A comment in line with my sine vs cycloid thinking :

http://science.slashdot.org/story/13/02/15/1747226/asteroid-2012-da14-approaches?utm_source=rss1.0mainlinkanon&utm_medium=feed
 
Re:are we sure it has nothing to do with DA14? (Score:4, Informative)
by Clueless Moron (548336) on Friday February 15, @02:51PM (#42914591)

No... if that meteorite was in an orbit 30,000km radius from DA14 (which it 
would have to have been in order to hit Russia when it did), its orbital 
velocity would necessarily have to be very low. As in, so slow it would take 
millenia to complete even one orbit. Since DA14 is moving at a whopping 
30km/second relative to Earth, anything orbiting it that far out would be 
moving in virtually the same direction and speed with respect to us.

In short, there's no way that meteorite could have been orbiting DA14

- - - - - - 
I plugged the best numbers I could find into a spreadsheet.

The asteroid of mass m1 passes d1 above earth, with velocity v1
For the meteor to just graze earth 16 hours ahead of the asteroid, it must be 
d2 = time*velocity ahead of it.

We then have a right triangle with sides d1 and d2 ... hypotenuse d3 = radius 
of orbit.

Ignoring the mass of the meteor, we have the period 2 pi * sqrt( d3^3 / G m1 )

Indeed, it gives an orbital period of 153 millenia -- so they're pretty much 
travelling in the same direction. No cycloid motion.

Asteroid 2012 DA 14 and Russian meteorite
        v1      2013.2.15:A

        v1            30km/sec        30000m/sec   Velocity of asteroid relatve 
to earth
        d1         27000km         27000000m       Distance from surface of 
earth
        t2            16hrs           57600secs    Meteor ahead of asteroid 
(hours)
        d2                       1728000000m       v1*t2   Meteor ahead of 
asteroid (m)
        d3                       1728210925        sqrt(d1^2 + d2^2) Radius of 
meteor orbit

        m1        130000tonnes    130000000kg      Mass of asteroid
        G                           6.7E-11        G       gravitational 
constant

        t2                      4.83674E+15        orbital period seconds = 2 * 
pi * sqrt ( d3 / G m1)
                                1.34354E+12        hrs
                                55980833311        days
                                153372146.1        years

Reply via email to