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RSS feed with expanded content.| From | Mark Reiff <markreiff@xxxxxxxxxxxxx> |
| Date | Thu, 11 Aug 2005 01:19:47 -0500 |
FYI, "Dribs & Drabs II" Selenian Boondocks Blog http://selenianboondocks.blogspot.com : So I'm reading through the leaked reports on the new architectures : that Keith Cowing has posted over at NASAWatch.com's subsidiary : SpaceRef. In a sense reading it is almost like a slow motion train : wreck - you know the doom that is coming but nothing can be done to : avoid it. : I think the thing that puzzled me the most was the imbalance in : cited figures between the two systems studied. While there were a : lot of heming and hawing about concerns with EELVs, there seemed to : be a complete turnaround with the SDHLV. Here's how much it'll : cost, how long it will take to deliver, 100% confidence in results, : etc. : The EELVs are initially cited as favorably reviewed, especially the : super-sizing: "Planners found in their trade analyses that scaled : up variants of both families could lift in excess of 40 metric : tons, to as much as 80 metric tons. The latter figure was believed : to be the smallest payload envelope a heavy lift design would need : to carry in order to participate in a lunar mission." : I'm not sure why 80 mt is the minimal lift requirement. This seems : to preclude anything like on-orbit operations such as assembly or : post-launch systems verifications. : Reading through Mr. Cowing's analysis, it becomes clear that NASA : really doesn't want to invest in human-rating (whatever that means) : the EELV class of D-IV & A-V, and they don't want to think about : facilities upgrades required by their 40 mt (CEV) and 80 mt (Lunar) : minimas. : So either way we're looking at the investment of between ~$6Bn and : $8Bn, and you and I both know that rounds to ~$10Bn (and includes : modifications to the launch facilities!). Some of the more obvious : hidden expenses are the crawler upgrades that are going to be : required and the re-configuring of the launch pads. Some of the : more subtle costs are things like the over-engineering of payloads : that has to be done on the ground to ensure 100% operability post- : launch, since we're not doing any kind of on-orbit assembly or : inspection (that sort of thing is tough to build into a parametric : model, so tends not to be considered). : The difference to me seems to be that the main architectural : differences lie in the differences between the "build-a-little, : test-a-little, grow-our-architecture" philosophy and the "all or : nothing, shoot for the Moon" philosophy where everything works just : perfectly the first time and every time because we've figured out : every little thing that could conceivably go wrong and addressed it : beforehand. : I'm not privy to the inside workings of NASA, but from what Mr. : Cowing has shown us it appears to me that the decision was taken : early to go with the SDHLV, and that's where the bulk of the effort : went in this study, in an engineering orgy of strap-ons and : 109% thrust. I find it inconceivable that NASA's EELV concerns of : human-rating and super-sizing and launch-pads are sufficient to : cost the taxpayers between $6 and $8 billion. : I'm becoming resigned to the fact that America will be saddled with : this behemoth for the next 20 years. The engineers all seem to be : going bananas over it (which for me is always a huge red flag). : All the while the rest of the world will work to wrest the : remainder of the 20 mt payload market from American launch : providers, who will become resigned to essentially break-even on : the few launches that have to be done domestically because of : technology export limitations. : Using ISS as a starting point, Europe and Russia could easily move : to dominate cislunar trade while we're busy leapfrogging to the : Moon. Using Bigelow balloons, ATVs, and Klipers & Soyuzes they move : to EML-1 and start working on larger broadcast arrays in GEO, while : cleaning up the garbage for salvage and learning from the garbage : how to build better assets in GEO. : We'll construct a disposable Moon base to do some touch-n-go : practice for Mars, try to pawn it off on industry, and if the : funding continues we'll be on Mars by 2025 and the "objective" of : the VSE will have been achieved. : Except it won't have been, and we'll just have a Kennedyesque : "Flags & Footprints" moment on Mars to savor over the years while : we buy European anhydrous optic digital binoculars, Japanese : vacugel coats, and Russian honeymoon flights to our Moon. -- Mark Reiff <markreiff@xxxxxxxxxxxxx> -- Space Future | To unsubscribe send email with the subject "unsubscribe" www.spacefuture.com | to "sf-discuss-request@xxxxxxxxxxxxxxx".