archive/ES_0.6683648672952885---------------------------

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: 2023-04-25T19:59:59.373
Launch V∞: [5.988296626448164, -8.975142897232814, -2.4246670666064882] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-0.0019228430134693995, 0.0009694589815097379, 0.0020045098662270847] km/s
	V∞_out: [-0.0009242893519641091, 0.0019727501618984895, -0.0019769836712157226] km/s
	time of flight: 9.589292991855013e7 seconds
	arrival date: 2026-05-09T16:55:28.373
	thrust profile: [0.4868186217595121 -0.398685880883744 -0.2753263644221887; 0.31514503303165786 -0.09043377438234629 -0.2660848471221104; 0.09956096762161003 -0.00942522106024 -0.12506508585417417; 0.027630187940019653 0.001587501234550543 -0.04384855386065674; 0.021888515834866718 0.0025911758731942914 -0.040158684751002004; 0.02201065651529536 0.0036538524334563637 -0.04112827919991203; 0.01839973779874327 0.005136490435910041 -0.03903497074333639; 0.08546903488518931 0.01117961409953839 -0.17516842000615662; 0.0031642350995992265 0.001439861634123095 -0.008362333378969208; 0.002672794695790305 0.0018692938221789464 -0.0063728367133893404; 0.0002031102059233213 0.0004626319549466848 0.0002736724350381328; -0.000600974254300764 -0.0008852578898481578 -0.0014250452737733512; -0.0010964228941604036 -0.0005898192262435279 0.001892218450521413; 0.008203955075616626 -0.009879681563864838 -0.014136485081859508; -0.0037707074083035176 -1.846777243262841e-5 -0.002499977519119151; 0.006494058709496856 -0.006338228546652312 0.0023240401988231744; 0.009616045023570266 0.009341911972411486 -0.0027140650555370644; -4.75025950727992e-5 0.0021288202078945323 -0.0010486009010772948; 0.0039346532306314165 -0.0002308109877574799 1.989693112372569e-5; 0.0025322138681684783 -0.002601900363940292 0.011970958640298263] %

Mass Used: 66.38961328470623 kg
Launch C3: 122.29189689596521 km²/s²
||V∞_in||: 0.0029419782077846368 km/s