archive/ES_0.5625690140581341---------------------------

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: 2024-05-11T05:56:21.983
Launch V∞: [7.855544560532541, -5.71300784136092, 0.07385434056678351] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-3.337034345446958e-5, -2.569216492654994e-5, -2.198972728300355e-5] km/s
	V∞_out: [-4.179275239545147e-6, 3.0273214148791032e-5, -3.634365161599976e-5] km/s
	time of flight: 1.8549029978598747e8 seconds
	arrival date: 2030-03-28T03:01:20.983
	thrust profile: [0.4077249235220596 0.006681766198488071 -0.10108243176412714; 0.1565916374124992 0.10210439648304646 -0.1378994234626441; 0.055268291117998566 0.06390331264299709 -0.09182271671850632; 0.06931363334664795 0.10497967155746168 -0.16824243161648464; 0.03172636001750451 0.06010072184596202 -0.11158010498596128; 0.015157346407436937 0.03762810251591306 -0.08015024002207684; 0.00445316313233704 0.015908806918640005 -0.03560307043047502; 0.004527769941231443 0.023831413448779426 -0.04443982457937043; 0.003562034479618303 0.005170238434673717 -0.014943907125492742; 0.008310693431836439 0.010700701534445621 -0.027395503557042525; -0.0028783540799751425 0.003587662331030991 -0.004924984855889851; 0.0014131654035723748 -0.0029560361823924098 -0.0020258259039598434; -0.0030088652436624994 -1.8738541664724273e-5 -0.005875433940806265; 0.0007026673697701802 0.0028945415862807254 -0.01146011932933404; -0.003801265384530227 0.007726376617782271 -0.0010450886821717752; -0.0012710313776967122 0.0038305694021876736 0.004826830341060302; 0.008570660598225515 -0.0026462824304117898 -0.012232869740943087; 0.0001062808973048186 0.0009538770914480311 -0.0053147785713103125; -0.009533458094074368 0.01398622512515 -0.007308405095731107; 0.0067784452911954455 0.0007735955058679384 0.0006556549733322597] %

Mass Used: 105.93513822524801 kg
Launch C3: 94.3534934015843 km²/s²
||V∞_in||: 4.7510159617319475e-5 km/s