archive/ES_0.6802028794769404---------------------------

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: 2024-04-15T08:48:21.403
Launch V∞: [6.968501041069467, -5.921325083108335, 1.4549449457211217] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [1.8941181380884958e-6, -3.4022101198942264e-6, -1.3389380676361563e-5] km/s
	V∞_out: [-1.2608809819604975e-5, -1.4226614235537589e-6, 5.029457067405176e-6] km/s
	time of flight: 1.8749577787946093e8 seconds
	arrival date: 2030-03-25T10:57:58.403
	thrust profile: [1.0 -0.1658543436575036 -0.004051040335535767; 1.0 0.6166071124635462 -0.10548512527599369; 0.5167411424574556 0.5818288732779207 -0.11083689122225018; 0.20472142044042535 0.3478283008679858 -0.0754530537155473; 0.07923373216132079 0.19783156976415603 -0.04662204285317392; 0.051539858003774815 0.17288039078150652 -0.042465008924287714; 0.015631075730466324 0.06147383120307523 -0.016635188437831527; 0.006421957764711719 0.03600562129286619 -0.010370015560293426; 0.0015380796942918331 0.008123547463853702 -0.002124749304437673; 0.0022355432682422305 0.001300544084879635 0.00039400028943879653; -0.0004863440512317598 0.0007026912315716697 -0.0006720003507685819; 0.002665210560124627 0.0006236511058850206 -0.0004413365522879953; -0.0006221232252339602 0.0011072755612846893 0.0021699610696952272; 0.0011378286170341916 -0.0007157983827024833 -0.0015967740030106443; -4.720360001734527e-5 -0.0011682647826959888 0.00041769977073345536; -0.0005158283206885277 -0.00016663025483058314 -0.0005175835271408799; 0.0005477874025024115 -0.001441837263681094 3.335566952163236e-5; 0.0025552627398353505 0.0008312754216315413 -0.0017073387940209504; 1.432919170291471e-6 0.002382525575652207 -0.0023796870361217953; -0.0030798877357397334 0.0018564461930393162 -0.0003384352672052024] %

Mass Used: 293.4260793396011 kg
Launch C3: 85.73896229431361 km²/s²
||V∞_in||: 1.3944111019260817e-5 km/s