archive/ES_0.5577652473416893---------------------------

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: 2024-05-14T11:04:53.747
Launch V∞: [8.047518396728222, -5.654084331138808, 0.1757301113943622] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-0.001686635209714849, 0.0011244984107767928, 8.617797255924886e-5] km/s
	V∞_out: [-0.001437811431154941, -0.000678435519875021, 0.0012561838395124991] km/s
	time of flight: 1.8749577777247402e8 seconds
	arrival date: 2030-04-23T13:14:30.747
	thrust profile: [0.32853377356668567 -0.00021551610431456498 -0.10335084251575616; 0.07567459373936299 0.04300078116952451 -0.08854452911817322; 0.032724685358808916 0.02988244231591365 -0.06981566353634537; 0.02852814160403995 0.03411995752991902 -0.08951332590823216; 0.021430428307725315 0.03165150445317881 -0.09216378299652873; 0.010208917061145262 0.017031926148657745 -0.05582290215948696; 0.02244354639263336 0.04351708012313381 -0.15003782262632948; 0.010702235925838867 0.022673083282169666 -0.08452149127233136; 0.0032376214120921057 0.00833871045888707 -0.0339712879222845; 0.0013717165054833698 0.0035434304621692774 -0.015248500029606274; 0.0002202076559634703 0.0011831499008232405 -0.00521022907634023; 0.000401576491911328 0.003184610198598351 -0.01004350334562464; 0.0005022242929292813 0.00127205005123949 -0.0017106526374081883; 0.0009350916551997105 -0.002986585392261227 -0.003903118160273901; -0.0002035072791905708 -0.00013254060148647977 0.00044541116096879184; 0.002817097463647571 0.0004938258887278854 0.0011502699397837614; 0.002295964092092758 -0.00034425939082575205 0.0026012902880166626; -0.0016590935302775033 -0.0020341995995989707 0.0029144937490876094; -0.00453331529981395 0.0003070941289348556 -0.0024527036676236015; 0.003967238242525814 0.008459985982912543 7.858830128535809e-6] %

Mass Used: 86.28052082404201 kg
Launch C3: 96.76210304135923 km²/s²
||V∞_in||: 0.002028955802732974 km/s