archive/ES_0.5701302003149444---------------------------

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: 2024-05-05T18:10:39.722
Launch V∞: [7.521062977666012, -5.469101231519245, 0.3608045644359459] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-0.00042005498109760355, 0.0025900121462541672, 0.0031515332773739265] km/s
	V∞_out: [-0.0014277988730993945, 0.0012143284573646429, -0.0036458613867303316] km/s
	time of flight: 1.8749577787336463e8 seconds
	arrival date: 2030-04-14T20:20:16.722
	thrust profile: [1.0 0.009328366434935589 -0.2145534051693982; 0.3609187007273937 0.2436352900273366 -0.26480143128612466; 0.15869217063608723 0.18197067407261372 -0.22041223423785164; 0.03829591716219964 0.06165656658769647 -0.08604500093737867; 0.010363987546646277 0.022176427287658052 -0.03632334103061475; 0.003399698707641402 0.008926516260412043 -0.016561586631157817; 0.004213306036915499 0.01431096705836324 -0.026778280110861342; 0.0015543396243992889 0.007563379924324729 -0.0162570914241487; 0.0004486633521697214 0.0024021981305425094 -0.005309579231307329; -0.0003696416341007541 0.004360849063871465 -0.009804278530060035; 0.0005119938204589058 0.004995259783286999 -0.012315127718651099; -0.0008659775939126617 -6.039209556330492e-5 -0.001050249720615347; -0.0007946008216078676 0.000935008392495085 -1.1643221210253223e-5; -0.00021965876640491112 -0.0006279827787490026 -0.002067041710469554; 0.0009971025908772635 0.0004616145559535385 -0.0013755536772578744; 0.00475179201477 0.003327379546564462 0.002202533765718288; -0.003032943352148109 -0.0007550847146290051 0.0013664793953570972; -0.0004601820582979227 0.000373930976837687 -0.0023291807783267786; -0.0007362462513186445 -0.0007756735251651629 -0.0007421245639308325; -0.004585185414577144 0.006843580117465709 0.0037389325044388253] %

Mass Used: 159.94068728544335 kg
Launch C3: 86.60763652834146 km²/s²
||V∞_in||: 0.004100825661166818 km/s