archive/ES_0.5584429447437844---------------------------

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: 2024-05-14T02:17:52.324
Launch V∞: [8.09760431841875, -5.577596394711461, 0.19504763274697234] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [4.718874063181292e-7, 2.8808312984067874e-6, -7.217577432141387e-5] km/s
	V∞_out: [-2.352127599197437e-6, 7.219283104182641e-5, -4.1795826454178993e-7] km/s
	time of flight: 1.874957778749395e8 seconds
	arrival date: 2030-04-23T04:27:29.324
	thrust profile: [0.3867438194164464 -0.001476876664611271 -0.12210135984891601; 0.02941897801312988 0.017116098570348952 -0.03821840830910572; 0.019761558851728644 0.016940042009378754 -0.04495942017439206; 0.01418823161351085 0.017821108443595125 -0.049227360294415226; 0.0250494322568418 0.037007313913291005 -0.11209629443500395; 0.017483548598798734 0.030597249208876996 -0.10393325427962968; 0.011805529132073155 0.024787959669289934 -0.08529524721059284; 0.009988884493248988 0.022886854892675595 -0.08772910846022519; 0.005674618346712551 0.01686249304930908 -0.06363435826080682; 0.006158874933405746 0.018182954589950076 -0.07942396286828408; 0.0011273057701149923 0.0036733687037338535 -0.016157160819610487; 0.0002576896195340551 0.001332586963521111 -0.008501319998867577; 0.00030439723175138667 -0.0020220551430987096 0.00048043194225113966; 0.0006063291610861019 -0.00046845612613901467 0.001606007457374475; -0.0009163055798300767 -0.0017464196873902575 0.0015383201597551706; -0.0009329088733031975 -0.0015967948738649976 0.002704466931513382; -0.0010875522684424693 0.0004949211046158193 0.0037308447635007753; 0.0006065214665526556 -3.402361074853876e-5 0.001841810240900569; -0.00018870917482093435 0.0019990674492034594 -0.0008023015091297071; -0.0014233976458744753 -0.004111158921140829 -0.001980063088964559] %

Mass Used: 87.3236474235091 kg
Launch C3: 96.71882081901246 km²/s²
||V∞_in||: 7.223478570321771e-5 km/s