archive/ES_0.5585621186956828---------------------------

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: 2024-05-10T10:57:37.745
Launch V∞: [7.7113007988953415, -5.605806768462785, 0.1932706953451506] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [1.1411864102662826e-5, 9.051585126262427e-5, -0.0016679131362233827] km/s
	V∞_out: [-6.68595874944899e-5, 0.001662250780865691, -2.1548398303339808e-5] km/s
	time of flight: 1.8613596856291556e8 seconds
	arrival date: 2030-04-03T19:23:45.745
	thrust profile: [0.7402394396290365 0.007313648807831413 -0.1915042985819171; 0.16688788375067967 0.10526517728515357 -0.16298297270796833; 0.05466021418921908 0.05646644021696119 -0.1021929079782081; 0.055282482641853425 0.07831288266348123 -0.15353720657173264; 0.02237453837658505 0.03943440081479446 -0.08861616019278573; 0.01082854286905821 0.023021439915342636 -0.05703336260139691; 0.007385369873612948 0.01836471605855119 -0.0485939102651073; 0.0029104026521122543 0.009330692581304641 -0.025757820932020406; 0.004253850247424283 0.015112186644098637 -0.043977896258259284; 0.0006487829818609162 0.0026732737247633213 -0.008254833191440247; 6.257456928790427e-5 0.0002803842930589409 -0.0004002872710795796; -0.0004025601497931761 -0.00013742760390172168 -0.0009143125121511924; 3.6060942983300796e-5 -0.00042685800339301944 -0.000445919925552993; 0.0004506196092027391 0.0005666965969065017 -0.0008471816739502754; 0.00011084064029776942 0.00029059370629232396 -6.827649948367321e-5; 4.191812129374984e-5 0.00016953221944507497 -0.0008248951712044076; 9.732603880424325e-6 0.0003003513851289949 -0.0006944969669168055; -0.0007627268981069426 1.9847347307027296e-5 -0.000989569507108837; -0.00015049812264010808 0.000938883428826455 0.00014381419463695426; 7.672476342965084e-5 -0.00016985640738025043 0.0006356804524977268] %

Mass Used: 121.25073707290994 kg
Launch C3: 90.9265830980663 km²/s²
||V∞_in||: 0.0016704064116132382 km/s