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thesis/archive/non_saturn/EN_2021-10-14T22:19:11.393/mission

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archive/EN_2021-10-14T22:19:11.393/mission---------------------------
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: 2500.0 kg
Launch Date: 2022-04-16T10:37:51.889
Launch V∞: [9.93430356594082, -9.814231711705617, -9.723022803164637] km/s
Phase 1:
Planet: Neptune
V∞_in: [-3.330351073892173, -5.42324969269204, 0.08855958401956425] km/s
V∞_out: [-3.300747312670549, -3.328777757532345, 3.3127008443655095] km/s
time of flight: 1.007092354462312e8 seconds
arrival date: 2025-06-25T01:25:06.889
thrust profile: [0.8753926904953222 0.6832826274506226 -0.12190291359862054; 0.8755956380471712 0.6667237002096869 -0.1464038516358984; 0.8745742225785343 0.5149107423186586 -0.17002603241860648; 0.8637408209307073 0.25941037509054327 -0.19687061798657313; 0.8873044529895101 -0.013949833656543549 -0.20801896083211308; 0.8603140096952885 -0.22178564312493226 -0.21226327319113722; 0.8722049558724008 -0.35639346957623513 -0.20814872623709274; 0.8798839779340266 -0.4459725813099044 -0.2408854578792029; 0.8297808636995301 -0.4620621965066881 -0.1882977763047611; 0.860562943045671 -0.48184951051800107 -0.19082816411413117; 0.8605004943271973 -0.44955972119045773 -0.19270354692519773; 0.8747678471057356 -0.47094234663449625 -0.19348022139751583; 0.8729759234509828 -0.47846767255653266 -0.1955394172393871; 0.8588899256657108 -0.4743430479827928 -0.18332350007377493; 0.8588081308592396 -0.46834855863482244 -0.18530291711509578; 0.9286451187684647 -0.4728485531364328 -0.24687867162402924; 0.8722317541853327 -0.472450161676079 -0.21522005038654823; 0.8290733251430757 0.6523310686037682 -0.0183400190880806; 0.8629624567917368 0.9173769916931223 -0.01773284000590214; 0.8426122479515165 0.860803708329764 -0.020651982695331434] %
Mass Used: 825.0187357617949 kg
Launch C3: 289.5467038621722 km²/s²
||V∞_in||: 6.364803084509432 km/s