archive/ES_0.5755064745441583---------------------------

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: 2024-05-22T17:44:00.034
Launch V∞: [7.632789889383906, -6.469594063924877, -0.41814865261009626] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [1.1983230978685446e-9, -7.747299608050722e-9, -5.025125633825494e-9] km/s
	V∞_out: [-3.87821762142259e-9, 3.2093361149681488e-9, 2.014314658303085e-9] km/s
	time of flight: 1.874957777799855e8 seconds
	arrival date: 2030-05-01T19:53:37.034
	thrust profile: [0.4129737980071394 0.012856265999300556 -0.16573031709954397; 0.035210645269817105 0.01521469322009352 -0.049102843972277696; 0.02483052894162927 0.01641640389819381 -0.060673709434411034; 0.022719612415422103 0.01820037495741089 -0.08044891125479026; 0.029935334658666605 0.03024599478995793 -0.14403328787416667; 0.017144932497854107 0.017006624324834668 -0.09768680498984497; 0.010533950370820562 0.010530743832777677 -0.06645651520184517; 0.011286193750988813 0.011608264742410994 -0.0812836516591285; 0.00557550214390478 0.006032760690785981 -0.03795679043365469; 0.00064617540820556 0.0008477409924186842 -0.0052978399286904825; -0.00010847233754369447 0.0001594729922737158 -0.0022143308196076053; 0.0006820162997259386 -0.00014959850458481395 -0.0039649565474668014; 3.664662112385763e-8 0.0019113021574521153 -0.003661865560711952; 0.00017957171894073757 -0.0001512784190217224 -0.001420299379233176; -0.0005290991749705048 0.0002955372997864057 -0.00182279411681399; 0.004928066631963563 -0.003945486044002183 -0.0025484597419682484; -0.0010973682684754006 -0.00010027000754273506 -0.012265798534779318; -0.0035527769347811246 -0.0025605360968915507 -0.0018115018034840528; 0.003954864036044642 -0.002921611170328418 -0.006979236185149979; 7.530644861997399e-5 -0.0012598292070940746 -0.004271166360658132] %

Mass Used: 86.39935363324321 kg
Launch C3: 100.28997714313282 km²/s²
||V∞_in||: 9.31174082003565e-9 km/s