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Re: [Phys-l] video



At 12:10 PM 4/1/2008, John M., you wrote:
Regarding:

<http://video.google.com/videoplay?docid=369888258105653405&q=space&total=301436&start=0&num=10&so=0&type=search&plindex=0>



Brian wrote:

> An interesting challenge. If one descends at the local speed of
> sound, what is the maximum g felt for a standard atmosphere
> profile, and for how long?

That (or a slight modification of that) is a fun challenge. Of
course, the answer to the posed question is that, *if* you are free-
falling (except for drag) *at* the local speed of sound, then your
deceleration will be maximum at an altitude of zero where the density
is largest. For reasonable estimates of mass, cross sectional area,
and drag coefficient you'll get 20 to 30 g's, so I suggest not trying
that experiment!

More interesting is the question, "If you jump at a large altitude
and reach high velocities before encountering substantial atmospheric
drag, what is your maximum subsequent deceleration." So I threw
together a spreadsheet (see <http://www.csupomona.edu/~ajm/special/
kittinger.xls>) that models the motion of a falling object through an
exponential atmosphere and subject to dynamic drag.

In the case of Kittinger I used

mass = 100 kg
drag coef = .7
area = .7 m^2
surface density = 1.3 kg/m^3
scale height = 7000 m
init speed = 0 m/s
init altitude = 30,000 m
g = 9.8 m/s^2

I found that the speed topped out at 1000 m/s (~1% error from the
quoted value in the film) about 45 seconds after jumping and at an
altitude of about 22 km. I also found that the maximum deceleration
was ~4.0 m/s^2 (subjecting Kittinger to ~1.4 g's) and occurred one
minute after jumping at an altitude of about 18 km.

Now, according to Wikipedia,
<http://en.wikipedia.org/wiki/Joseph_Kittinger> ,
Kittinger fell for 276 seconds before opening his
parachute at an altitude of 5500 m. My spreadsheet indicates that he
would have reached that altitude in ~153 seconds. So the Wikipedia
value doesn't seem very likely to me unless his drogue chute a) had a
pretty substantial effect and b) was only deployed *after* reaching
the maximum speed and I guess that might be pretty likely.

John Mallinckrodt
Cal Poly Pomona

Interesting response.
It is just possible that the folks at Wikipedia were accounting for
the atmospheric temperature lapse rate, which puts the density as
high as 20% more than your values at some points in the descent.

It brings up an interesting point: it would not do for different
altimeter makers to model the atmoshpheric according to their
own lights -
as little as 500 ft difference could be crucial on some reduced
separation paths across the Atlantic - accordingly, they all
adhere to a mid-latitudes model promulgated by ICAO,
which gives numbers like
0.01842 kg m-3 at 30 km
0.08891 at 20 km
0.41351 at 10 km
0.73643 at 5 km
1.2250 at mean sea level.

Brian Whatcott Altus OK Eureka!