%0 Book
%@nexthigherunit 8JMKD3MGPCW/446AF4B
%@nexthigherunit 8JMKD3MGPGW/45823FH
%3 INPE-11422.pdf
%X An historical development since 1959 is given followed by a complete set of equations necessary for the analytical or numerical evaluation of third body perturbations on a satellite. In a caused by a third body on a satellite of a planet or primary are discussed.
%T Third body perturbations on satellites
%@secondarytype LN
%K celestial mechanics, perturbations, third body, space vehicles.
%P 140
%@usergroup administrator
%@usergroup jefferson
%@group DMC-INPE-MCT-BR
%@e-mailaddress prado@dem.inpe.br
%C São José dos Campos
%@copyholder SID/SCD
%@secondarykey INPE-11422-RPQ/763
%F self-archiving-INPE-MCTIC-GOV-BR
%2 sid.inpe.br/marciana/2004/09.21.13.37.01
%I INPE
%4 sid.inpe.br/marciana/2004/09.21.13.37
%D 2003
%@documentstage not transferred
%A Giacaglia, Giorgio Eugênio Oscare,
%A Prado, Antonio Fernando Bertachine de Almeida,
%@dissemination NTRSNASA, BNDEPOSITOLEGAL.
%@ 85-17-00010-2
%@area ETES
%@holdercode {isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S}