archive/ES_0.557935356926101---------------------------

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: 2024-05-13T07:49:47.377
Launch V∞: [7.945701496545313, -5.736791365601548, -0.214699504782922] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-0.010921117827720076, 0.0070861100890934935, 0.0004703216649129304] km/s
	V∞_out: [-0.009554240174272135, -0.004220757954986261, 0.0077532524086496545] km/s
	time of flight: 1.8749577787556085e8 seconds
	arrival date: 2030-04-22T09:59:24.377
	thrust profile: [0.28802164084533227 0.01431431957416294 -0.07392645803296491; 0.10082550427909272 0.06881047611718788 -0.09733165130847714; 0.07446863885762305 0.0839185500842902 -0.12900462969320547; 0.0615773298748603 0.09818853659097107 -0.16657494783858606; 0.022609135981595224 0.04519274864002445 -0.0885796139744419; 0.019048831545037673 0.04081983646918119 -0.08683074045079911; 0.010166177154171636 0.02950353117451617 -0.06956105501075896; 0.0036005969675457095 0.01359144324995046 -0.03352151572604928; 0.004469382417213494 0.020580478042397727 -0.051255759144548475; 0.0006126264259049385 0.0005130904052235036 -0.0007848742671049292; -2.3820475137712743e-5 4.986975013069196e-5 -0.0004270853604301781; 0.0007190690168191022 -0.00042516344911533514 -0.0015485689781394195; 0.0006400535881936646 0.0005468987405198359 -0.0003487174714898373; -0.0011075425078368156 -0.0022825766021131104 -7.347740235339167e-6; -8.14310247719504e-6 0.0010524772915226602 0.0009224623643710099; -0.001661803197089664 0.00022398257101700133 0.0013343934947232894; -0.0001733638219283226 -7.656243668123438e-5 -0.00024636328639355165; 0.00048037776395873626 0.0004155988340512869 -0.0009596899444138756; -0.0007135577227384529 -0.00028716351102014254 -0.00040308842225824336; 0.000580886156848781 0.002121856875814165 -0.0013750348995601215] %

Mass Used: 90.39349703546895 kg
Launch C3: 96.09104332199693 km²/s²
||V∞_in||: 0.013027086138894773 km/s