23 lines
1.9 KiB
Plaintext
23 lines
1.9 KiB
Plaintext
archive/ES_0.7147336424301873---------------------------
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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: 2023-04-29T00:10:18.497
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Launch V∞: [6.279563498878469, -7.443238645346673, -0.12881030889281234] km/s
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Phase 1:
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Planet: Saturn
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V∞_in: [1.2815208513685269e-9, -1.8361212833781008e-9, -1.275883969519786e-9] km/s
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V∞_out: [1.1974870133089178e-10, -2.5382337079149974e-10, 3.849807893100264e-10] km/s
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time of flight: 1.8118670857980534e8 seconds
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arrival date: 2029-01-24T01:48:46.497
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thrust profile: [0.4641603227265268 -0.1451139413801847 -0.13930324834385283; 0.019898611878432376 0.001595833025431568 -0.05086849626943207; 0.05125363780689901 0.02828299961731172 0.003324998383651967; 0.0546190692943736 0.004840268156027203 -0.12250280228174079; 0.06067352712145431 0.012126171408888789 -0.23250664608568147; 0.027966479779706302 -0.0008639868844048139 -0.15034950351544824; 0.02424385721000459 0.013312535908830669 -0.07189621807546631; -0.02792939886507178 0.06860743744593205 -0.014383288672201837; 0.006023570961345908 0.0002061886510303292 -0.0833876183369962; -0.03417306929864722 -0.09803525591142527 -0.087253845482051; 0.02374029728733915 0.03505478896203923 -0.004939906763706561; 0.03682186926504505 0.11084622578322027 -0.04297782800209732; -0.0395281290516324 0.06066711185006937 0.041726205336622545; -0.01494915038075974 -0.08797974862292153 0.00772672557391145; 0.22276983125857203 0.05600787688150215 -0.0648943371726816; 0.09172025535030218 0.08278897156367207 0.03130251549450451; 0.062251824545085085 0.3211761141977274 -0.028713879115260008; 0.2674197802380159 -0.24448246942897955 -0.08996902335980764; 0.39021851898909415 0.03740274032651875 0.2412607393689995; -0.45452022857233165 -0.005616125864269111 -0.2122056286585054] %
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Mass Used: 280.55659988026673 kg
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Launch C3: 94.85131136370603 km²/s²
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||V∞_in||: 2.5771140765290004e-9 km/s
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