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thesis/archive/ES_0.5714720332383227
2022-04-18 10:59:25 -06:00

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archive/ES_0.5714720332383227---------------------------
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: 2024-05-23T00:08:48.199
Launch V∞: [8.022422430080818, -6.343467455119923, -0.1228051136004346] km/s
Phase 1:
Planet: Saturn
V∞_in: [-2.106536685347406e-7, 7.972589047465384e-7, 2.161390264506476e-6] km/s
V∞_out: [2.071787112482341e-6, 2.444560465981093e-7, -1.0032924242926967e-6] km/s
time of flight: 1.8539238720351958e8 seconds
arrival date: 2030-04-07T18:01:55.199
thrust profile: [0.009750151514058303 -0.0016918588799306085 -0.004991884037067994; 0.009659406220149032 0.0007787639147808585 -0.01662838358358368; 0.032364143748465427 0.0014559325360365826 -0.09467788437041735; 0.03237321962081594 -0.0009384662903693546 -0.1263348511477777; 0.027376889242380423 -0.003320345218215699 -0.12829370066831658; 0.01948138151235636 -0.004203409058461484 -0.10356299316415267; 0.01940482143815872 -0.005916201669607517 -0.11155860021286403; 0.01271210285591663 -0.004010926252729063 -0.07705824560056405; 0.00860789035247183 -0.003251692093099895 -0.05400686184892776; 0.0013364408076164626 -0.0005908831068226558 -0.010723524959602257; 0.00011848348135017067 -0.00014615511572906405 -0.0011677595562350695; 0.0006757848039278527 -0.0003570516998136419 -0.004643788696811756; -3.431375313114123e-5 -0.00014208072204028064 -0.0004180382442350999; 7.08109312570941e-5 -7.013914039233411e-5 -0.00047304708984883994; -0.0002141372993486717 -0.00018823926698436673 -0.000771147227961132; -4.258056685458702e-5 -0.00031293185532423154 -0.0009368781847502147; -6.482937563023864e-6 7.521245147936774e-5 -0.00011069183707517632; -0.00011164528546055592 0.0009263498981100186 -0.0003028714843557967; -5.983258998017052e-5 -0.00019509578809814192 0.00020512828659342516; -0.00016978280441769006 -5.670442606750694e-5 -0.00011490618087706345] %
Mass Used: 56.469493213633996 kg
Launch C3: 104.61392209675586 km²/s²
||V∞_in||: 2.3133535408078396e-6 km/s