archive/ES_0.7229658741792592---------------------------

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: 2023-04-26T04:58:22.374
Launch V∞: [6.817415198660851, -9.050186328316482, -2.5497544749861007] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-0.18036929735982798, 0.11780648735228626, 0.22343357031044783] km/s
	V∞_out: [-0.10477967874491005, 0.20983230372792613, -0.20326861464195797] km/s
	time of flight: 8.595403584418784e7 seconds
	arrival date: 2026-01-15T01:05:37.374
	thrust profile: [0.6207796013332625 -0.4734784760949419 -0.26927337520627753; 0.33737146286563063 -0.09938736619226989 -0.20567046054287422; 0.08948587978421023 -0.010671230929828673 -0.06913025888433494; 0.030013300962707976 -0.001857509240817201 -0.03196419318914327; 0.017950672317508125 -0.0009619234772463097 -0.02380270304894358; 0.01966881661959937 0.0018889008343605388 -0.02325517129843572; 0.015600729949247315 0.008539953681030912 -0.002083342384499748; 0.006291242987827764 0.0010940630043272783 -0.01075814033729755; 0.0059183178088441325 0.00808994689161095 -0.002310630472914118; 0.019008365203213987 -0.011618556832259624 -0.014582140831576761; 0.01674749658440002 0.010846975394147102 -0.008898089560404297; 0.011414027610637836 -0.0003646199357775527 -0.007854316765338851; -0.012655924680223352 0.00026741402492224124 -0.014266000675066233; 0.009040983156963465 0.0016557168087949978 -0.014336757306941506; 0.015646690846797505 0.0052492429093055 -0.002192748514076335; 0.006616617090472825 0.002407404862278792 -0.007319155955145786; -0.000847178801116644 0.011984121724496755 -0.006185400035078891; -0.0007684775392023651 0.0004947046541609419 -0.004046188363472475; -0.004451781328127392 0.007737648739197037 -0.009750453074899308; 0.006622812490502887 0.0015708059003953917 -0.00011777321590291344] %

Mass Used: 56.63527557894304 kg
Launch C3: 134.88427045089017 km²/s²
||V∞_in||: 0.31037720959187104 km/s