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thesis/archive/ES_0.5609203029886916
2022-04-18 10:59:25 -06:00

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archive/ES_0.5609203029886916---------------------------
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: 2024-05-15T18:37:53.376
Launch V∞: [8.245736520954294, -5.535834027237761, 0.3488872737079204] km/s
Phase 1:
Planet: Saturn
V∞_in: [1.7764188758842281e-7, 1.1075367743652694e-6, -2.672810444827693e-5] km/s
V∞_out: [-3.2159577296369163e-6, 2.6540393633199458e-5, -3.2658194015875843e-7] km/s
time of flight: 1.8519900936264795e8 seconds
arrival date: 2030-03-29T06:48:02.376
thrust profile: [0.2845344378589719 -0.09022676202443282 -0.12471390151070887; 0.021797190381411813 0.0013221254733468764 -0.033296509126960284; 0.01576052190631502 -0.0012131732472497646 -0.046271443802678246; 0.02341772008618174 -0.007010502966442249 -0.09546330488001195; 0.029010371198511773 -0.013932183003397854 -0.14251674262485808; 0.022515859590458365 -0.012828073362709956 -0.12357337488296155; 0.01977634149520766 -0.012422689915795006 -0.11754606293105616; 0.012484411586394158 -0.0076455633248900656 -0.07720437901318448; 0.006236704143860163 -0.0034246290541526106 -0.03919903557669422; 0.0019205251737865578 0.0017089149826678058 -0.005944729986257445; -4.3639312071254194e-5 0.00043357476959866577 -0.0017162722969883814; 0.0014970439109932734 -0.0005372028850054038 -0.002230300213744207; -0.0005841653183019588 0.00013149955968928774 -0.0023328327667457337; 0.00014649952468044234 -0.00023862992033460423 -0.0010753847824058627; -0.0004939282174850165 -0.0027421303378811317 -0.0011793547289693802; -0.0006802385133753476 -0.001715463612475723 0.0016056380184219965; -0.003452722966729563 -0.003017402460567966 0.002112559267365016; -0.0021224374299200453 -0.0073786116690116275 -0.0026251801085191676; -0.001207429419171608 0.0005507481821830358 0.0045792914118976645; -0.001292904676287655 0.0016299141209683518 0.0015923724308080202] %
Mass Used: 78.3108031875172 kg
Launch C3: 98.7593514798782 km²/s²
||V∞_in||: 2.6751631010927136e-5 km/s