archive/ES_0.5624770444150198---------------------------

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: 2023-05-01T04:14:17.974
Launch V∞: [6.505377313828419, -7.375778090388343, 0.18620660897509694] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-1.9239329840975577e-5, -2.8305316002230192e-6, 4.9630728465172736e-8] km/s
	V∞_out: [3.7247482984060673e-6, -8.40649408503162e-8, -1.9085245778104873e-5] km/s
	time of flight: 1.8749577787490153e8 seconds
	arrival date: 2029-04-09T06:23:54.974
	thrust profile: [0.25385666204160545 -0.06269763985892908 -0.08608780638886614; 0.1405791353108641 0.0367793351859259 -0.14352550880055048; 0.07335820893864742 0.03770829797376431 -0.12964949277167173; 0.047907188619815834 0.032783450508983354 -0.12021266827381259; 0.03850131395372804 0.032866496453332825 -0.1246727029903094; 0.026663534486245356 0.024789301870509706 -0.10334457869774519; 0.015261862116982309 0.016849723284038203 -0.07436841141549545; 0.008086008749655081 0.00926670749852496 -0.045184302860820494; 0.0013666594009747392 0.0016037495072631443 -0.009024825064512434; 0.006980729285886089 0.0093417698309214 -0.04781654103164112; 0.0007980980117649344 0.0006548152729008653 -0.0038218510047591694; -3.2367920274919905e-5 0.0006132412276146858 -0.004000606336212768; 0.00019988485577649535 0.0004948524803658288 -0.004060082744678712; -0.0005841186213519629 0.0026318373892078965 -0.0016664566965577023; -0.0021330272404725937 0.0031566832855406636 -0.0030747463355029325; 0.0015625570758160648 -0.0015411195322179965 -0.004304432862540517; 0.0023749853897160576 0.0009970544444068109 -0.0015083135350562062; 0.0006993221491002269 -0.0020076497997356803 -0.0015099364399851994; 0.00037773052674642377 -0.0003104405094289829 -0.0006543421520914491; -0.00013878434670003753 0.001131571272966187 0.004254974715275768] %

Mass Used: 91.8090806958021 kg
Launch C3: 96.75670933515218 km²/s²
||V∞_in||: 1.944649544465332e-5 km/s