 cubic meters vs 9.3 cubic meters pressurized.
« Last Edit: 05/15/2020 07:46 pm by ncb1397 »

Offline yg1968

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Re: Commercial Crew - Discussion Thread 3
« Reply #265 on: 05/16/2020 07:00 pm »
Yes, and that flawed logic came back to bite NASA in the behind...hard.

But NASA has apparently learned its lesson: Boeing was not selected for the Gateway Logistics Services contract. Boeing was also not selected for the Human Lander System. NASA has now finally understood that Boeing no longer is the “safer/known” choice.

The pity is that Boeing pushed right in, taking a slot in Commercial Crew that could have – and, IIRC, was whispered up until the very last moment would have – gone to SNC and DreamChaser. Let's be real: DC as a cargo-only vehicle is a depressing waste of potential.

SNC / DreamChaser shot itself in the foot by making the (IMO, very wise and prudent) decision to switch its primary propulsion from a hybrid system to all liquid fuel. While this was probably a really good move long-term (looking at how Virgin Galactic / SpaceShip Two is going), in the immediate term (in 2014) it put them at least a year behind Boeing and SpaceX in terms of schedule. Keep in mind NASA was at that point looking to start commercial crew rotations in 2017. With the benefit of hindsight, thanks to multiple and varying delays to both SpaceX and Boeing for various reasons, SNC may have been able to catch up to the other (which likely would have been Boeing anyway) by now and we'd probably still be about where we are now.

All true and valid, and I know that hindsight offers perfect vision. But DC development has continued, nonetheless, and we will see it flying to ISS. I just wish its development had continued as part of CC instead of CRS2.

CCtCap has a maximum of 6 post-certification flights per company. If NASA decides to have a new commercial crew contract after CCtCap, SNC would have a chance. CCtCap also has an on-ramp clause.
« Last Edit: 05/16/2020 08:45 pm by yg1968 »

Offline woods170

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Re: Commercial Crew - Discussion Thread 3
« Reply #266 on: 05/16/2020 08:11 pm »

Dragon was baselined for high energy reentry and 7 crew, and still has about 800 m/s of delta-v and the same internal volume as Orion.

Not really the same internal volume. ~20 cubic meters vs 9.3 cubic meters pressurized.

Unfortunately, you are partly mistaken.

The TOTAL pressurized volume of Orion is 19.6 cubic meters. But, over half of that volume (10.7 cubic meters) is reserved for stowage space. The actual HABITABLE volume of Orion is only 8.9 cubic meters.

SpaceX, on its website lists the volume of Crew Dragon as 9.3 cubic meters. What they didn't mention was that this figure represents the HABITABLE volume of Crew Dragon.
The TOTAL pressurized volume of Crew Dragon is 12.5 cubic meters. 3.2 Cubic meters of this is "under the floor" (stowage and systems).

So, when envy887 stated that Crew Dragon and Orion have the same internal volume, he was partly correct. Correct on HABITABLE volume. Incorrect on total pressurized volume.

Offline ncb1397

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Re: Commercial Crew - Discussion Thread 3
« Reply #267 on: 05/17/2020 05:48 am »

Dragon was baselined for high energy reentry and 7 crew, and still has about 800 m/s of delta-v and the same internal volume as Orion.

Not really the same internal volume. ~20 cubic meters vs 9.3 cubic meters pressurized.

Unfortunately, you are partly mistaken.

The TOTAL pressurized volume of Orion is 19.6 cubic meters. But, over half of that volume (10.7 cubic meters) is reserved for stowage space. The actual HABITABLE volume of Orion is only 8.9 cubic meters.

SpaceX, on its website lists the volume of Crew Dragon as 9.3 cubic meters. What they didn't mention was that this figure represents the HABITABLE volume of Crew Dragon.
The TOTAL pressurized volume of Crew Dragon is 12.5 cubic meters. 3.2 Cubic meters of this is "under the floor" (stowage and systems).

So, when envy887 stated that Crew Dragon and Orion have the same internal volume, he was partly correct. Correct on HABITABLE volume. Incorrect on total pressurized volume.

The traditional definition of net habitable volume is this:

Quote
Net habitable volume is defined for this study as the pressurized volume left available to the
crew after accounting for the Loss of Volume (LOV) due to deployed equipment, stowage,
trash, and any other structural inefficiency that decreases functional volume. The gravity
environment corresponding to the habitable volume must also be taken into consideration. Net
habitable volume is the volume the crew has at their disposal to perform all of their operations.
In order to estimate the net habitable volume requirement for the CEV for each phase of flight,
this study first looked at the crewed operations required in the spacecraft, what operations
must be done simultaneously, how many crew members might be expected to perform each
operation, how long each operation might last, how often each operation might be required
during the mission, the complexity of the task, and the potential impact to the task by vehicle
structure, shape, and gravity environment. The analysis took into account the entire spacecraft
pressurized volume and the estimated volume and layout of internal systems equipment and
stowage volumes by mission type and phase. Pressurized and net habitable volumes of previous and current spacecraft were used for comparison. Full-scale rough mockups were made
for the internal volumes of both the CEV CM and LSAM to assist in the visualization and
evaluation process.
https://www.nasa.gov/pdf/140636main_ESAS_05.pdf

Those variables are flight profile and nominal mission dependent (stowage/trash for instance), and as such aren't necessarily directly comparable. For instance, if you were to increase the crew dragon duration on orbit (free flying) by 10x, habitable volume for the crew to work in would necessarily decrease. It is a human factors calculation derived based on a number of assumptions, and isn't necessarily transferable between spacecraft. Sure, if you subtract ~11 cubic meters from Orion and ~3 from Dragon, they are the same size. Anyways, both photos below are each system occupied by 4 astronauts. You can literally fit Dragon's crew compliment in one section of the floor of Orion.
« Last Edit: 05/17/2020 05:51 am by ncb1397 »

Offline envy887

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Re: Commercial Crew - Discussion Thread 3
« Reply #268 on: 05/17/2020 07:05 pm »
if you were to increase the crew dragon duration on orbit (free flying) by 10x, habitable volume for the crew to work in would necessarily decrease.

I was referring to habitable volume, since I couldn't find the total pressurized volume. As woods was kind enough to provide it, we can make a better comparison: Dragon has about 60% of pressurized volume and 60% of the delta-v, but only about 35% of the liftoff mass of Orion.

Dragon is advertised as capable of 20 person-days of free flight. The nominal Gateway mission is IIRC not 10x but about 2x that: 4 crew for 5 or 6 days each way, remainder of the flight docked at Gateway. How much would the habitable volume decrease with doubling the flight time?
« Last Edit: 05/17/2020 07:16 pm by envy887 »

Offline dglow

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Re: Commercial Crew - Discussion Thread 3
« Reply #269 on: 05/18/2020 02:31 am »
How much would the habitable volume decrease with doubling the flight time?

I wonder if it needs to decrease at all. Why couldn't Dragon's trunk house additional consumables and other gear, SM-style?

Offline envy887

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Re: Commercial Crew - Discussion Thread 3
« Reply #270 on: 05/18/2020 02:14 pm »
How much would the habitable volume decrease with doubling the flight time?

I wonder if it needs to decrease at all. Why couldn't Dragon's trunk house additional consumables and other gear, SM-style?

Hard consumables and other things the crew needs to access have to go inside the pressure vessel.

But fluids, and equipment that handles fluids, could go in the trunk. For example, if they need to increase capacity for scrubbing CO2, they could pump air to scrubbers in the trunk and then back into the crew compartment.

Offline dglow

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Re: Commercial Crew - Discussion Thread 3
« Reply #271 on: 05/18/2020 03:24 pm »
How much would the habitable volume decrease with doubling the flight time?

I wonder if it needs to decrease at all. Why couldn't Dragon's trunk house additional consumables and other gear, SM-style?

Hard consumables and other things the crew needs to access have to go inside the pressure vessel.

But fluids, and equipment that handles fluids, could go in the trunk. For example, if they need to increase capacity for scrubbing CO2, they could pump air to scrubbers in the trunk and then back into the crew compartment.

Okay, thanks; so extra O2/H2/H2O in the trunk. What types of lines and connections are currently present on Dragon's trunk umbilical? At minimum there must be some comms and power from the solar. How is the radiator handled?

Also, allow me to ask, if Dragon needed additional delta-V (for, let's say, Gateway rendezvous) what would make most sense: propellant tanks in the trunk feeding the onboard Dracos, or feeding a separate engine housed within the trunk?
« Last Edit: 05/18/2020 03:28 pm by dglow »

Offline abaddon

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Re: Commercial Crew - Discussion Thread 3
« Reply #272 on: 05/18/2020 04:17 pm »
I feel like we're straying away from Commercial Crew Dragon, and into "how can we make Crew Dragon into Orion" isn't really on topic for this thread.

Offline envy887

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Re: Commercial Crew - Discussion Thread 3
« Reply #273 on: 05/18/2020 04:40 pm »
I feel like we're straying away from Commercial Crew Dragon, and into "how can we make Crew Dragon into Orion" isn't really on topic for this thread.

Agreed. There is actually a thread for this:

Are Commercial Crew Vehicles Usable or Upgradeable for Beyond-LEO Needs?

Offline dglow

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Re: Commercial Crew - Discussion Thread 3
« Reply #274 on: 05/18/2020 04:47 pm »
I feel like we're straying away from Commercial Crew Dragon, and into "how can we make Crew Dragon into Orion" isn't really on topic for this thread.

Boo, hiss. Light inquiry into the nature and potential limits of CC vehicle performance feels on-topic to me. Probably less so the comparisons to Orion, which began further upthread.

"Could Starliner or Dragon ferry crew to Gateway?"   Perfectly legitimate here, IMO.
"Would NASA ever do (or Congress fund) this?"   Belongs in another thread.


Agreed. There is actually a thread for this:

Are Commercial Crew Vehicles Usable or Upgradeable for Beyond-LEO Needs?

Sure, but that thread hasn't seen activity since August of 2017. So let's be real, we gravitate to the places people are talking - right?

Offline FutureSpaceTourist

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Re: Commercial Crew - Discussion Thread 3
« Reply #275 on: 05/20/2020 01:41 pm »
Quote
The numbers don’t lie—NASA’s move to commercial space has saved money
“Together, we have become stronger for this nation.”

ERIC BERGER - 5/20/2020, 12:30 PM

When NASA astronauts Doug Hurley and Bob Behnken blast off inside a Crew Dragon spacecraft later this month, they will not only launch into space. They will also inaugurate a potentially transformative era for the space agency.

No private company has ever launched humans into orbit before. Therefore the success of their mission, and others to come in the near future, may go a long way toward determining whether the promise of commercial spaceflight and lower cost access to space becomes the new reality.

https://arstechnica.com/features/2020/05/the-numbers-dont-lie-nasas-move-to-commercial-space-has-saved-money/

Offline woods170

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Re: Commercial Crew - Discussion Thread 3
« Reply #276 on: 05/20/2020 02:09 pm »
Quote
The numbers don’t lie—NASA’s move to commercial space has saved money
“Together, we have become stronger for this nation.”

ERIC BERGER - 5/20/2020, 12:30 PM

When NASA astronauts Doug Hurley and Bob Behnken blast off inside a Crew Dragon spacecraft later this month, they will not only launch into space. They will also inaugurate a potentially transformative era for the space agency.

No private company has ever launched humans into orbit before. Therefore the success of their mission, and others to come in the near future, may go a long way toward determining whether the promise of commercial spaceflight and lower cost access to space becomes the new reality.

https://arstechnica.com/features/2020/05/the-numbers-dont-lie-nasas-move-to-commercial-space-has-saved-money/

Ouch!

Former shuttle astronaut Scott Horowitz just got toasted by Eric Berger over his involvement in Ares I.
If Scott Horowitz really did make that ludicrous $400 million comparison between Ares I-X and F9 v1.0... not good.
« Last Edit: 05/20/2020 02:50 pm by woods170 »

Offline Nomadd

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Re: Commercial Crew - Discussion Thread 3
« Reply #277 on: 05/20/2020 03:22 pm »
Quote
The numbers don’t lie—NASA’s move to commercial space has saved money
“Together, we have become stronger for this nation.”

ERIC BERGER - 5/20/2020, 12:30 PM

When NASA astronauts Doug Hurley and Bob Behnken blast off inside a Crew Dragon spacecraft later this month, they will not only launch into space. They will also inaugurate a potentially transformative era for the space agency.

No private company has ever launched humans into orbit before. Therefore the success of their mission, and others to come in the near future, may go a long way toward determining whether the promise of commercial spaceflight and lower cost access to space becomes the new reality.

https://arstechnica.com/features/2020/05/the-numbers-dont-lie-nasas-move-to-commercial-space-has-saved-money/

Ouch!

Former shuttle astronaut Scott Horowitz just got toasted by Eric Berger over his involvement in Ares I.
If Scott Horowitz really did make that ludicrous $400 million comparison between Ares I-X and F9 v1.0... not good.
  I thought you were exaggerating with the ludicrous comment until I read the article. Sorry.
 It boggles the mind that someone who's supposedly intelligent could think he'd get away with nonsense like that. It's like comparing the cost of buying an updated Dodge Ram at the dealership to the cost of designing, developing and building the manufacturing facilities for a Model S.
 Did he forget minor items like "$1.8 billion to begin design work"?
 What a way to finish up your legacy after a career like that.
« Last Edit: 05/20/2020 03:24 pm by Nomadd »
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Offline yg1968

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Re: Commercial Crew - Discussion Thread 3
« Reply #278 on: 06/01/2020 01:12 pm »
I missed it when it came out in November 2019 but this OIG report has the price per seat for commercial crew:

Quote from: page 4 of OIG Report
As of May 2019, Boeing and SpaceX’s contracts were valued at $4.3 billion and $2.5 billion, respectively. Of those amounts, Boeing’s costs for development and test flights were $2.2 billion, while SpaceX’s were $1.2 billion. For crewed missions to the ISS, NASA awarded each contractor six round-trip missions. Assuming four astronauts per flight and using publicly available information, the estimated average cost per seat is approximately $90 million for Boeing and approximately $55 million for SpaceX, potentially providing cost savings over current Soyuz prices.[6]

[6] The average cost per seat was calculated by taking the total contract value and subtracting the development and test flight costs (previously disclosed in NASA’s fiscal year 2020 budget request) and the special studies costs (disclosed in past Government Accountability Office reports) to determine the total mission cost for each contractor. This number was divided by the 24 seats currently assumed over the contactors’ six confirmed missions. These figures were calculated using publicly available information and are averages, not exact costs.

Quote from: page 21 of OIG Report
Due to slippage in the commercial crew schedule, in March 2018 NASA purchased two additional Soyuz seats for $86 million each, one for the September 2019 Soyuz flight and another on the upcoming April 2020 mission.

https://oig.nasa.gov/docs/IG-20-005.pdf

However, Boeing disputes these prices per seat namely because it doesn't take into account the potential 5th seat on Starliner (which can be replaced with cargo):

Quote
In regards to to the per-seat cost estimate, Boeing said that its craft "will fly the equivalent of a fifth passenger in cargo for NASA, so the per-seat pricing should be considered based on five seats rather than four."

https://www.spacedaily.com/reports/Boeing_Starliner_to_cost_90_Million_per_seat_999.html
« Last Edit: 06/03/2020 12:01 am by yg1968 »

Re: Commercial Crew - Discussion Thread 3
« Reply #279 on: 06/01/2020 01:44 pm »
Quote
However, Boeing dispute these prices per seat namely because it doesn't take into account the potential 5th seat on Starliner (which can be replaced with cargo):

Quote
In regards to to the per-seat cost estimate, Boeing said that its craft "will fly the equivalent of a fifth passenger in cargo for NASA, so the per-seat pricing should be considered based on five seats rather than four."

https://www.spacedaily.com/reports/Boeing_Starliner_to_cost_90_Million_per_seat_999.html

What does this even mean... both Dragon and Starliner have theoretical capacity for 7 seats.
‘The equivalent of a fifth passenger in cargo’ sounds like nonsense to me, comparing apples to oranges. Is Dragon’s cargo capacity even lower than Starliner’s, never mind lower enough to justify a 35*4= 140 million $ difference in cost per mission?
« Last Edit: 06/01/2020 01:47 pm by AbuSimbel »
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