"There's a pretty general consensus that one of the greatest barriers to the exploration and development of space is the cost of launch to low earth orbit"
http://www.fourmilab.ch/documents/rocketaday.html
I would say roughly with economy of scale of hundred or two launches per year you could get a launch price of $500 per lb for Low Earth orbit and $1000 per lb for High Earth Orbit and/or Escape. Current prices are about $3-4000 per lb for LEO and $8000 for High Earth Orbit/Escape.
I would say that if you had on order of scale hundreds of launches per year for a decade or more you could get to around $100 per lb to LEO, but that's about as cheap as it gets using chemical rockets and throwing away the hardware each launch.
But we aren't really looking at a mature market when we look at market of hundreds of launches per year, compared to say the airline business. Suborbital trips are about a 1/4 to 1/2 of what it takes to get to orbit. I believe the ticket price for a suborbit trip is going to be about $100,000 per passenger- roughly $500 per lb with idea that evenually this could get around the $5,000 per passenger in a maturer market [1/20th of current price so it's $25 per lb for suborbital]. This "route" could lead to $50 per lb to LEO. But all this is a bit like predicting the cost of car travel at the beginning of 20th Century.
Space/Science » in reply to If you had economy of scale, what would be cheapest conventional rocket to get a lot of a mass to orbit?
re: If you had economy of scale, what would be cheapest conventional rocket to get a lot of a mass to orbit?
The whole thread (21 posts)
- If you had economy of scale, what would be cheapest conventional rocket to get a lot of a mass to orbit?
- Your framework of assumptions is completely unrealistic
- Musk's "Falcon" launchers are turbopump fed.
- I am an engineer just trying to understand design space tradeoffs
- Why the snark? If you don't want to play then don't play. (n/t)
- re: If you had economy of scale, what would be cheapest conventional rocket to get a lot of a mass to orbit?
- SeaDragon is one end of the curve
- Your framework of assumptions is completely unrealistic
