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Planetary and Space Science
Volume 45, Issue 5 , May 1997, Pages 595-602
Asteroids, Comets, Meteors 1996 - I

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doi:10.1016/S0032-0633(97)00039-1    How to cite or link using doi (opens new window) Cite or link using doi  
Copyright © 1997 Published by Elsevier Science Ltd.

Meteoroids captured into Earth orbitnext term by grazing atmospheric encounters

Jack G. HillsCorresponding Author Contact Information and M. Patrick Goda

Theoretical Astrophysics Group, T-6, M.S. B288, Theoretical Division, Los Alamos National Laboratory, Los Alamos, NM 87545, U.S.A.

Received 2 September 1996;  revised 7 February 1997;  accepted 10 February 1997. ; Available online 8 June 1998.


Abstract

Some meteoroids, such as the one that produced the daytime fireball of August 10, 1972 that passed over the western United States and the European fireball of October 13, 1990, graze the atmosphere of Earth before returning to space (at reduced previous termspeed)next term. Other grazing meteoroids, such as Peekskill, penetrate deeper into the atmosphere and lose enough energy to plunge to ground. It is evident that if a grazing meteoroid is within some critical range of closest approach distance and previous termspeed,next term it is captured into a gravitationally bound previous termorbitnext term around Earth. It must ultimately plunge to ground after further orbital dissipation in subsequent atmospheric passages unless the gravitational pull of the Moon and Sun or other intervention raise its perigee above the atmosphere. A spherical atmospheric model is used to integrate the passage of meteoroids in grazing atmospheric encounters. It is found that the corridor for capture narrows with increasing values of Vinfinity, the approach velocity of the meteoroid prior to gravitational acceleration by Earth. As an example, if Vinfinity= 5 km s-1, stony meteoroids with closest-approach distances of h = 40 km above the Earth are captured if their radii, R, are between 3 and 9 m while if Vinfinity = 15 km s-1 and h = 40 km, they are only captured if R is between 1.5 and 2m. Irons with Vinfinity = 5 km s-1 and h = 40 km, are captured if R is between 1 and 3.5 m, while if Vinfinity = 15 km s-1, they are captured if R is between 0.6 and 0.9 m. The cross section for orbital capture of iron meteoroids and small stony meteoroids is about 0.001 that for directly hitting Earth. Large stones are never captured except at very low impact velocities because of the large increase in drag resulting from fragmentation.


Corresponding Author Contact InformationCorresponding author. Correspondence to: J. G. Hills



This Document
Abstract
Abstract + References
PDF (869 K)

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Planetary and Space Science
Volume 45, Issue 5 , May 1997, Pages 595-602
Asteroids, Comets, Meteors 1996 - I


98 of 230 Result ListPreviousNext
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