During the joint Senate-NASA presentation in September 2011, it was stated that the SLS program has a projected development cost of $18 billion through 2017, with $10 billion for the SLS rocket, $6 billion for the Orion Multi-Purpose Crew Vehicle and $2 billion for upgrades to the launch pad and other facilities at Kennedy Space Center.[55] These costs and schedule are considered optimistic in an independent 2011 cost assessment report by Booz Allen Hamilton for NASA.[56] An unofficial 2011 NASA document estimated the cost of the program through 2025 to total at least $41bn for four 70 t launches (1 unmanned in 2017, 3 manned starting in 2021),[57] with the 130 t version ready no earlier than 2030.[58] HEFT estimated unit costs for Block 0 at $1.6bn and Block 1 at $1.86bn in 2010.[59] However since these estimates were made the Block 0 was dropped in late 2011 and is no longer being designed,[25] and NASA announced in 2013 that the European Space Agency will build the Orion Service Module.[60]
The SLS rocket will not survive the multi-year Congressional funding battle, for a variety of reasons including the impending squeeze on the US government discretionary budget. It will make some early development flights, but the thing as now envisioned will never become an operational flight system in regular service.I see a lot of opinions expressed here on this forum. Thought I'd add my opinion for the record.
When doing comparisons, it's easy to concentrate on the things that are comparable, like mass-to-orbit, or which year it will fly at.But the bigger differences fall by the wayside.1. SpaceX's SHLV is reusable. That right there is much more important than the mass of the payload.2. SpaceX's SHLV is designed to meet cost and operational goals. SLS is politically designed, with most propulsion choices dictated by congress. (It's not that congress didn't learn from STS, it's that congress considers STS to have been a great success - by their metrics.) 3. And then there's this: (From wiki)QuoteDuring the joint Senate-NASA presentation in September 2011, it was stated that the SLS program has a projected development cost of $18 billion through 2017, with $10 billion for the SLS rocket, $6 billion for the Orion Multi-Purpose Crew Vehicle and $2 billion for upgrades to the launch pad and other facilities at Kennedy Space Center.[55] These costs and schedule are considered optimistic in an independent 2011 cost assessment report by Booz Allen Hamilton for NASA.[56] An unofficial 2011 NASA document estimated the cost of the program through 2025 to total at least $41bn for four 70 t launches (1 unmanned in 2017, 3 manned starting in 2021),[57] with the 130 t version ready no earlier than 2030.[58] HEFT estimated unit costs for Block 0 at $1.6bn and Block 1 at $1.86bn in 2010.[59] However since these estimates were made the Block 0 was dropped in late 2011 and is no longer being designed,[25] and NASA announced in 2013 that the European Space Agency will build the Orion Service Module.[60]I don't suppose anyone is suggesting SpaceX will spend $10B or anywhere near this on their SHLV, right?
Does the "lack of payloads" problem apply equally to SLS and BFR? Or is there something intrinsic in "MCT as the sole payload" that makes it fundamentally better than "MPCV as the sole payload?"
"If the FH at 53mt can be so inexpensively manufactured and operated, why is the SLS, with only 17 more mt so much more expensive to manufacture and operate, to the point that once your finished you don't have enough money to fly it and even if you could, no money to build the payloads it was intended to launch towards Mars?"
Musk has the Tesla motors card to play for cash. So if the next generation Tesla car rolls out successfully (not quite a sure thing) than he will be able to fund the BFR development from around 2017 with about $1B annually with other revenue steams from Solar City, batteries sales and SpaceX launches.
Quote from: rcoppola on 08/30/2014 06:43 pm"If the FH at 53mt can be so inexpensively manufactured and operated, why is the SLS, with only 17 more mt so much more expensive to manufacture and operate, to the point that once your finished you don't have enough money to fly it and even if you could, no money to build the payloads it was intended to launch towards Mars?" FH's price is uncertain and Block 1B TLI performance will dwarf that of FH.Still, I agree that FH is probably the biggest 'competitor' to SLS, much more so than a hypothetical BFR which would likely end up as expensive as SLS given a similar low launch rate.
Quote from: rcoppola on 08/30/2014 06:43 pm"If the FH at 53mt can be so inexpensively manufactured and operated, why is the SLS, with only 17 more mt so much more expensive to manufacture and operate, to the point that once your finished you don't have enough money to fly it and even if you could, no money to build the payloads it was intended to launch towards Mars?" FH's price is uncertain...
...and Block 1B TLI performance will dwarf that of FH.
Still, I agree that FH is probably the biggest 'competitor' to SLS, much more so than a hypothetical BFR which would likely end up as expensive as SLS given a similar low launch rate.
If the problem with the SLS was that there was no money to do missions with it...
..why do people think a SpaceX BFR wold be..any different?
They don't even have a non-NASA customer booked for their DragonV2 and it's supposedly 2 years away from flying.
Also, the money to develop the rocket, its spacecraft, and manufacturing facilities is not going to come out of the aether and will be more than a billion - an amount of money that they couldn't have possibly made in profit yet (not revenue)
What I'm getting a lot of on the internet is that, the rules that apply to every other company and government entity just don't apply to SpaceX because unicorns!
It probably will be some time before SpaceX can get on par with SLS, since Falcon Heavy hasn't flown just yet. However, especially if the worst fears about SLS manifest, Falcon Heavy could prove to be more cost effective that SLS at the least.