archive/ES_0.5656318919458854---------------------------

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: 2023-04-28T11:26:50.133
Launch V∞: [6.801249158576139, -7.164221208361966, -0.20139543678908628] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-1.5159712962324358e-7, -3.906061881736378e-8, 4.9877171321908124e-8] km/s
	V∞_out: [-1.5272723310754315e-7, 4.076810452714763e-8, -3.907059726486791e-9] km/s
	time of flight: 1.8749577784859926e8 seconds
	arrival date: 2029-04-06T13:36:27.133
	thrust profile: [0.26688594181570857 -0.06783928549399068 -0.09610082523228398; 0.08585572768021166 0.025000030921855713 -0.09409264904645555; 0.05011556347383327 0.028175366131781596 -0.09366415121776868; 0.0503382085997942 0.038386068840181545 -0.1324794777591383; 0.041427932727718206 0.040346622371516025 -0.14218570126556354; 0.036231112522750346 0.039660200816823976 -0.1527676718889515; 0.014501342835617645 0.017360067115293663 -0.07206970423812327; 0.012254552307270307 0.016309433153300093 -0.07063254568369222; 0.003897854874180987 0.005450873756483766 -0.02511822957502231; 0.002096952609001236 0.0030350921864929613 -0.015088568834353734; 0.00017822605275980696 0.0006864256431083968 -0.002180565845110942; -0.0004092645619534507 0.001555989147955442 -0.0024388157281943473; -0.00012607719092153275 0.00017901499299290624 -0.0017850921646472692; 0.00046518386015274133 0.0010065152047265633 -0.00323036146075951; -0.0013327536305031797 0.0008377156928908024 -0.0006928076537745299; 9.051124284833491e-5 0.0013416065262417452 -0.002605537364239441; 0.00046799032698465945 0.002320883170037838 -0.0019499385008292032; -0.0003339074272884386 2.1502412087370793e-5 0.0016391273903721298; 0.0016200058906725657 0.0029023550730484828 -0.002113159898481802; -0.0017657061755024508 0.0015963183908782406 -0.0022915590021072556] %

Mass Used: 90.43278199574252 kg
Launch C3: 97.6236157613355 km²/s²
||V∞_in||: 1.6430202029030832e-7 km/s