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thesis/archive/ES_0.6370850789822546
2022-04-18 10:59:25 -06:00

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archive/ES_0.6370850789822546---------------------------
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: 2024-06-01T05:36:19.432
Launch V∞: [7.845607303341686, -7.4709544860943025, -1.4421966627838825] km/s
Phase 1:
Planet: Saturn
V∞_in: [-1.217089617555473e-9, -4.28565102692583e-10, -1.5498333888339338e-9] km/s
V∞_out: [7.191585239981749e-10, 9.091567741651445e-10, 4.0100624555242725e-11] km/s
time of flight: 1.8191171480342913e8 seconds
arrival date: 2030-03-07T16:38:13.432
thrust profile: [0.004725165075078091 -0.002638964263823945 -0.0033527002780787928; 0.0025062219880532853 -0.0028970848687393503 -0.006266633287152016; 0.007435953775488162 -0.013115896098203513 -0.02818505421286008; 0.025084237973161522 -0.051213846770530626 -0.10732600854270818; 0.03150202962987133 -0.06601001814367198 -0.13869116904350048; 0.03004634613144765 -0.06298428149784709 -0.13289841766316027; 0.019617106746253436 -0.04126964195469426 -0.08730106744861542; 0.008478166753308574 -0.01746050698011293 -0.037398827808496744; 0.003978011669088891 -0.007944670562843032 -0.017395055524321502; 0.00042648285391913874 -0.000859058251766941 -0.0018498992161519797; 0.00023041967473201193 -0.0004630226165680695 -0.0009471089330530739; 0.0003906783412044017 -0.0007071033474662298 -0.0012370747827386839; 9.667756806215725e-5 -0.0001365997683559847 -0.00040728133426610097; 0.0001224916409959056 -0.00028779492134122474 -0.000525580758235625; 0.0001333904979763674 0.00011458883083793203 -0.00018962186389368717; 0.00011506910170612028 -0.0001310102748724242 -0.00022219906442989655; -0.00018372847254694434 -0.00013154418304527302 -0.00030173694134487665; -6.323080604497442e-5 7.39737441686148e-5 7.0191340336662e-5; -2.0806814785815454e-5 0.00011253358376213894 -0.00019424406974059404; 0.0001792320252199788 -0.0003826453683732218 7.759299969640836e-5] %
Mass Used: 46.48215652946237 kg
Launch C3: 119.44864610568595 km²/s²
||V∞_in||: 2.0166702054504865e-9 km/s