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RE: nuclear plant threat (off-topic answer to a semi off-topic observation)
Good point. In recent literature, Clive Cussler used a variation of that
scenario (an LNG 'tanker' ship in the NY ship channel.
Dave Neil neildm@id.doe.gov
-----Original Message-----
From: Tim [mailto:tstead@ntirs.org]
Sent: Thursday, November 08, 2001 3:29 PM
To: radsafe@list.vanderbilt.edu
Subject: RE: nuclear plant threat
I think that some of the most vulnerable are the LNG
tanks at New York harbor that are "guarded" by simple
chain link fences. A terrorist could simply plant a
bomb next to one and light up half of Eastern NYC!
Why aren't the anti-nukes screaming about the Port of
new York then? Are they really interested in safety
or just interested in shutting down nuclear plants?
Tim
--- "Franta, Jaroslav" <frantaj@AECL.CA> wrote:
> Chris,
>
> I think that your & Glen's points are very good.
> I would just like to add some numbers to the point
> Glen was making -- FYI,
> the wingspan of a Boeing 767 (for example) is 47.6m
> (as compared, for
> example, to the 44m O.D. of a CANDU-6 containment
> dome), but its engines are
> only 15.6m apart - or 7.8m from the plane's center
> line. So if the plane
> were to impact with its fuselage centerline exactly
> aligned with the
> building centerline, then the engines would impact
> on the wall at an angle
> of 69° -- ie. 21° off perpendicular (and assuming a
> perfectly in-plane
> horizontal approach at an altitude of only a
> dozen-or-so metres !!! ....the
> width of the fuselage is 5m and overall height is
> 15.9m.... normal runway
> approach speed with MLW - maximum landing weight -
> is about 165mph or
> 265kph, according to Jane's All the World's
> Aircraft).
> As Glen said, for missiles "striking concrete
> structures.... there is a
> significant reduction in
> penetration if the impact vector is anything other
> than normal to the impact
> surface. Even if the containment were flat, if the
> shaft of the engine did
> not strike the surface perpendicularly, the shaft
> will rotate and slam
> broadside into the containment. The force instead
> of being over the cross
> sectional area of the end of the (airliner engine)
> shaft is then dispersed
> over the entire cross sectional are of the long side
> of the shaft. The
> resultant penetration is <5% of that for a normally
> incident crash."
> Its very unlikely that a perfectly perpendicular
> impact could be achieved on
> a cylindrical structure, unless you put the plane on
> a rail track, like the
> F-4 Phantom in the 1988 Sandia test, with an 8m
> offset from the center line
> of the building....
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