archive/ES_0.565612041946955---------------------------

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: 2024-05-13T14:37:05.625
Launch V∞: [7.617199158843039, -6.077433017618617, -0.2730684578204187] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-9.503523530802447e-6, -7.560305706181158e-6, -6.083121417327273e-6] km/s
	V∞_out: [-1.3164482505137375e-6, 8.906031710869905e-6, -1.0157302513764892e-5] km/s
	time of flight: 1.8749577787426522e8 seconds
	arrival date: 2030-04-22T16:46:42.625
	thrust profile: [0.24706950103168615 0.028952331955518485 -0.0635527753737683; 0.17039580266340915 0.14187095971740973 -0.12725288634471368; 0.09796501626039038 0.13745028518650146 -0.13604932699700287; 0.06044301358716032 0.12100932820319557 -0.131053694815414; 0.04855620700060682 0.13358961588117244 -0.145721569453928; 0.019891321063688384 0.06989646217412614 -0.09298809392822475; 0.00988677255227137 0.04414218168713727 -0.06332532743178627; 0.0033752814023085094 0.018371078722019145 -0.028824920554022318; 0.000740552017796243 0.0025287781605094805 -0.004154219117901032; 0.00013993130982951782 0.004002817232767889 0.0014965302710328553; 1.3278272126567107e-5 0.0021477658156285485 -0.0019554076658864243; -0.0005069076641351061 0.0010374823775010013 -0.001831797104248573; -0.000344343645207628 -5.195472804003288e-5 -0.0010467649775648847; 0.0010795473962884547 -0.0028066679586084644 -4.9232586048195614e-5; -0.005416681359806275 0.005058682217609011 -3.0563262285001605e-5; -8.082924241758927e-5 -0.0068687843851182135 0.0006818393655584616; 0.002697499957386189 0.002300895503627223 -0.002236051076659758; -0.0010358768920165056 0.0033711450163014757 -0.002102970162336977; -0.00023182722966420702 -0.011427744714423614 -0.0015869429541363745; -0.0046380747519071145 -0.0028999995712055155 -0.00799651777337953] %

Mass Used: 105.53040690275157 kg
Launch C3: 95.03148149177646 km²/s²
||V∞_in||: 1.3582324839635405e-5 km/s