From: ShldWulf@a...
Date: Sat, 26 Apr 2003 01:30:32 EDT
Subject: Re: (OT) Rutan spaceplane
> ias@sprintmail.com (Imre A. Szabo) wrote: Space Ship 1 is specificlly designed for experimental purposes and is not a commercial model nor will it be used as such. According to the website and an article in AWST. On the other hand, Burt IS planning on using the White Knight to loft small payloads into orbit. They will be Pegasus class micro-sattilites, not manned. They hybrid rocket motor is a poor choice for any type of orbital try, and would/will have to be replaced, along with Space Ship 1, (probably so called because he has plans for Space Ship 2 running around already:o) for any orbital attempt. > Sanger had the right idea decades ago. A two stage fully reusable Actually Sanger's idea was a captive sled booster, so technically it was a stage and a half:o) > KH.Ranitzsch@t-online.de wrote: It's an X-prize official entery so it, (according to the rules of the contest) can't be in any way shape or form funded by the government. (Burt does follow SOME rules:o) > What is the cost of Rutan's program ? He won't say and it will in all likely hood be quite a bit more than the prize of $10million dollars. > Accounting can be quite a creative art, so everything about this must This is the main reason why they are silent on the cost. It is NOT a commercial, but a test vehicle. Maintenance, recurring, and other costs will be closely tracked once the system starts testing to give a ballpark figure for how much a commercial operator would need to charge to make a profit. There is already a good amount of data on the White Knight, but till it flys repeatedly, the operations cost of Space Ship 1 are all asumed. On the converse side, it's been known for decades that what REALLY costs for current flights is: a. The requirement for high redundancy and reliability for launchers because they are essentially "one-shot-must-work-the-first-time" vehicles. b. The massive amounts of support and engineering staff required at launch to support the above vehicle. WK/SS1 does away with a majority of (b), but so did the Pegasus and Sea-Launch. They were still stuck with (a). > This is generally not known until the program is complete, but > ias@sprintmail.com (Imre A. Szabo) wrote: > That's only because Soyuz are done in Russia. If the Russian's had to In actuallity flying in a Russian rocket or the Shuttle, a passenger would have had to pay around the same price. The Russians agreed to do it for money where as NASA won't take the liability. The Russians don't charge 'true' prices either:o) > This is what is significant about Rutan's spaceplane. It is the cost Again that is because it doesn't require the amount of support team that a 'regular' rocket requires. And that's because of the principle rather than a function of design. I'd ALSO point out that we're talking a SUB-ORBITAL ride costing as much as an ORBITAL ride and stay at the ISS:o) This is not a good thing:o) (Seriously? The AWST article and the Space.com article state that the 'target' price is @ $50,000 per passenger:o) > To win the X-Prize requires a two week turn around which implies (but To be honest, it means exactly "two flights in two weeks" and nothing more:o) > The info on the Scaled Composite web site implies that most of the Actually it's also for full vehicle check outs and data gathering. But Rutan, like most of the X-Prize designers expects the second flight within ONE week, rather than two. But the plan is for less than 20 flights with SS1. > There is no reason why an improved engine of much lower maintence can't The engine 'maintenance' is not the problem. The engine can be 'refueled' within a few days, and the Lox tank filled in less than an hour. In fact the "good" thing about the Hybrid solid/liquid engine is that the entire empty solid engine casing can be removed and replaced with a full solid in less than a few hours and then topping off the Lox tank and your ready to go again. To get an ORBITAL craft though, would require a much more powerful engine and a VERY different vehicle design. (Larger at least) The SS1 'should' be able to take Mach 3, and up to 6 plus G's on entry and climb out, but it is not well designed for orbital reentry or heating. > yh728@victoria.tc.ca (Brian Burger) wrote: Just an FYI, undergoing current testing are several "X" craft from the X-40a to the X-50. Out of the 10, only two, (the X-44 and the X-48) are supposed to be Manned vehicles. (The X-43 Hyper-X MAY turn into a manned craft someday:o) The rest are ALL prototypes of Unmanned Combat Air Vehicles. (UCAV) The X-44 is to be a 'stealth' bomber version of the F-22, and the X-48 is a "Blended Wing/Body" idea for a new transport aircraft. (As a note, the X-41/X-42 are "black" projects so noone is really sure WHAT they are:o) > Likewise the first private venture of this sort to get this far Technically? The Thunderbird team has all thier gear tested and ready, they just need the funds for assembly and launch:o) The DiVinci team is awaiting a balloon and funds. So though Rutans is the only one that has parts actually flight tested, one of the other teams COULD jump ahead if they got a sudden influx of funds:o) > The X-Prize doesn't require actual orbital flight to win, just Just a correction or two:o) 1. The goal to win the prize is 62 miles. (100km) 2. They craft must carry and return 3 people or one crew and the equivilent mass of two more people. 3. The craft must be capable of flying again within two weeks. 4. The craft must use the same cabin and @80% of the vehicle again for the second flight. There are several other 'rules' to the prize. It's on the X-prize website. Randy