Re: msnbc/oberg: 'Murphy's Law' rules outer space

From: Jeff Findley (jeff.findley_at_ugs.nojunk.com)
Date: 10/22/04


Date: Fri, 22 Oct 2004 09:52:17 -0400


"Christopher M. Jones" <christopher.m.jones@gmail.com> wrote in message
news:opednYendPQal-TcRVn-hQ@comcast.com...
> To bring in a different set of examples, Mars Polar
> Lander and Mars Climate Orbiter. Different designs,
> different spacecraft, different sub-systems, both
> failures. The reason behind the failures lies not
> in redundancy but in the organization.

I made the point later in my posting that you shouldn't have your first and
only test flight also be the operational mission. That definately falls
into the "organization" category.

> > I'd actually say that integration testing and full up test flights are
more
> > important than budget and design.
>
> This also can fail. As with Galileo, where a g-test was
> performed on the Jupiter atmospheric probe. However, the
> test was invalid because the test harness was wired
> backwards (fyi, Oberg covers this in his article). An
> organization with a high rate of failure is also likely to
> have a high rate of failure in testing procedures. There
> is no silver bullet solution in design, or testing, or
> funding, or anything of that sort for organizational problems
> on this scale, the only solution is fixing the organization.

This is true. A healthy organization will generally perform analysis,
design, integration, and testing in far more optimal ways than an unhealthy
one. The challenge is how to change the "culture" so that the organiztion
becomes healthy. One way to do this is for everyone to really focus on the
processes involved and constantly work to optimize them.

Unfortunatley, I think that unhealthy cultures generally fight change. As
an example, they tend to implement changes like ISO standards to satisfy the
"letter of the law" instead of the spirit. Things like ISO standards can be
viewed as tools to actually help you improve you processes. Unfortunately,
too many companies become focused on ISO certification as a goal in and of
itself. In doing so, they completely miss the opportunity to add value to
their processes.

> Reusability doesn't necessarily gain you much depending on
> how you fly and test. If you fly irregularly and constantly
> tweak the vehicle then, as with the Shuttle, you never really
> know how reliable the mission is.

While this is true, I don't think of the shuttle as a truly reusable
spacecraft. You simply can't "gas and go" between missions. Remember the
times when the SSME's were routinely pulled from the orbiter and torn down
for inspections on each and every flight? That's not reusing the SSME's,
that's rebuilding them. Same thing goes for the SRB's. And the ET clearly
isn't reusable.

> If you fly regularly enough
> and start off with a serious testing regime then you can be
> more confident. However, for experiments like Genesis this
> really isn't the answer. A more bug-tested spacecraft bus
> (and return capsule) would help, but the spacecraft would still
> be fairly custom.

This is true. Until unmanned probes are being sent out in the thousands per
year, you're going to have real trouble getting the reliability up. We've
got a long way to go.

As for manned spaceflight, I'm betting the CEV will be about as reliable as
the shuttle. This is mostly due to similar (low) flight rates and the fact
that the same organization will be running the program. I don't believe
that there will be anything fundamentally different about the way the CEV
program will be run that will make it more reliable.

Jeff

-- 
Remove icky phrase from email address to get a valid address.


Relevant Pages

  • Re: Lack of bit field instructions in x86 instruction set because of patents ?
    ... You do not get genuine reliability by complexity; ... evidence for) the claim that ALL failures ... the design in such a way that you haven't introduced new error modes. ... Compare the Internet to the phone system: ...
    (comp.arch)
  • Re: Lack of bit field instructions in x86 instruction set because of patents ?
    ... systems do not provide genuine reliability, ... the design in such a way that you haven't introduced new error modes. ... designed with the assumption that failures would be common -- which gave ... In practice failures are not as common as expected, ...
    (comp.arch)
  • Re: SpaceX Falcon I Hold-Down Firing Scheduled
    ... > willing to accept some failures. ... > this company who calulated the reliability etc. ... Will they not launch the ... It's the difference between a design calculation and a test measurement. ...
    (sci.space.policy)
  • Re: Lack of bit field instructions in x86 instruction set because of patents ?
    ... started with a naive design and, as each error is discovered, they hack on the code to deal with it -- introducing multiple new errors, so the complexity grows exponentially. ... practice rarely if ever suffer massive failures. ... Compare the Internet to the phone system: the Internet has never been entirely down in its entire history, while the phone system has -- but people think the phone system is more reliable because it only has a system-wide outage once a decade or so, while we experience tiny parts of the Internet being down every day... ... failures does NOT lead to reliability of the whole - the DNS! ...
    (comp.arch)
  • Re: Lunacy from Brussels
    ... "The first serious attempt to design a nuclear pulse rocket was Project Orion (See the article for details, including the vehicle sizes, problems, propulsion cycle and shielding). ... Orion reacted small directional nuclear explosives against a large steel pusher plate attached to the spacecraft with shock absorbers. ... This low-tech single-stage reference design would reach Mars and back in four weeks from the Earth's surface (compare to 12 months for NASA's current chemically-powered reference mission). ...
    (sci.electronics.design)