archive/ES_0.558941838206383---------------------------

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: 2024-05-14T05:55:39.871
Launch V∞: [8.04599126330741, -5.767317503521621, 0.09400031040637756] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [1.2637159192593738e-5, -2.0864654362604635e-5, -9.211709167177464e-5] km/s
	V∞_out: [-8.701000416723068e-5, -1.01719855467747e-5, 3.7055378887156685e-5] km/s
	time of flight: 1.8430278841463128e8 seconds
	arrival date: 2030-03-17T09:08:47.871
	thrust profile: [0.22576753198430755 -0.0061779037583529605 -0.07801235330633721; 0.06119943136321726 0.03136178471005857 -0.07727930771858418; 0.039480785975172225 0.031983752623796255 -0.08831022580725328; 0.04099395647191182 0.04181005588108715 -0.12631454594425917; 0.021551207118390092 0.02816092951158314 -0.09446159721944089; 0.013132498467546381 0.018762206722224742 -0.07163659137935709; 0.01495775801608952 0.025915868472215362 -0.10242804542591533; 0.011362080126795016 0.022444731354361952 -0.09569558458798368; 0.004524600317872273 0.008935968592034087 -0.04231563304776098; 0.0035658995906446894 0.00762867726032972 -0.03680518764146798; 0.0016654554762708807 -0.0017096853927092554 -0.0018155389618796742; 0.000256340108319981 0.00020959033584054223 0.0005547429925850107; -0.0012033820892899019 -0.000928078608651623 -0.0039452951671670854; -0.0008950116015354408 -0.00015317157138851518 0.004464734210440708; -0.0019607037074129887 0.0031468469367218763 -0.0030318780952586655; -0.007050832456289248 0.0029859913385736807 0.0010229301093829944; 0.00027935054778924825 -3.4431290077954735e-5 -0.0010062441026700056; 0.00395214529509437 -0.00023529941702122204 -0.008948747918483418; 0.0016177982470324188 0.006622191208513514 -0.009356047704624565; -1.777510973605535e-5 0.0002152674852928838 -0.001421582423847557] %

Mass Used: 80.38102909243207 kg
Launch C3: 98.00876265400252 km²/s²
||V∞_in||: 9.529213069396678e-5 km/s