archive/ES_0.5600396446680661---------------------------

Spacecraft: mySat
	dry_mass: 200.0 kg
	specific impulse: 3200.0 kg/s
	max_thrust: 0.00025 kN
	num_thrusters: 1
	duty_cycle: 1.0
Launch Mass: 3500.0 kg
Launch Date: 2024-05-15T17:20:29.218
Launch V∞: [7.971700528415906, -5.842591802096005, -0.12332839055951829] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-1.849409789403285e-9, 1.986102373301159e-9, 8.113216054707976e-10] km/s
	V∞_out: [1.8294145594700012e-9, -1.7133647276574294e-9, -1.4631117271962397e-9] km/s
	time of flight: 1.8562765478514493e8 seconds
	arrival date: 2030-04-03T04:34:43.218
	thrust profile: [0.23949714139401568 -0.010460865912826967 -0.08721254946499404; 0.11573931354048868 0.05607164725307729 -0.14065015680215764; 0.03061049156788385 0.024659511186986786 -0.07142005831802682; 0.02540702302377544 0.02582894856549493 -0.08480808653918392; 0.021518654506148673 0.024836816530296863 -0.09311812461628316; 0.016956937609448657 0.023293268849772703 -0.0963065816612169; 0.013178454775373662 0.018928216770066692 -0.08408500489051485; 0.007830471762718645 0.013382516562408622 -0.06401194304586054; 0.0057600097280943625 0.010180613441406191 -0.0525251566123857; 0.001881185645772929 0.00403546875444719 -0.02126999499661127; 0.0016864383089297496 0.005118399994095751 -0.031025578732172047; -0.00011609021130545688 -0.000647707937508528 -0.0015876285385581076; -0.0009439770807728955 0.0001934929868720471 -0.001402526359680602; -0.005967922558099161 0.0008364973057112194 -0.008100486704765309; -0.004628969188365092 -0.0029771088852978797 -0.002503875602572957; -0.0007589612868985739 -0.0005307735157486088 0.0024560883516418462; -0.0006636837539894721 0.0003937387299088251 0.0001715928901486317; 0.0006979690562153344 0.0008765533639857972 0.006154889480629502; 0.010037079489686053 -0.004850541992367499 0.00022403684905817375; -0.0025519329620106667 -0.0032302354164662032 0.009195649670692745] %

Mass Used: 83.46817943933775 kg
Launch C3: 97.69909817258389 km²/s²
||V∞_in||: 2.8325186590518536e-9 km/s