![]() |
|
|
Thread Tools | Display Modes |
|
#1
|
|||
|
|||
![]()
Jeff Findley wrote:
"Pat Flannery" wrote in message ... Pat Flannery wrote: Over at NASA Watch, the ESMD PAO has said they are reviewing Cowing's questions and expect to get a reply to him within 48 hours. Pat And here's their reply: http://www.spaceref.com/news/viewnews.html?id=1266 From their reply, "These longitudinal forces may increase the loads experienced by the Ares I during flight, and may exceed allowable loads on various portions of the vehicle and allowable forces on the astronaut crew. ", followed later by, "Thrust oscillation forces may be reduced by vehicle structures, as is the case with the space shuttle and Titan IV", and later by, "The Orion and Ares teams are holding detailed discussions and developing a plan to fully characterize Ares I thrust oscillation, assess any design changes that may be proposed, and manage sensitive design parameters with additional tests, trade studies and analyses". So they're still trying to characterize the thrust oscillation and see how it impacts the design. Unfortunately, experience from Titan IV and shuttle isn't quite directly applicable since both of those use twin SRB's side mounted to a central, liquid, core. Ares I is a distinct departure from this design with only one SRB and one upper stage on top of the SRB. And I absolutely love this little gem from near the end of the NASA response, "Thrust oscillation is a new engineering challenge to the developers of Ares". Maybe this is new to upper management, but I'm sure that there are a few propulsion engineers at Thiokol and NASA who saw this one coming. It's a problem that would have manifested itself with any inline design using a shuttle derived SRB for the first stage. Considering the weight issues associated with Ares I and Orion, there isn't much in the way of excess mass which can be spared to throw at this problem. It's starting to look like Ares I is a real pig of a design. Large segmented SRB's ought not be used on any new launch vehicle. Their drawbacks aren't worth their perceived advantages. Wow, and it only took you two and a half years to figure that out. I left for the Bahamas in the spring of 2005 confident that not only would Griffin not be confirmed, but that this vehicle would be excluded on first principles physics arguments alone. Was I ever surprised and horrified after I dragged my sorry ass back to the states after the two worst hurricane seasons I have ever experienced, and the ensuing two and a half years have been just one nightmare after another with this thing. At least the hurricanes have been cooperating since then. I'm surprised it took Cowing so long to figure this out. |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
Keith Cowing Makes His Move | kT | Space Shuttle | 35 | January 18th 08 02:45 PM |
Keith Cowing Makes His Move | kT | Space Station | 26 | January 18th 08 02:45 PM |
Rand pisses off Keith Cowing | Jeff Findley | Policy | 6 | August 20th 07 02:42 PM |
Keith Cowing tells it how it is . . . | Tom Merkle | Policy | 6 | February 3rd 04 02:24 PM |
A really great essay by Keith Cowing | Al Jackson | Policy | 429 | December 22nd 03 02:30 PM |