archive/ES_0.565812411562571---------------------------

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: 2023-05-02T04:30:50.978
Launch V∞: [6.452548119927482, -7.583826683967991, 0.08660530007934021] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-3.7498556992719035e-8, 5.940798320322717e-8, 4.072071491612141e-8] km/s
	V∞_out: [-2.0239275735947533e-8, 4.122277277722133e-8, -6.736597439697562e-8] km/s
	time of flight: 1.8180770227802536e8 seconds
	arrival date: 2029-02-03T10:39:12.978
	thrust profile: [0.14282535146509215 -0.05082683175829674 -0.060005349672201946; 0.042392653850797844 0.004513910644086575 -0.05355690983107503; 0.049963591830211124 0.013639527958031326 -0.10648588259023883; 0.0547029982744765 0.01974542034904127 -0.16158698112234057; 0.047102856461397634 0.019598843422306205 -0.17575434225098419; 0.03387215530349658 0.015368023176494404 -0.15136442689467874; 0.020194386878306533 0.009663501097211438 -0.10424605116997802; 0.010231022238721587 0.004740735229941442 -0.0587084682995996; 0.0028257416318729486 0.0029787478916892592 -0.02487808790951806; 0.001080426357557873 0.0016669605463232628 -0.00740556596415788; 0.0031774841488209737 -0.0027121476476436313 -0.00634016491346534; -0.0020263456489445454 0.0032000114637497105 -0.0005687253910285155; 0.0014642393589394359 -1.1393077074672658e-5 -0.007737063013592957; 0.003472464496284888 -0.0038681248904882735 0.000368610543330883; -0.001333844909849467 -0.000213279931183635 -0.004007373247031114; 0.00039335901760885613 -0.0007664371802637335 0.010884382982369576; 0.00018091202000989758 -0.0018500721046066412 -0.002421319631897709; 0.0018477076738220742 -0.000997974239458597 0.005235485954811098; 0.00438826592810179 -0.0026366847349900573 0.001350090829129274; -0.0007863457211818143 -0.008869590689439412 0.012134038842052186] %

Mass Used: 81.69686829539523 kg
Launch C3: 99.15730489044645 km²/s²
||V∞_in||: 8.120115065743312e-8 km/s