A recent newspaper column by Michael Griffin and Daniel
Dumbacher claims the new SLS launch vehicle is essential to the nation’s space
program. The column also claims that SLS
costs are expected to be about the same as current commercial launchers. Griffin is a former NASA administrator, and Dumbacher is a former deputy associate
administrator.
NASA has its critics,
and it has a demonstrated history of badly underestimating costs, which is primarily why it has critics. I am not interested in criticizing
anyone. Personally, I am just interested in the best facts and
estimates that I can uncover. The SLS
will certainly have its critical uses. I
am less confident than Griffin and Dumbacher in its cost-effectiveness.
Back in 2012, I
searched out payload data and launch cost estimates for several launch
vehicles, some domestic, and some foreign. There was some conflicting information, which I resolved as best I could. Where possible I used data direct from the
manufacturers. Some of the vehicles I
researched are no longer flying, some
have not flown yet, but most are flying today.
To this database I have added this year the historical data
for the NASA space shuttle (now retired),
and the best available projections from NASA (and from NASA’s critics) for
its new SLS vehicle, currently under
development. There is considerable
disagreement and uncertainty about the projected launch prices for SLS in its 3
projected versions. Much depends upon
the actual flight rate, which was
presumed to be once a year for the data I used.
See figure 1 for my database.
This kind of data comes from sources across a multitude of years, which requires correction for inflation to a
common comparison year. My original
database is corrected to 2012 dollars,
and I did not change that. The
SLS estimates have not really changed by any amount I could find from 2012 to
present. Inflation rates have been quite
low for many years. I used 2% as a
representative figure. See figure 2 for
my inflation-adjusted launch prices.
Figure 2 – How Launch Costs Were Adjusted for Inflation to 2012 Dollars
What I generated with this data was a plot of unit prices to
low earth orbit (LEO) as a function of payload mass sent to LEO. You calculate this as launch price divided by
the max payload capability (in this case to LEO). Then you plot that unit price versus max
payload. It is generally expected that
there should be a gently-decreasing trend of unit price as payload size
increases, especially for vehicles that
compete commercially in the satellite launch business. This is the “price break for larger sizes”
effect, in rockets.
This unit price (expressed here as millions of 2012 dollars
per metric ton of payload) represents a minimum unit cost to send payload LEO, obtained only because the rocket flies “full”. You must remember that the rocket costs the
same to launch whether it flies “full” or not.
If the rockets fly “half full”,
then the achieved unit prices are twice those reported here. 10% full is 10 times the price, etc.
The units of measure here are 2012 dollars (in millions) and
payloads measured in metric tons. A
metric ton is 2205 pounds per ton instead of the US customary 2000 pounds per
ton, so a metric ton is about 10% larger
than a US ton. But that’s still pretty
close.
I used two estimates for NASA’s SLS system: their target is $500 million per launch at
about one flight per year, while their
critics contend that figure is likely closer to $1000 million ($1 billion) per
launch, at that same flight rate. Thus I show a lower-bound curve (NASA) and an
upper-bound curve (their critics) for SLS.
See figure 3. I used the same
launch price for all three versions of SLS,
because the data are still too uncertain to resolve the price
differences among the three configurations.
The expected trends of gentle price break with larger
rockets is definitely there, as
illustrated by the commercial rockets.
That would be the Spacex Falcon family,
the ULA Atlas-V group,
Ariane, Proton, and ULA’s Delta-IV. For the 20-ton class of payloads, prices range from about 5 to about 8 million
dollars per ton to LEO.
Extrapolating, we would expect
lower numbers at 50 and 100 tons, based
on these trends, perhaps in the 1-3
million dollars per ton range.
The Titan-IV data are considerably higher at around $23M/ton
for a 20-ton-class payload, but that is
because Titan-IV was never used for commercial competitive satellite
launch. The others discussed so far
were; it’s not about the rocket as much
as it is the logistics that support it.
That is how prices were reduced by a factor of 3 or 4, for the same basic technology and the same
payload class. Titan-IV no longer
flies, it is obsolete and fairly-recently
retired.
The data point for the space shuttle represents an
entirely-different technology: the semi-reusable
boosted space plane, not a throwaway
rocket booster. Its deliverable payload
in the cargo bay was 20 tons to LEO, but
what was sent to orbit was that plus a recoverable space plane, totaling 100 tons. For my curves, I based the unit price on deliverable
payload. If instead you base that on the
entire orbiting vehicle, that unit price
drops from $75M/ton to about $15M/ton,
very comparable to the non-commercial Titan-IV.
However, that’s still
about factor 2-3 higher than what is currently available commercially in the
same payload tonnage class. In that
sense, the two government-only vehicles
(shuttle and Titan-IV) illustrate quite clearly the effects of commercial competition
upon simplifying logistics to lower the price per launch. Commercial is about factor-3 cheaper for the
same thrown payload than government.
That government-vs-commercial effect shows up in the
projected unit prices with NASA’s new SLS,
even if you accept their launch price estimates. Over the 70 to 130 ton payload range, that unit price ranges from about $7M/ton
down to about $4M/ton.
So far there are no commercial vehicles in that payload
class, but based on the commercial unit
price trend, one might reasonably expect
such vehicles to price out closer to $1-3M/ton.
The SLS might actually turn out to be closer to $8-14M/ton (my
upper-bound curve), if NASA’s critics
are closer to right. In any event, it is unlikely to fly before 2018 at the
earliest, based on what I read. And it is very unlikely to be as cheap as
any commercial rockets that may come to exist in that size class.
Given those data that demonstrate a clear commercial cost
advantage, I would suggest for the near
term using SLS only for those missions absolutely requiring 70-130 ton
payloads. Anything and everything else
ought to “fly commercial” for around factor 3 savings. And soon,
we won’t be restricted to 20-ton-class payloads on those commercial
rockets. Falcon-Heavy is supposed to fly
its first time this year, or next
year, providing a 53 ton
capability.
I don’t know about the other companies, but Spacex is reportedly considering an
upgrade to its not-yet-flying Falcon-Heavy that could up its payload capability
closer to the low end of the range covered by the SLS configurations (about 70
tons).
Spacex is also reportedly considering an entirely-new
vehicle called “MCT” that equals or exceeds the payload capability of all the
SLS configurations. It will be very
interesting to see how that one prices out,
as it will be designed by people with real competitive experience, and with commercial competition in mind from
the outset, just like its earlier
siblings.
Meanwhile, the
political “long knives” have come out in Congress over the recent failures of a
Spacex Falcon-9 and an Orbital Sciences Antares. They seek to kill the new initiatives aimed
at commercial crewed launch and commercial unmanned space station
resupply.
When you think about it,
all the rocket makers have had their histories of failures to
overcome, so it is clear the “long
knives” are politically motivated to protect the older companies from the
competition of the newer companies.
Commercial is demonstrably cheaper than
government-supplied, and likely will
always be cheaper. It would be very unwise to listen
to the “long knives”, or to let them win.
Update 12-25-15:
Spacex has just returned its Falcon-9 to flight with a successful satellite launch. Plus, for the first time, they successfully landed and recovered its first stage booster, all in the same mission.
Meanwhile, Blue Origin also landed and recovered one of its suborbital boosters.
And, Orbital Sciences has returned its Cygnus cargo carrier to flight status after switching to Atlas-5 instead of its in-house Antares as the booster.
There is no longer any excuse for the "long knives" to be out in Congress, seeking to destroy the new commercial space initiatives.
Update 12-25-15:
Spacex has just returned its Falcon-9 to flight with a successful satellite launch. Plus, for the first time, they successfully landed and recovered its first stage booster, all in the same mission.
Meanwhile, Blue Origin also landed and recovered one of its suborbital boosters.
And, Orbital Sciences has returned its Cygnus cargo carrier to flight status after switching to Atlas-5 instead of its in-house Antares as the booster.
There is no longer any excuse for the "long knives" to be out in Congress, seeking to destroy the new commercial space initiatives.
The SLS will provide two things that no other launch vehicles will be capable of.
ReplyDeleteWhen fully operational, it should be able to deploy at least 95 tonnes to LEO with an upper stage (essential for beyond LEO missions). No other vehicle, not even the Falcon Heavy, will come close to this.
Secondly, the SLS will be able to accommodate large payloads within a fairing diameter that could range from 8.4 meters to 10 meters in diameter. No private launch vehicle will have a payload fairing larger than 6 meters in diameter.
So the SLS will be the only vehicle capable of deploying Bigelow's largest payload concept, the BA-2100. Bigelow Aerospace has already asked NASA about launching its largest space habitat concept.
The SLS will also be the only vehicle capable of deploying uber-lite 8.4 meter in diameter Deep Space Habitats directly derived from repurposed SLS propellant tanks that could have internal volumes exceeding that of the ISS (the Skylab II concept).
A large payload fairing may also be essential for deploying large ADEPT decelerators for deploying crewed vehicles and large cargoes (20 tonnes plus) to the Martian surface.
The annual cost of being able to launch Space Shuttle has been estimated at nearly $1.875 billion a year (in 1994 dollars)-- without launching a single Shuttle flight. The additional cost per Shuttle launch has been estimated at approximately $125 million (19994). In today's dollars that would be approximately $3 billion with $200 million added for each launch.
So one Shuttle launch per year, in today's dollars, would have cost NASA $3.2 billion. Five launches would have cost them $4 billion, $800 million per launch.
NASA estimated that the Sidemount Shuttle cost for five launches would be about $500 million (much lower than the Space Shuttle) and estimated that an SLS type of vehicle would cost about 10% more than the Sidemount Shuttle ($550 million) per launch.
Even though these launch cost don't include the cost of payloads, spending less than $3 or $ 4 billion a year for five heavy lift launches doesn't seem to be excessively costly within NASA's ~$8 billion a year human spaceflight related budget-- to do things that no other vehicles can!
Marcel
Hi Marcel:
DeleteYou're right for the near term about SLS being the only game in town for big stuff. Longer term (a few to several years from now), I think Musk's MCT might do an even better job a lot cheaper.
I also think that we won't need as many 8 to 10 m diameter payloads as a lot of folks contend. Not if we get off dead center and start doing real assembly and construction work in LEO.
Which requires a supple spacesuit, among other things. And MCP is the way to achieve it.
-- GW
Appreciate your comment Gary!
ReplyDeleteI wasn't attempting to imply that the SLS was the only game in town. I just said that the SLS will be able to do some things that smaller rocket vehicles with much smaller fairing sizes simply could not do.
8.4 meter in diameter habitat modules makes it a lot easier to internally mass shield inhabited sections with water for interplanetary journeys. This would be much more mass efficient than attempting to externally shield an entire habitat module.
And for long multi-month interplanetary journeys, I think 8.4 meter in diameter habitat modules should make it much more physically and psychologically comfortable for astronauts.
Similar 8.4 meter in diameter habitats deployed to the surface of the Moon and Mars could be externally mass shielded with regolith, allowing astronauts to live in habitats as spacious as multilevel homes on Earth.
Marcel