archive/ES_0.5716910814024115---------------------------

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: 2023-05-01T00:46:40.297
Launch V∞: [6.340419807569118, -7.414760986266031, 0.22382923934612609] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-0.024030921770962825, -0.0003903872875998755, 0.02056097449582832] km/s
	V∞_out: [-0.031016408947115486, 0.00023014951681816484, 0.006150941134414483] km/s
	time of flight: 1.874957778728931e8 seconds
	arrival date: 2029-04-09T02:56:17.297
	thrust profile: [0.36854535738034194 -0.08317664873658107 -0.11792807319111911; 0.1369098339529802 0.0431321531983949 -0.1348553112482777; 0.09403939637560474 0.05549341482170255 -0.15685845403978985; 0.03741520957173225 0.02999665127322615 -0.09414320341171732; 0.044730457405323186 0.04383740769386602 -0.14060126366229758; 0.02374304804683809 0.028765629080636783 -0.09815209286251955; 0.010453338353606512 0.013330947161333456 -0.05044206201805312; 0.01237443557940563 0.01713157572716763 -0.06130065330818299; 0.008978436232238676 0.014444780999589563 -0.05568962026772533; 0.004125759083326639 0.0026020573983937915 -0.012424983273398645; -0.0018749177358854444 0.006650176526520822 -0.00380147233935048; -0.0015320027962743752 -0.0020531167289194207 0.0003010049936392118; 0.002092216211540164 0.0024536631547604796 0.004039680742412759; 0.0001727504270750756 0.0011505842554918513 -0.0033679529384890773; 0.003918102324080887 -0.012628375193681561 0.004195606510771098; -0.014520611479282481 0.014128228282054841 0.010978380702749282; -0.008399349742260013 0.004391205240183396 0.009788088510659567; -0.003409446507569495 -0.0016718508583082054 0.015930923186052298; -0.00039372819429403516 0.013657735901152723 -0.02973535679156292; 0.010099161532359457 -0.03388795981589754 0.007251891180277546] %

Mass Used: 111.46632543916576 kg
Launch C3: 95.22970334805389 km²/s²
||V∞_in||: 0.0316289626073091 km/s