... 23 Algorithm fo r evalua tion of two burn maneuv ers using linearity Input information: ( t t E1 , rEI , v t1L , t E2 2L ( ) EI )T )T ­ ­ ­ ­ the time and the state vector of initial orbit for this time ; interval of possible thrusts for transition from initial orbit to the transfer on e; the time and the state vector of the target orbit for this time ; ... We cal culate the state vector for the initial orbit for the time t1a and the target one ­ for the time t2 a . ...

... Страница: Космос станции , Mars Global Surveyor ( Part #1 , Part #2 , Part #3 , Part #4 , Part #5 ), Mars Odyssey ( Part #1 , Part #2 , Part #3 , Part #4 , Part #5 , Part #6 , Part #7 ), Разведчик MRO ( Part #1.1 , Part #1.2, Part #2 , Part #3 , Part #4 , Part #5 , Part #6 , Part #7 , Part #8 ) , Mars Express ( Part #1 , Part #2 , Part #3 , Part #4 , Part #5 , Part #6 ), Миссия Phoenix ( Part #1 , Part #2 , Part #3.1 , Part #3.2 , Part #3.3 , Part #3.4 ), Фобос-Грунт ( Part #1 , Part #2 , Part #3 );...

... GCR and SCR are primary cosmic rays. 10-15 years after the discovery of cosmic radiation (1919) there emerged two main avenues of investigation in the physics of cosmic rays (CR): 1) nuclear - elucidation of the origin of elementary particles and nuclear interactions; and 2) astrophysical (space physics) - solution of the problem related to the origin and variations (changes in intensity) of CR. ... Besides, the CR flux in interplanetary space is, strictly speaking, not isotropic. ...