archive/ES_0.5629660880627777---------------------------

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: 2023-05-02T22:38:15.928
Launch V∞: [6.506268356737844, -7.565059091807201, -0.031182876024331094] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-0.012773277769634123, -0.00035591092256944166, 0.00897581924612454] km/s
	V∞_out: [-0.015041803124011335, 0.0001432758290515128, 0.004188692357808605] km/s
	time of flight: 1.8568220545820457e8 seconds
	arrival date: 2029-03-21T01:01:40.928
	thrust profile: [0.10051407537799785 -0.024035715269606572 -0.03824783703779798; 0.04282066778172882 0.011700353156600854 -0.04720948130625767; 0.052059921645881434 0.028658196587636707 -0.09566548188098743; 0.03204429160436005 0.023602022266838454 -0.08466980781819125; 0.03757217281569341 0.03268304453900067 -0.12347794981861256; 0.02720274812185457 0.026796236480690332 -0.10125342735315859; 0.0331477775167375 0.03467486561588758 -0.14156598900963235; 0.024650211740205655 0.02993123585262709 -0.1268035895077981; 0.00896159685921584 0.012407119714873542 -0.05710291428466869; 0.0021087286229188023 0.003179451144124972 -0.01557353461406365; 0.00037779571742631334 0.0007039635789010311 -0.003370905602933389; 0.00498312512336695 0.00805709753933532 -0.04231088015518839; 0.00015824408476105165 3.22480316526213e-6 -0.00013229761143941044; 8.839271642280017e-5 0.00010985196237532974 -0.00021301764682538923; 0.00015947364304880513 -0.00012768185858099768 1.6683334577841563e-5; -7.902130022515856e-5 0.00012427528996659463 -2.3489847683083685e-5; -9.104980763844755e-5 -0.00012641955620704574 -3.2962467467237446e-5; 3.194617468948428e-5 -0.0001530113342663748 -3.508299645934135e-5; -2.6759314288825927e-5 1.3748404294586298e-5 -2.8141040274752663e-5; 7.838395215076861e-5 7.509963975638275e-5 0.000286464616625001] %

Mass Used: 76.01182311552338 kg
Launch C3: 99.56261936418011 km²/s²
||V∞_in||: 0.015615653323000394 km/s