archive/ES_0.5634737479917851---------------------------

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: 2024-05-08T16:24:33.089
Launch V∞: [7.516116281104868, -5.677180637424939, 0.011623335906044597] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-6.976040731436137e-5, -5.7101480365928066e-5, -4.6082886311387174e-5] km/s
	V∞_out: [-9.424057654872186e-6, 6.327621239534564e-5, -7.835498184248351e-5] km/s
	time of flight: 1.8559386178030565e8 seconds
	arrival date: 2030-03-26T18:15:34.089
	thrust profile: [0.7970246800619629 0.006405897370524198 -0.18290695805922427; 0.3024278931208139 0.19996384978017673 -0.2428744049844204; 0.08806715282042253 0.09963099097131305 -0.13823818431629514; 0.052728256272246934 0.08294089225950849 -0.1292096803928654; 0.020169717638571602 0.041272081533940075 -0.07230584650915169; 0.0073344543988018715 0.01844635607605562 -0.03481069574209994; 0.00971776174561734 0.03136655229312888 -0.06212249411429959; 0.0022982345291728927 0.009102723153605599 -0.018611672814698228; 0.002298692855587313 0.00967623244921392 -0.021488706887694293; 0.0001738168369804971 0.002104484364524093 -0.005224741834583149; 0.0003555691194930353 0.002416556193033709 -0.0047251982432117935; -0.00036229822403916406 0.0006255330504038887 -0.0018532250967384784; -0.001029980286646927 0.0022454988237743637 -0.0017791729645115757; 0.00625302983960176 0.003027839689260705 -0.006401012163385134; 0.0005693187452227849 -0.002165304191859626 -0.004938744960253658; 0.0005713839690488484 -0.0003487011424227898 -0.0015966659539699518; 0.0013274682603587017 0.0057121357033033514 -0.0034210442612303523; 0.0001427137644261708 -0.0010422542733604812 -0.0010130875485081805; 0.00037253917895636597 0.0008569402929175474 0.0012286008016782809; -0.0008213238866218919 -0.0005483441515920385 0.0001107714913980689] %

Mass Used: 139.83801157303333 kg
Launch C3: 88.72251904297988 km²/s²
||V∞_in||: 0.0001012458685548912 km/s