archive/EN_2021-10-14T21:24:00.053/mission---------------------------

Spacecraft: mySat
	dry_mass: 200.0 kg
	specific impulse: 3200.0 kg/s
	max_thrust: 0.0005 kN
	num_thrusters: 2
	duty_cycle: 1.0
Launch Mass: 2500.0 kg
Launch Date: 2022-08-05T13:09:42.428
Launch V∞: [7.8646219457877775, 5.391423246731976, 0.21664193585734026] km/s
Phase 1:
	Planet: Neptune
	V∞_in: [4.3825277514495635, 0.4972219444711066, -0.033282491583832376] km/s
	V∞_out: [1.2613145775799692, 1.2541088206742887, 1.19448213244607] km/s
	time of flight: 7.239210268385214e7 seconds
	arrival date: 2024-11-20T10:04:44.428
	thrust profile: [0.5570971125040689 0.46523336275569166 0.24443397992833363; 0.5455353078277998 0.37771233171043145 -0.2905042836424388; 0.5373067044309571 -0.3697335845815613 -0.23280971000434258; 0.5789141430780081 -0.4290239526125613 0.17533812742230417; 0.6282895761794832 -0.4760003782283056 -0.02869288371312378; 0.5937505020656196 -0.44907996753558815 0.008871484612811375; 0.583505825104241 -0.4419058605742258 0.0024181680115527163; 0.5999629018966298 -0.4488350427074705 -0.0010636832749702108; 0.6282809657618084 -0.4727189600895791 -0.0029164733714258264; 0.6387620784811242 -0.4812400030251487 -0.004086578863408878; 0.6291065200722094 -0.4782777977932136 -0.004926811268235369; 0.6685784074664406 -0.5147308829624088 -0.005566898376192713; 0.6402182196889159 -0.4886680265057143 -0.005534056457267186; 0.7138116778721744 -0.5642610603445648 -0.006396711596120154; 0.6435783521271209 -0.5330961196095906 -0.005999671526644724; 0.596620975387932 -0.5192282791418487 -0.005575460237394601; 0.5813910956156 -0.5172814194247172 -0.00522147564686555; 0.6107615648872227 -0.524352387609911 -0.0051458063628017055; 0.6046402368385538 -0.4209917190545011 -0.005257320993026065; -0.23129745811295646 -0.24034385286604382 0.002372195721427373] %

Mass Used: 1747.3636846345928 kg
Launch C3: 90.9666567039407 km²/s²
||V∞_in||: 4.4107694202412375 km/s