archive/ES_0.5573582314784152---------------------------

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: 2024-05-14T12:06:56.511
Launch V∞: [8.047913388637948, -5.649540251258871, 0.16746191985934528] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [8.120921028703875e-7, -7.448714584366031e-6, 1.3307527431501173e-6] km/s
	V∞_out: [-1.181192309855768e-6, 4.383804501753365e-6, 6.107979109499203e-6] km/s
	time of flight: 1.8749577787493584e8 seconds
	arrival date: 2030-04-23T14:16:33.511
	thrust profile: [0.3212323180965184 -0.0072494604662601495 -0.10667691405523096; 0.08936944777692282 0.04799474938124221 -0.10667649340323808; 0.04169948331916683 0.03652185269887154 -0.09184705512522744; 0.03067270047133568 0.035988031086508734 -0.10617058270132451; 0.021632857331026562 0.02921284377528113 -0.0940529329629678; 0.017924941651634427 0.02780222611660501 -0.10067603775304786; 0.013373568993756938 0.024836335957386924 -0.09587211490535821; 0.003983371326425269 0.008474480710221303 -0.03425989450895714; 0.003086517405664589 0.00707520541202714 -0.03171509525655946; 0.002420610808737147 0.004303701940928045 -0.02264655781163144; 0.0004919214204796523 0.001083223383296344 -0.0078138477864468; 0.0014021935537828231 0.0015922091035263143 -0.0033917473044053044; -0.0018805473773238315 -0.000958675756830112 -0.0008657087761377453; 0.0005323440194236278 -0.0030339582985456906 0.00017502315506135076; -0.0016239442861260642 0.005125132829713471 -0.0015477600159380736; 0.0005721116679907841 -0.0008036246142245607 -0.004401338348149955; -0.001523037921603625 -0.0021817435140161386 0.0013010471986086704; 5.6874767379083994e-5 -0.004354458699101221 -0.004273820011076563; -0.005129787459767908 0.0031552682462866444 -0.0025309250216649357; -0.00037057206470209004 -0.0007003742367315295 -0.0026007934831861748] %

Mass Used: 86.08476239689662 kg
Launch C3: 96.71425845621506 km²/s²
||V∞_in||: 7.610108107398555e-6 km/s