archive/ES_0.5806858804953149---------------------------

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: 2023-04-24T08:58:11.439
Launch V∞: [5.53086756865834, -8.130440593057426, -0.41840490544719705] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [1.5517346847532922e-8, -7.229121907997683e-9, 1.315697814972357e-8] km/s
	V∞_out: [5.906552933325535e-9, -1.3137557622859933e-8, -1.7420039362662866e-8] km/s
	time of flight: 1.5163516666761318e8 seconds
	arrival date: 2028-02-12T09:50:57.439
	thrust profile: [0.2970385818794691 -0.1417450984468394 -0.12051763206125761; 0.1432721534138985 0.008499847149275146 -0.14372063895865747; 0.11102406378386168 0.032187913998651195 -0.174034251981472; 0.08965344754381711 0.03950230118119863 -0.18697543352671298; 0.07293112386734418 0.04020477297388168 -0.1847559634303198; 0.05516037362274949 0.034570477797835036 -0.16407162193122746; 0.05495442888135294 0.035250030297224406 -0.173922546728768; 0.023258934972142743 0.01635325655353703 -0.08755735734491994; 0.0188031504297443 0.01625249907637369 -0.06945463944512159; 0.0037127875409874705 -0.0007877666440181015 -0.01078634950610139; 0.004314600740175698 -0.003921635518613149 -0.007802894343559717; 0.0001446733396978714 -0.0008220105659735625 -0.004695063086711427; 0.004567807665913775 -0.001638751884981774 -0.006710712831090211; -0.0038746406704187695 0.0029094100161481977 0.004003143583446626; -3.8636358770376134e-5 0.0032489678810691605 -0.002716895023753746; 0.002509117623450045 0.007025093391113892 -0.013128652738717802; 0.007465812380110597 -0.0031337135677679834 -0.004301298466561702; -0.000547310994983949 0.0018684056262103354 -0.0022864934211250156; -0.0017267898574535876 0.02691287259247928 0.019290655649965297; -0.0017163213549582484 0.051541596373187934 0.005707213708748814] %

Mass Used: 112.39405995351399 kg
Launch C3: 96.86962296417487 km²/s²
||V∞_in||: 2.159060746666558e-8 km/s