Re: Japans Moon Ambitions - They're KIDDING, Right ?
From: Rand Simberg (simberg.interglobal_at_org.trash)
Date: 03/09/05
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Date: Wed, 09 Mar 2005 15:08:21 GMT
On 8 Mar 2005 19:50:15 -0800, in a place far, far away, "Will"
<mclean1382@aol.com> made the phosphor on my monitor glow in such a
way as to indicate that:
>> >> >The last two add failure modes that aren't
>> >> >present with an expendable vehicle.
>> >>
>> >> No, but there are ways to mitigate component failure, by designing
>> >the
>> >> system for regular inspections.
>> >
>> >Yes. But it is an additional failure mode that reusable vehicles
>must
>> >address.
>>
>> Why do you think that they wouldn't?
>>
>
>Do you think that regular inspections will reduce failures from wear
>and fatigue to a negligable level?
It does for aircraft.
>That hasn't worked for manufacturing errors.
That's a different problem. In order to eliminate manufacturing
errors, each unit has to be inspected. For a reusable device, to look
for wear (which is a gradual phenomenon), inspections are only
required once per certain number of flights.
>> >And the last one isn't a different
>> >> category of failure--it's just part of the overall mission profile
>> >> that has to be designed for and tested.
>> >>
>> >
>> >It is a different category in that it is only relevant to reusable
>> >vehicles. It's only part of the mission profile if you recover the
>> >vehicle.
>>
>> I guess I'm failing to see the relevance, if you're saying that this
>> will somehow result in a lower reliability than low-rate expendables,
>> given a sensible flight test program.
>>
>
>What I am is disputing is how much of a reliability improvement you get
>from reusability alone. If you specify that the expendable must fly
>fewer flights, then *that* would effect reliability. But it doesn't
>necessarily follow that the expendable will fly fewer flights, as a
>comparison of STS and Soyuz shows.
You continue to miss the infant mortality issue. *Every* flight of an
expendable is a first flight. Once a reusable has a track record,
chances of it failing to a manufacturing problem is much diminished.
In addition, a reusable can be affordably flight tested before
actually carrying payloads.
>Consider a hypothetical mature expendable with more than 100 flights,
>like Delta II, with a failure rate of ca 2%. Half of that is
>manufacturing error not caught in ground tests. The other half is other
>issues, such as processing errors like ice in the propellant lines,
>tape not removed on stage separation switch, error in loading flight
>software, or wrong commands from ground control.
I would hope that the reusable design would be such as to minimize
such processing errors (e.g., flight software wouldn't require
"loading" for each flight, and "ground control" wouldn't be involved).
>Also design flaws that
>haven't shown up in the first 100 flights, weather, lightning, etc.
In the case of the reusable, a hundred flights would be a reasonable
flight test program. And an affordable one, since the marginal cost
per flight would be much lower...
>> >The optimal solution for the airline industry has limited relevance
>to
>> >reaching space, and even less to reaching orbit.
>>
>> I think that you're deeply mistaken. It has the utmost relevance in
>> doing so affordably and reliably. Sadly, the industry has ignored
>it,
>> because the market hasn't demanded it.
>
>Some of it does, some doesn't. The tricky part is knowing which is
>which. Surely you aren't suggesting that since air-breathing engines
>are optimal for airlines, they are the best way to get to orbit?
No. It's not as tricky as you seem to think.
The things that are similar are:
o Don't throw the vehicle away every flight.
o Build in lots of margin.
o Have an extensive flight test program with gradual envelope
expansion.
o Design for minimum turnaround operations.
o Keep the wheels in the well.
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