archive/ES_0.5612450710214788---------------------------

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: 2024-05-15T11:40:41.648
Launch V∞: [8.021909703077354, -5.749151157124916, 0.11902775093900021] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [1.3316682097336525e-5, -0.0010029826523570576, -1.6561290482246377e-5] km/s
	V∞_out: [-0.0009667817282817482, 0.00014861606757605157, -0.0002216379055435342] km/s
	time of flight: 1.8749577787363833e8 seconds
	arrival date: 2030-04-24T13:50:18.648
	thrust profile: [0.25898531295065824 -0.00040690788571314364 -0.08896190851570146; 0.08135582119724258 0.04577799421254492 -0.09866815612569588; 0.047493770915380595 0.042511322543608315 -0.10515002442165951; 0.0462783567246968 0.054219841566489825 -0.14915519421386064; 0.022333510722506146 0.0313708144696423 -0.09978175634840003; 0.011358868559776619 0.01844052870025684 -0.06546816391541554; 0.007141857739476762 0.013471605960071121 -0.05400046037034536; 0.003928021619223811 0.011738555456816197 -0.03964312200838907; 0.0024333104079123317 0.006316481961933044 -0.03157875973538905; 0.003538727865920152 0.009324637793772227 -0.045378666913846386; 0.0014782979455162284 0.0024539947929646177 -0.009862640269862888; 0.00033347322992988604 0.0021792535753370782 -0.013858673149924158; -0.0004670299324331761 -0.00121886043940949 -0.0008905378306694398; -0.005921292157185904 -0.0036544651990440425 -0.005163985591909229; 0.00044397176555433676 -0.004167114433582173 0.005045310230716602; 0.017115788027416964 0.009210518313671992 -0.006188484553223383; -0.003431487903855754 -0.0009323367699462815 -0.004157301541212065; -0.0008328726348185562 0.0005077556019957499 0.008159394452316171; 0.012464408286538768 -0.0031460884291330217 0.003024551585243364; -0.010234932971081252 -0.0039636952289608665 0.01688539310188163] %

Mass Used: 86.51458834086134 kg
Launch C3: 97.41794191729096 km²/s²
||V∞_in||: 0.0010032077607822405 km/s