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archive/ES_0.5669769926901171
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archive/ES_0.5669769926901171---------------------------
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Spacecraft: mySat
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dry_mass: 200.0 kg
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specific impulse: 3200.0 kg/s
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max_thrust: 0.00025 kN
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num_thrusters: 1
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duty_cycle: 1.0
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Launch Mass: 3500.0 kg
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Launch Date: 2023-05-02T01:42:20.789
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Launch V∞: [6.595798636599028, -7.397144432090494, 0.03572214931100197] km/s
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Phase 1:
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Planet: Saturn
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V∞_in: [-3.537230983022231e-5, -9.075326720559897e-6, 1.5924710070306108e-7] km/s
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V∞_out: [7.143342882467819e-6, -1.5656135708308514e-7, -3.574249853556275e-5] km/s
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time of flight: 1.8749577786520475e8 seconds
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arrival date: 2029-04-10T03:51:57.789
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thrust profile: [0.20411038745388677 -0.05098539949213173 -0.0756557772555091; 0.05784574076496233 0.014331125865577027 -0.06601513057217796; 0.04674156970370141 0.022512309126944578 -0.08913960675010589; 0.048096068251937726 0.032414839194856375 -0.128342398574254; 0.0339402713383258 0.02693945580957217 -0.11601011838295446; 0.02540801207243859 0.022800920479226817 -0.10632173127692911; 0.01581636272503195 0.016554616452715804 -0.07867142405179514; 0.008445179409669983 0.01093542636124833 -0.06638494602615716; 0.006889625728960032 0.006637613387544257 -0.04351390881208038; 0.010412307026857637 0.01566995417226142 -0.07477166326030135; 0.003385001154130638 0.004143849668354118 -0.015013507114477511; 0.0019879150478651396 0.006964567438320016 -0.002969422557538971; -0.0016732400733475987 0.0030424718308473334 -0.007787680182639858; 0.002747994670420028 -0.003957363463891221 -0.007782969891523138; 0.0014875188494075909 0.000936545443220641 -0.0004468605945149545; 0.0009883636195916205 0.016093583498704045 -0.020653393214226864; 0.0017760734133095844 0.0006459923116129956 -0.006696962697694493; -0.012439291639991742 0.0013745068631110112 0.005656111027574608; 3.4629887211981965e-5 0.0017917264416819807 -0.007893214106924059; 0.016951736030142515 0.010442824607070507 -0.013004021278721389] %
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Mass Used: 88.50226619676778 kg
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Launch C3: 98.22358147572038 km²/s²
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||V∞_in||: 3.651831345296812e-5 km/s
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