Author Topic: Jim's "Myth" thread: CxP's only problem was that it was underfunded.  (Read 130882 times)

Offline savuporo

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Re: Myth: CxP's only problem was that it was underfunded.
« Reply #40 on: 05/28/2010 09:05 pm »
....we need to drop the cost of access to space both by-the-kilogram and by the cubic meter. Griffin chose to do this with mass fraction by building a massive launcher...

I actually agree almost 100% with this paragraph.

~Jon

I dont. Griffin never made a choice to reduce launch costs. ( he made a lot of other choices, like attempting to gear everything up for a direct-to mars launch etc, but no choice about launch costs )
Orion - the first and only manned not-too-deep-space craft

Offline gospacex

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Re: Myth: CxP's only problem was that it was underfunded.
« Reply #41 on: 05/28/2010 09:26 pm »
I too believe that Constellation was never funded to a level to ensure success. One of the reasons Apollo succeeded was because it received generous funding early on. The cuts came later. But if one didn't know better, one could claim that Constellation was *deliberately* programmed for failure from the beginning. But I struggle to understand how anyone could have believed Constellation was going to get some sort of Magic-Beanstalk, "somehow, someday, you'll see!" funding boost to finally come into focus after Shuttle. Especially in this era of post-Hurricane Katrina, two wars and the world economic meltdown. The architects of Constellation needed to think smarter, think more pragmatically to ensure Constellation could somehow be made "cancel-proof". Not create some wish-list of fantasy Mega-rockets that nobody was going to pay for, for decades to come.

Now, we are seeing a similar "somehow, someday, you'll see!" faith-based approach to the so-called "Obama spaceplan". WHO is going to ensure the new plan -- such as it is -- is cancel-proof? WHO is going to make hard decisions to preserve sensible goals and destinations? WHAT destination? WHERE? At least with the Moon, mankind could learn (or is that relearn?) how to traverse the solar system and adapt the vehicles and technologies for other missions. But building vehicles to land on Asteroids will mean you can land on... Asteroids and not much else.

America needs to do better. It CAN do better in space. Constellation doesn't need cancellation; it needs pragmatic alteration

Yes, an alteration which makes it possible to fail. NASA was not (and even now still is not) going to lose its $20bn/y however badly it performs. Musk has no such cushion. Therefore he must succeed or disappear.

Offline gospacex

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Re: Myth: CxP's only problem was that it was underfunded.
« Reply #42 on: 05/28/2010 09:28 pm »
Don't build a launch vehicle around a fixed first stage and expect to get all of your spacecraft requirements to be met.

Clearly this is the fundamental flaw in the overall Constellation design. All other issues with Constellation arise from or become much more difficult/expensive to solve because of this.

One question I would like to see answered is why this mistake was committed? We've all heard of Griffin's "my way or the highway" style of management, and we all know of the then NASA IG's "ineffectiveness" that allowed all sorts of abuses to happen, but Griffin was supposed to be a smart and talented designer. Was this a case of hubris, false pride, graft, institutional inertia, or something else that let such a fundamental flaw continue on so long that it might be impossible to kill?

Power corrupts, and similarly availability of steady stream of non-earned funds corrupts, just in s lightly other ways: you stop designing to budget...

Offline robertross

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Re: Myth: CxP's only problem was that it was underfunded.
« Reply #43 on: 05/29/2010 12:42 am »
I'm sorry, but you are wrong.
They clearly said we could build the rockets right now, without all the R&D being proposed. That isn't a position for 'large rockets', it's one of conservative use of existing capabilities.

I said development program, not research.  Development is required for CxP or any other Apollo-style program.  In their mind a large cost-plus development program is required to return to the moon or do anything worthwhile in manned spaceflight (even to get to ISS).

R&D is Research & Development together, so my R&D statement still applies, since any provider would need to develop the interfaces, fairings, and interstages to accomodate any new spacecraft outside the standard offering. As to their 'mind-set' of large cost-plus development, that's not entirely clear from their statements. It might be perceived by some as such, but utilizing existing rocket capabilities (as they have stated), rather than new R&D work on future 'game-changing' technologies (something they said wasn't required), sort of negates the whole premise behind cost-plus.

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As I indicated in the hearing thread, the '10 year' statement by Cernan was for BOTH safe & affordable. They'll be lucky to have a safe flight history in that time.

Still laughable.  From LV standpoint commerical already has a "safe" track record (EELV). 

From capsule standpoint, Boeing (and the companies it subsumed) has already made several successful manned capsules.  And in the past capsules haven't needed a 5-7 year clean flight history in order to be considered "safe".
[/quote]

From a pure rocket standpoint, absolutely. But for the combined finished product (launcher + capsule), safety & reliability it starts from day 1. If they make any significant changes to the rocket, like software, then it (design) starts to get muddied. And for a destination like ISS, with a political life (at this point) looking like 2020, that's T-(10 years-contract award date-development time). That could be only 3 years. Hardly an affordable business case at 2 flights/year = 6 flights. This also assumes a design where an Orion-style capsule is not handed to them pre-designed, but 'start-from-scratch', which seems only fair. It is 'commercial' after all ;)

Quote
The so-called 'experts' we have heard prior to this hearing have made some of the most non-sensical, flawed, and outright incorrect statements of them all. Bolden's "we don't have a HLV now" statement will be remembered for all eternity for me.

In an important way of speaking he is right.  From the standpoint of payload, we have no HLV right now. 
[/quote]

Umm, so what is shuttle?
« Last Edit: 05/29/2010 12:48 am by robertross »

Offline jongoff

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Re: Myth: CxP's only problem was that it was underfunded.
« Reply #44 on: 05/29/2010 12:53 am »
....we need to drop the cost of access to space both by-the-kilogram and by the cubic meter. Griffin chose to do this with mass fraction by building a massive launcher...

I actually agree almost 100% with this paragraph.

~Jon

I dont. Griffin never made a choice to reduce launch costs. ( he made a lot of other choices, like attempting to gear everything up for a direct-to mars launch etc, but no choice about launch costs )

Well, I said almost...

~Jon

Offline SpacexULA

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Re: Myth: CxP's only problem was that it was underfunded.
« Reply #45 on: 05/29/2010 12:55 am »
In an important way of speaking he is right.  From the standpoint of payload, we have no HLV right now. 
Umm, so what is shuttle?

A 2nd stage so heavy it turns a HLV into a MLV? :)
« Last Edit: 05/29/2010 12:59 am by SpacexULA »
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Offline robertross

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Re: Myth: CxP's only problem was that it was underfunded.
« Reply #46 on: 05/29/2010 01:03 am »
In an important way of speaking he is right.  From the standpoint of payload, we have no HLV right now. 
Umm, so what is shuttle?

A 2nd stage so heavy it turns a HLV into a MLV? :)

Yeah, I suppose you got me there  :)

Offline DaveJes1979

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Re: Myth: CxP's only problem was that it was underfunded.
« Reply #47 on: 05/29/2010 01:24 am »
R&D is Research & Development together, so my R&D statement still applies, since any provider would need to develop the interfaces, fairings, and interstages to accommodate any new spacecraft outside the standard offering.

Super, but how does that address or contradict the point I was making?  My original criticism of the astronaut statements had to do with the fact that they believe that human spaceflight requires large government-run cost-plus development programs.  This is not true.  Launch services or taxi to LEO and ISS can be contracted as fixed price services.

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As to their 'mind-set' of large cost-plus development, that's not entirely clear from their statements. It might be perceived by some as such, but utilizing existing rocket capabilities (as they have stated), rather than new R&D work on future 'game-changing' technologies (something they said wasn't required), sort of negates the whole premise behind cost-plus.

Except that Constellation, which they support, is indeed the same old cost-plus model that was followed previously.  Government-designed (top level design) and owned vehicles contracted out to contractors who are then micromanaged in eye-watering detail by government.

Quote
From a pure rocket standpoint, absolutely. But for the combined finished product (launcher + capsule), safety & reliability it starts from day 1. If they make any significant changes to the rocket, like software, then it (design) starts to get muddied.

That's why Boeing and ULA have systems engineers.  How does this make that approach unsafe in relation to NASA's approach, when they have to do the exact same thing?

Quote
And for a destination like ISS, with a political life (at this point) looking like 2020, that's T-(10 years-contract award date-development time). That could be only 3 years. Hardly an affordable business case at 2 flights/year = 6 flights.

There is a business case because they will charge NASA a fixed price high enough.  And it will still be far less than the legacy cost-plus model.  That is because private industry does not have the gargantuan overhead of NASA's fixed costs.

Quote
Umm, so what is shuttle?

The shuttle is precisely what I had in mind.  The shuttle payload is only 25 metric tonnes.  In the context of the recent hearings heavy lift means 80+ mt of payload, certainly not anything below 50 mt.

IOW, gross mass to LEO is not the same as payload to LEO.
« Last Edit: 05/29/2010 01:50 am by DaveJes1979 »

Offline FinalFrontier

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Re: Myth: CxP's only problem was that it was underfunded.
« Reply #48 on: 05/31/2010 01:37 pm »
[W]hat is there to show for the 9 billion spent so far[?] 
A few examples.
 
- Ed Kyle
Sorry Ed thats not good enough. We could have had a functioning SDHLV with Orion nearly finished. Instead we have "nothing".
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Offline FinalFrontier

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Re: Myth: CxP's only problem was that it was underfunded.
« Reply #49 on: 05/31/2010 01:48 pm »
This is depressing.
Why is it that its always got to be CXP or bust CXP or bust with congress and with some on this site?!?!?! Why is it that no one seems to ever mention (even if they are considering) what the middle ground is?


One extreme to the left is no better than its sister extreme to the right.

(i.e.Fy 2011 is not > <  but is = to CXP for equal and opposite reasons).
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Offline robertross

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Re: Myth: CxP's only problem was that it was underfunded.
« Reply #50 on: 05/31/2010 03:42 pm »

From a pure rocket standpoint, absolutely. But for the combined finished product (launcher + capsule), safety & reliability it starts from day 1. If they make any significant changes to the rocket, like software, then it (design) starts to get muddied.

That's why Boeing and ULA have systems engineers.  How does this make that approach unsafe in relation to NASA's approach, when they have to do the exact same thing?

Quote
And for a destination like ISS, with a political life (at this point) looking like 2020, that's T-(10 years-contract award date-development time). That could be only 3 years. Hardly an affordable business case at 2 flights/year = 6 flights.

There is a business case because they will charge NASA a fixed price high enough.  And it will still be far less than the legacy cost-plus model.  That is because private industry does not have the gargantuan overhead of NASA's fixed costs.

Two covered at once here:

Do you expect ULA (since I think many are on the same page that these are the better contenders) to offer a capability for a future BEO spacecraft for firm fixed price? I mean, that's what it comes down to. CxP's Orion was for a BEO capability that was re-arranged to support ISS in the near term. These astronauts are fighting for what they lived through: BEO manned spaceflight.

The alternative is to:

1. Cancel Orion right now with $XB in contract termination costs, and have the people working on the program let go (paying them as well)
2. Open the tender process for a firm fixed price LEO taxi.
3. Open the tender process for a firm fixed price ISS CRV (6-month lifeboat); or combine 2&3.
3. After a few years, open another tender process for a new vehicle which is BEO capable, or re-start Orion as block II. If this is to be a commercial service, I highly doubt you would find a provider, or if you did, then the price for a scarry business model would be astronomical.

(have to continue later)

Offline DaveJes1979

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Re: Myth: CxP's only problem was that it was underfunded.
« Reply #51 on: 06/01/2010 05:43 am »

Do you expect ULA (since I think many are on the same page that these are the better contenders) to offer a capability for a future BEO spacecraft for firm fixed price? I mean, that's what it comes down to. CxP's Orion was for a BEO capability that was re-arranged to support ISS in the near term. These astronauts are fighting for what they lived through: BEO manned spaceflight.

They said nothing of the kind and you are changing the subject.  They are against commercial for launch services and LEO taxi.  They are not simply opposing commercial for deep space.  The Obama FY2011 does not propose commercial for deep space capsule.  There is no reason to oppose commercial taxi to LEO in order to support a NASA-designed and owned deep space capsule.

Quote
3. After a few years, open another tender process for a new vehicle which is BEO capable, or re-start Orion as block II. If this is to be a commercial service, I highly doubt you would find a provider, or if you did, then the price for a scarry business model would be astronomical.

A BEO deep space capsule could debatably be done either as traditional cost-plus-NASA-designed or commercial fixed price, but again it is a separate subject from LEO taxi and launch services. 

If it was done as commercial fixed price, it would not be a "scary business model" because with fixed-price contracts the requirements are set in stone BEFORE a company commits to a project. 

Offline Jorge

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Re: Myth: CxP's only problem was that it was underfunded.
« Reply #52 on: 06/01/2010 01:35 pm »

3. After a few years, open another tender process for a new vehicle which is BEO capable, or re-start Orion as block II.

The latter option is not possible. See my other posts on the subject.
JRF

Offline khallow

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Re: Myth: CxP's only problem was that it was underfunded.
« Reply #53 on: 06/01/2010 02:00 pm »
This is depressing.
Why is it that its always got to be CXP or bust CXP or bust with congress and with some on this site?!?!?! Why is it that no one seems to ever mention (even if they are considering) what the middle ground is?

Because there isn't enough funding for a middle ground. Not every decision can be made via compromise.
Karl Hallowell

Offline jml

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Re: Myth: CxP's only problem was that it was underfunded.
« Reply #54 on: 06/01/2010 03:43 pm »
This is depressing.
Why is it that its always got to be CXP or bust CXP or bust with congress and with some on this site?!?!?! Why is it that no one seems to ever mention (even if they are considering) what the middle ground is?

Because there isn't enough funding for a middle ground. Not every decision can be made via compromise.

There may not be enough dollars to do everything at once. But there still can be a middle ground. Some decisions can be made with a compromise.
Link:
http://www.launchcomplexmodels.com/Direct/documents/nasa-compromise-budget.xls

Edit: (No, I'm not trying to imply that the "D" word is the one and only true way - just that there are other possible paths forward besides the two extremes of pure PoR vs pure FY 2011 or pure commercial vs pure NASA-run)
« Last Edit: 06/01/2010 04:06 pm by jml »

Offline neilh

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Re: Myth: CxP's only problem was that it was underfunded.
« Reply #55 on: 06/01/2010 08:46 pm »
Dennis Wingo just released a piece which has some good discussion of CxP and its various problems:

http://www.spaceref.com/news/viewnews.html?id=1398
Quote
There have been two major congressional hearings recently that brought together two of our most respected moonwalkers, Neil Armstrong and Gene Cernan. There are two arguments that they make. The first is that if Constellation was adequately funded, that it would be moving merrily on to success. The second is that the lack of a destination and clear timeline in the Obama policy abdicates American leadership in space.

This following is from Gene Cernan's testimony relative to the funding issue:
"Important to note is that the Committee was directed to base their conclusions and recommendations not on the FY2009 budget, but rather on the FY2010 budget from which tens of billions of dollars had already been removed between 2010 and 2020."

However, NASA's funding problems started long before the FY2009 budget. This can be seen in NASA's own earlier documents and a 2007 study by the Government Accountability Office (GAO) on the Ares 1 program. The original Ares 1/Orion design was based upon a standard four-segment Shuttle solid rocket motor, an SSME (Space Shuttle Main Engine) with modifications for air start, and a 5.5 meter Orion capsule capable of carrying up to 6 people to ISS and 4 people to the EOR-LOR rendezvous point in Low Earth Orbit (LEO) (page 404 from the ESAS Final report TM-2005-214062).

The IOC (Initial Operational Capability) date was supposed to be 2011 for the Orion/Ares 1 combination (chart on page 56 of the ESAS doc [show in figure 1 here] plus Scott Horowitz's and Doug Cook's Exploration Strategy Workshop charts as late as April 28, 2006). Looking at the program in 2007, the GAO (GAO-08-51) found something completely different.

Here is the chart from the NASA Exploration Systems Architecture Study (ESAS) report: ...

By 2007, long before the Obama Administration, this all had changed. When President Bush announced the Vision for Space Exploration in 2004 it was stated that in order to minimize costs and workforce disruptions that the new launch vehicles be based as much as possible on the existing Space Transportation System (Shuttle stack) design. However, NASA changed the original ESAS Ares 1 design from the standard four segment booster and an modified Space Shuttle Main Engine (SSME), to a five segment booster and the J2X engine. This is what the GAO found (from page 2): ....

NASA knew in September 2007 that they would have insufficient budget for their planned work on Constellation in FY 2008-2010. Compounding this situation several changes were made to the Ares 1 vehicle that increased near term costs without any commensurate increase in funding by Congress. These changes, going from the four segment to the five segment booster, and changing from the SSME to the J2-X, required an additional $730 million over their existing 2007 budget, which did not happen (page 7). These changes also led to many unintended cost increases and schedule slips above that identified by NASA that were not anticipated or funded with the prime example being the Thrust Oscillation problem. ...

(The piece also has some rather interesting quotes from GAO reports on CxP)

I attached the chart from the ESAS study, which is kind of darkly comical in retrospect.
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Offline nooneofconsequence

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Re: Myth: CxP's only problem was that it was underfunded.
« Reply #56 on: 06/01/2010 08:58 pm »
This is depressing.
Why is it that its always got to be CXP or bust CXP or bust with congress and with some on this site?!?!?! Why is it that no one seems to ever mention (even if they are considering) what the middle ground is?

Because there isn't enough funding for a middle ground. Not every decision can be made via compromise.

Its in the nature of what a compromise suggests.

To have a compromise FY2011, the items have to look like a part of FY2011 - example: Orion CRV.

Some parts can't be made to fit in this format - so rather than say do DIRECT and abandon Ares I, the other side waits for capitulation and a totally new budget, bigger and shiner than before.

So this drives for a CR. But a CR doesn't help either side.

In the end we'll either get a CR or a slightly modified FY2011.

And the myth will continue...
"Wise men talk because they have something to say; fools, because they have to say something" - Plato

Offline robertross

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Re: Myth: CxP's only problem was that it was underfunded.
« Reply #57 on: 06/01/2010 11:24 pm »

Do you expect ULA (since I think many are on the same page that these are the better contenders) to offer a capability for a future BEO spacecraft for firm fixed price? I mean, that's what it comes down to. CxP's Orion was for a BEO capability that was re-arranged to support ISS in the near term. These astronauts are fighting for what they lived through: BEO manned spaceflight.

They said nothing of the kind and you are changing the subject.  They are against commercial for launch services and LEO taxi.  They are not simply opposing commercial for deep space.  The Obama FY2011 does not propose commercial for deep space capsule.  There is no reason to oppose commercial taxi to LEO in order to support a NASA-designed and owned deep space capsule.
I was simply adding context to this debate.
And they certainly did mention this:

"Armstrong: first, very much in favor of commercial activity and hope they have the progress they hope for. nevertheless, they face a very difficult business case. market is extremely thin, investor contribution must be substantially larger than government contribution by their business plan, business plan looks highly suspect. recalls reading article by Brewster Shaw, former astronaut and now Boeing executive, about difficulty in convincing his boss that there's a business case, but Shaw is hopeful. difficult for any commercial space provider to make the case to their investors without the developed market. hopes that market develops, but very difficult to see that it will."
Quote
Quote
3. After a few years, open another tender process for a new vehicle which is BEO capable, or re-start Orion as block II. If this is to be a commercial service, I highly doubt you would find a provider, or if you did, then the price for a scarry business model would be astronomical.

A BEO deep space capsule could debatably be done either as traditional cost-plus-NASA-designed or commercial fixed price, but again it is a separate subject from LEO taxi and launch services. 

If it was done as commercial fixed price, it would not be a "scary business model" because with fixed-price contracts the requirements are set in stone BEFORE a company commits to a project. 

Yes, the requirements are set in stone ahead of time, but the problem is also: how much will NASA end up paying in the end for 2 flights/year from early 2015 (start date) to end 2020 (ISS splashdown date). That's somewhere between 10-12 total crewed flights. The business model AFTER that falls apart. Sure, the contract would be written that they get paid if ISS taxi is not required for any reason. But what's after that? If we have no destination, ULA (or any other company) has just put a development effort into an uncertain future. They 'may' get a company like Bigelow to buy flights, but at this point in time there is scary business model. Though but a small portion of the business, shareholders still may have doubts. I would (if I were one).
« Last Edit: 06/01/2010 11:27 pm by robertross »

Offline kkattula

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Re: Myth: CxP's only problem was that it was underfunded.
« Reply #58 on: 06/02/2010 02:16 am »
IMO, CxP's biggest problem was not underfunding, but that it needed massive funding to succeed.

Building TWO new rockets and then trying to claim savings due to commonality? As some on this forum like to point out, rockets parts are not Lego blocks. An SRB used as a first stage has vastly different integration and handling requirements than when used as a side-mounted booster. Not that there is much commonalitly left anyway. J-2X?

NASA should have built only ONE new rocket. First stage only for crew and/or cargo to LEO. Add upper stage / EDS for BEO.

It seems to me that MSFC's reaction to any new spacecraft development, is to plan to use the entire budget on design and development. Actually building and operating it will require additional funding. Or, preferably, cancellation and a new project to design and develop.

Offline jimgagnon

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Re: Myth: CxP's only problem was that it was underfunded.
« Reply #59 on: 06/02/2010 02:58 am »
Yes, the requirements are set in stone ahead of time, but the problem is also: how much will NASA end up paying in the end for 2 flights/year from early 2015 (start date) to end 2020 (ISS splashdown date). That's somewhere between 10-12 total crewed flights. The business model AFTER that falls apart. Sure, the contract would be written that they get paid if ISS taxi is not required for any reason. But what's after that? If we have no destination, ULA (or any other company) has just put a development effort into an uncertain future. They 'may' get a company like Bigelow to buy flights, but at this point in time there is scary business model. Though but a small portion of the business, shareholders still may have doubts. I would (if I were one).

Forget 2020 as ISS splash date. The ISS will be up there even if we're duct taping parts on and it's leaking air more than Mir, then we'll take it apart, save the good bits, and upgrade the rest. Expect a need to send people there for a long time.

You're also stating NASA minimum requirements as of today; additional programs may require more personnel in space. Also Bigelow will have launch requirements starting around 2014-2015. All this doesn't take into account any other Hubble or other satellite servicing.

Yeah, starting a Space business is scary, but so is starting any other kind of business. Say commercial space misses its goals and is only able to equal Soyuz in efficiency: that's $50M/seat. With the $3B we spend on Shuttle, that 60 people in space a year, or 40 people with $1B infrastructure every single year.

Those are numbers Constellation could never touch. Old NASA way vs. new -- when you look at what's possible, it's a wonder we clung to the old ways so long.

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