Re: NASA's Ares I - The Stick is not big enough




Jeff Findley wrote:
"scottlowtherAT@xxxxxxxxxxxxxxxxxxxx" <lexcorp@xxxxxxxxxxxxx> wrote in
message news:1163623608.034946.158650@xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx

Incorrect. I quite accurately pointed out that Findley was incorrect
when he suggested that the Shuttle and the Ares 1 faced the same sort
of problems. The fact is... they *don't.* Shuttle started off as a
vastly more ambitious and complex concept than Ares did.

Ares I/V are most certainly less complex than the entire shuttle system.

And otherwise almost wholly different in design and concept to the
shuttle. The engineering challenges are not the same.


The long pole in the tent, last I checked, is the J2-X.

Which will be needed anyway for Ares V.

The biggest unknowns are likely from the components that aren't shuttle
derived (i.e. the J2-X), but I wouldn't count out significant teething
problems with the 5 segment SRB's either.

I would be surprised if *significant* issues arose. A five-segment RSRM
was slapped together and put on the stand, and it ran fine; nothing
about it was optimised. Hell, they made a bigger-throated-nozzle for
the 5-seg by the simple expedient of machining out several inches of
graphite from the existing RSRM throat, and it didn't even disintegrate.

.



Relevant Pages

  • Re: NASAs Ares I - The Stick is not big enough
    ... Jeff Findley wrote: ... Then it doesn't bother you that Ares I is starting out having the same sort ... Nowhere near the same problems that Shuttle had in the beginning. ... Ares I, in comparison, is a straightforward engineering design effort. ...
    (sci.space.policy)
  • Re: NASAs Ares I - The Stick is not big enough
    ... Jeff Findley wrote: ... Nowhere near the same problems that Shuttle had in the beginning. ... Ares I, in comparison, is a straightforward engineering design effort. ...
    (sci.space.policy)
  • Re: NASAs Ares I - The Stick is not big enough
    ... Jeff Findley wrote: ... Nowhere near the same problems that Shuttle had in the beginning. ... hypersonic aerodynamics of the orbiters and boosters, ... Ares I, in comparison, is a straightforward engineering design effort. ...
    (sci.space.policy)
  • Re: NASAs Ares I - The Stick is not big enough
    ... I quite accurately pointed out that Findley was incorrect ... when he suggested that the Shuttle and the Ares 1 faced the same sort ... vastly more ambitious and complex concept than Ares did. ... little temporary safety deserve neither liberty nor ...
    (sci.space.policy)
  • Re: Warum besteht Sojus aus drei Teilen
    ... bemannte Starts geeignet wäre, weil der Shuttle es ja auch ist. ... man wolle die um das Shuttle ... Ares V, das Ding verwendet ja auch zwei SRBs und den ET des STS ... das CEV anstatt auf Ares I auf Ares V zu starten. ...
    (de.sci.raumfahrt)