▲ | jjk166 5 days ago | |||||||
> Either they can never get the heat shield to be reliable, or they can't get cost down below Falcon 9 (meaning, refurbishment costs are too high). There are a lot of other potential technological problems (dozens of engines, stainless steel construction, the belly flop maneuver, etc). Ultimately if Starship would were to fail for technical reasons, it would only indicate the particulars of Starship's implementation don't work. Starship is not the only (or even in my opinion the best) way to achieve full reusability. And partial reusability, which just a few years ago was considered radical, has already been so firmly proven that just about everyone is doing, or trying to do it. The idea of "don't destroy this extremely expensive vehicle after only a single use" won't die for as long as people can see expenses on their books. If anything, the alternative approach, making a low cost, mass producible rocket has been abandoned, possibly pre-maturely. | ||||||||
▲ | GMoromisato 5 days ago | parent [-] | |||||||
Rocket Lab tried the alternative: low-cost, mass-produced expendable rockets, and Peter Beck famously ate his hat when they pivoted to reusable. Partial reusability won't get the cost down to the ~$100/kg range. And it definitely won't do that and still loft ~100 tons to orbit. Falcon 9 can get 15 tons to LEO for $45 million, and that's already the lowest price on the market. To hit $300/kg they would need to build a 2nd-stage, launch, recover (on a drone-ship) and refurbish for $4.5 million. That's just not going to happen. There are only two companies that are actively building hardware for 2nd-stage reusability: Blue Origin (which doesn't even have a prototype yet) and Stoke (which has a max 3-ton payload). If Starship fails, we are not getting $300/kg orbital costs for 1-2 decades minimum. I agree that Starship has lots of other potential technological blockers (although fewer each attempt--I never thought tower-catch would work the first time). But no other designs are even close to fulfilling the promise of low-cost orbital launch. | ||||||||
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