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distances.m |
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dist_MtoE = 401.3e9; %m %GMO orbit distance. Ts = 88642; %sec rmars = 3397e3; %m Mmars = 6.4191e23; %kg G = 6.672e-11; R_GMO = (sqrt(G*Mmars)*Ts/(2*pi))^(2/3) - rmars; %m Vsat = 2*pi*R_GMO/Ts/1e3; %km/s %max dist to ground term from satellite d = sqrt((rmars)^2+(rmars+R_GMO)^2); %distance between two GMO satellites dist_sats = sqrt(3)*(R_GMO+rmars) %beamwidth requirements sat-term link beamwidth_sat = 2*atand(rmars/R_GMO) dist_sats = 3.5382e+07 beamwidth_sat = 22.5609 |
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