archive/EV_2021-10-14T13:09:46.191/mission---------------------------

Spacecraft: mySat
	dry_mass: 2000.0 kg
	specific impulse: 3200.0 kg/s
	max_thrust: 0.0005 kN
	num_thrusters: 2
	duty_cycle: 1.0
Launch Mass: 4000.0 kg
Launch Date: 2022-08-27T18:20:28.271
Launch V∞: [4.976680389443524, -1.705424182457512, -0.3485682941979716] km/s
Phase 1:
	Planet: Venus
	V∞_in: [4.210457531789055, 0.3638419019608806, 2.167260083943969] km/s
	V∞_out: [-0.02718879860259023, 0.00013680384875937985, -0.40279343753838176] km/s
	time of flight: 2.616182260016269e7 seconds
	arrival date: 2023-06-26T13:30:50.271
	thrust profile: [0.1081478833164793 -0.04747352000316829 0.009803784528203987; 0.11190267398595631 -0.08489441529847341 -0.007286984410559111; 0.12911430752493627 -0.11099328002003525 -0.01943723546946303; 0.16688603565301258 -0.12840027043968893 -0.02332008672269124; 0.21714048180407453 -0.1362382567528611 -0.02567076757100798; 0.2764401329174762 -0.13402041782174592 -0.0287511421326799; 0.33266188746520187 -0.11957670801586273 -0.031093308044346353; 0.3820659935956181 -0.09253553276581379 -0.031479580308358644; 0.41374954552181137 -0.05951601425001449 -0.03348539939450036; 0.4271557515022211 -0.02469794622072092 -0.03284633186694413; 0.4196852691041662 0.011180284532007942 -0.03287929676767141; 0.39104446127168524 0.05467052960463492 -0.03128098668740266; 0.3397344905954879 0.11008642002736206 -0.024504191585152588; 0.2681377457360699 0.17570003550101684 -0.016577172053069123; 0.046833731659678475 0.23938547094636797 0.008263855085563338; 0.20692889271962633 0.2635523571087766 0.020761614548693325; 0.13667494276947326 0.28012067330618706 0.033686527674503336; -0.11957290103408791 0.269968116350337 0.04482701107136116; -0.16727049842201927 0.21796253025589696 0.0361909665435463; -0.21921062997276963 0.1091389154173985 0.005030961855685549] %

Mass Used: 250.70235015664184 kg
Launch C3: 27.797319196502702 km²/s²
||V∞_in||: 4.749457845699708 km/s