Stas Bush wrote:I am sorry, but they are encountering problems because they are trying to do something other space agencies, which had neither smaller funding nor a smaller incentive to try it, simply decided against as the payload loss is immense and the value of reusable engines when jettisoned in a rocket fashion goes down severely due to many reasons. In fact, NASA and other space agencies told that to SpaceX at the front. And keep telling them that. They did not have a viable plan and they do not have a plan for the second stage at all.
Yeah, that's why they are doing soft landings with the Falcon 9Rs out in the Atlantic.
Stas Bush wrote:Tell that to Musk who wants to make an ordinary rocket fully reusable and is almost a religious believer in the goal (which may be good, or may be just a lot of wasted resources). Reusable rockets are a problem; people told him that. Reliability suffers. Reusability will suffer as well, as you can never be truly certain the damn thing is safe. The difference between a spaceplane and a reusable rocket is that a spaceplane is a plane; planes fly a lot and thus are acceptable testbeds. Rockets do wear out very quickly and prototypes destroy themselves.
Your idea that a space plane is just a plane that goes faster and faster only counts if you are going to spend the effort to build it that way - and that costs a LOT of money. We don't even know how much that would cost, but you seem wedded to the idea of Horizontal Take-off/Horizontal Landing (HTHL), and I doubt I can convince you otherwise. I wonder why no one else is trying it seriously? Could it be the structural problems are just too nasty?
Stas Bush wrote:So? A Skylon can be operated from anywhere. A Falcon Heavy Reusable does not exist, just like Skylon, and perhaps very much like the latter... most likely never will; full reusability of a heavy rocket runs into yet more challenges than just 'making the stage survive descent' where at the second stage you have to either slash the payload, like, twice or lose the stage. That is pretty much it. People had the opportunity to work on such solutions, in the European agencies for example, and decided against it.
Way to miss my point.
The current payload cost (per SpaceX documents) for a Falcon Heavy launch (which they are booking for) is $2200 per kilogram. The target cost for your beloved Skylon (which doesn't even have the full prototype engines running yet - although I don't see any show stoppers) is 1430£ per kilogram, or about $2300. That is for an expendable Falcon Heavy, not a reusable one.
Also, you seemed to miss my earlier comment about making a second stage reusable:
TimothyC wrote:Second Stage recovery is more plausible with a TSTO spaceplane than with a conventional rocket.
Also, for the record, there was a reusablitlity study in the 1960s that showed that if you can recover a liquid stage with the engine and most of the tankage intact, you can have a refurbishment at less than 10% of the cost of a new rocket. At that point you can deal with a payload that is half the size and still come out ahead of your initial rocket.
Face it Stas,
any technology that allows for reusable SSTO operations allows for reusable TSTO operations at a lower price point*. It's reusability, not SSTO that saves money in the long term.
*Pending Polywell working out. Then we can have SSTS
"I believe in the future. It is wonderful because it stands on what has been achieved." - Sergei Korolev