... Solanki S. K. Small-scale solar magnetic fields: An overview // Space Sky . ... Fe I 5247,1 5250,2 е, Fe I 6301,5 6302,5 е. ), . ... Lvm 5250 , 6301 ­ . ... k, rv- (rvw), rv- - (rvf). , rvo = rvf + k* rvw, rvo ­ . ... 2 , Lvm, [6] е 5247 40,5 5250 58,5 6301 67 6302 73 Lvm, [5] 40,8 40,8 64,8 58 Lvm, k=0,8 40,8 53,2 65,5 65 Lvm, k=-0,8 39 61,2 69,5 80 Lvm, k=3,0 40,8 44,8 65 61 Lvm, k=-3,0 27,2 53,5 65,2 49,5 80 86 If*f, rvo = (rvf + k*rvw)/ [1 + (1-f)/f *Ip/If], k = (Ip*p)/(If*f) = 0,72p/f (3) (2) ....

Space Development: Theory and Practice 2005 . ... During the conference the participants had an exclusive opportunity to visit such Russian enterprises associated with Space industry as Scientific and Production Association “Zvezda”, which designs and produces helmets, spacesuits and emergency evacuation systems for aviation; Khrunichev Space center which is one of the world’s leaders in launch vehicle and spacecraft development ; Rocket and ...

... Moon Phase below . ... ARTICLE: Why the moon always shows us the same face . ... Before you continue reading, you should know that this was not always the case, i.e. the Moon once was rotating with respect to the Earth, so that on every night a terrestrial observer (if there was one, because this was long, long before mankind appeared on our planet, and even before any major animals had appeared) saw another face of the Moon. ... Figure 1 (not to scale) shows how we can imagine the system Earth-Moon...

... 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 . ...