archive/ES_0.5759047319107596---------------------------

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: 2023-04-28T05:47:48.791
Launch V∞: [6.720472210476635, -7.229183672225476, -1.1518974179902584] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [7.601252561439375e-8, -1.3879613304695228e-7, -5.6472396787448664e-8] km/s
	V∞_out: [5.498637435121226e-8, -7.609409276796132e-8, 1.352934518070403e-7] km/s
	time of flight: 1.8749577786239022e8 seconds
	arrival date: 2029-04-06T07:57:25.791
	thrust profile: [0.19684388088101892 -0.043933861083873836 -0.06407826299888597; 0.10522574891426507 0.036376169874497745 -0.09889183420358107; 0.06899041171362295 0.045726350439430755 -0.1083252800015999; 0.05459859031660195 0.049343776708167586 -0.12319137439832384; 0.03891419421836974 0.04447924699591419 -0.11298298834724146; 0.032264663156279114 0.04380688155442781 -0.11639083433690427; 0.032572733307362975 0.05035274967021794 -0.14004727308466935; 0.01654501896821645 0.0307172734101273 -0.08565200027109766; 0.0071112255434205495 0.014463615706806853 -0.043328542744931725; 0.0033376903074766795 0.006130126258006691 -0.01575453198032888; 0.002917308549846235 0.005585561165715964 -0.015842397074839105; -0.0010023786737326226 -0.0008503788608702858 0.00034505453215565073; -0.00015380008264866346 0.0009236545742651698 -0.0038368622707844703; 0.0054893480057191454 0.009831066651569227 -0.007575763208877753; -0.0008609719545968355 0.002644362953145518 -0.010747052072582175; -0.0088502411564154 -0.00434652599416645 -0.01338299460190695; 2.0280680368950742e-5 -0.0008452560005194985 0.0016970578316862087; -0.0008142459357422518 -0.0033783963313586234 0.005204561339178297; -0.0032366568588371543 -0.002280080081716326 -0.0035064088366809536; -0.0013930361038713528 0.0002262785425424997 -0.0011981737540748489] %

Mass Used: 95.83137329511192 kg
Launch C3: 98.75271096013275 km²/s²
||V∞_in||: 1.680220289068823e-7 km/s