archive/ES_0.5629699336834778---------------------------

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: 2024-05-10T10:37:58.398
Launch V∞: [7.833128630205404, -5.600021355530694, 0.2031285298439677] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [1.8307997364367636e-6, 1.5690475512335009e-6, -1.1847526628509775e-6] km/s
	V∞_out: [3.517368169202993e-7, 2.6594329358408217e-6, -1.2399142701866943e-7] km/s
	time of flight: 1.8530596213016438e8 seconds
	arrival date: 2030-03-25T04:30:40.398
	thrust profile: [0.635361525631605 -0.002564355735813012 -0.1458217881543325; 0.09578219584304053 0.05934007382724478 -0.09278148231218128; 0.0566855915490099 0.060054600312552296 -0.10115058035164187; 0.03582243894499629 0.04783674717137098 -0.0915440938012398; 0.03973963190624443 0.0689988956356222 -0.14133014322294254; 0.016747659169285587 0.03793164585454499 -0.08207335076350389; 0.01593316068184302 0.04044844332416133 -0.09680645405669133; 0.0018486709313224412 0.010909178792295528 -0.03253059209578526; 0.002979898214250699 0.010954337033318126 -0.027140524263287967; 0.0005343465890430433 0.007312786752396053 -0.0074898579874240765; 0.0015625465251456081 0.0035868171988226176 -0.007624933151657527; 0.003634125429762141 -0.0010809904461431012 -0.003506730364856681; 0.0035390516400073437 0.005592712963662539 -0.005565616822858944; 0.0019121354791894337 -0.0021569463940358663 -0.0051272112080029296; -0.0033800097653181108 0.0037914565401947816 -0.010012885930369822; -0.015251911695284379 0.0043300423942942215 -0.0023078577450335383; -0.006138365206466568 0.004286409693784101 -0.0011536384241145779; -0.0016564321245489877 0.0009484603805619109 -0.0015193170289273406; -0.0016691385347483425 -0.007153883871977056 -0.0010694018082219202; 0.002933890733142097 0.022066184997148828 -0.004914144709856002] %

Mass Used: 115.70172960100763 kg
Launch C3: 92.75940451937997 km²/s²
||V∞_in||: 2.6865175906926892e-6 km/s