[AR] Re: shuttle SRBs (was Re: Re: Phenolic regression rate)

  • From: John Schilling <john.schilling@xxxxxxxxxxxxxx>
  • To: arocket@xxxxxxxxxxxxx
  • Date: Wed, 7 Feb 2018 19:54:22 -0800

I think that not all failures require the use of an LES, at least in the narrow sense of "LES" that you are implicitly using here.

        John Schilling
        john.schilling@xxxxxxxxxxxxxx
        (661) 718-0955


On 2/7/2018 7:09 PM, William Claybaugh wrote:

John:

I find this interesting coming out of Circle A: you think that an LES of fixed probability of successful operation is better used on vehicles that fail much more often than on vehicles that rarely fail?

Did I get this right?

Bill

On Wed, Feb 7, 2018 at 7:42 PM John Schilling <john.schilling@xxxxxxxxxxxxxx <mailto:john.schilling@xxxxxxxxxxxxxx>> wrote:

    On 2/7/2018 9:47 AM, William Claybaugh wrote:
    > Henry:
    >
    > You do seem very fond of this “...but failures can be catastrophic”
    > line.  However, what happens to the rockets after the escape system
    > activates is *irrelevant* to crew safety.

    Except for the cases where the escape system itself is what endangers
    the crew.  And then there's the cases where the escape system doesn't
    activate and you've got no other option.

    Escape systems that can escape all or all-minus-epsilon of the failure
    modes of large solid rocket motors, are not going to be low-risk items
    from a reliability or safety standpoint.  And the ability to quietly
    turn off the propulsion system of a launch vehicle, rather than having
    range safety blow it up, may facilitate abort modes other than sudden
    bursts of 15-g rocket thrust (from rockets that might themselves fail
    catastrophically).   Save the LES, or at least the hard-mode LES, for
    the times when you absolutely can't live without it.

             John Schilling
    john.schilling@xxxxxxxxxxxxxx <mailto:john.schilling@xxxxxxxxxxxxxx>
             (661) 718-0955


Other related posts: