23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.6166051135886023---------------------------
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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: 2024-05-01T21:21:40.630
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Launch V∞: [7.081545070713602, -7.0729091815335625, -0.776577260159705] km/s
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Phase 1:
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Planet: Saturn
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V∞_in: [-0.12569211342020387, -0.19700859876116908, -0.07680141452474583] km/s
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V∞_out: [-0.14140915050284358, 0.1776207593128055, -0.09465864143283792] km/s
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time of flight: 1.1821819752862304e8 seconds
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arrival date: 2028-01-30T03:44:57.630
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thrust profile: [0.5002588515718371 -0.19771825906394763 -0.20353209361576632; 0.4054390241694503 0.040029185349386 -0.34107058991699124; 0.2423569923140263 0.0807257949835226 -0.3112829839329478; 0.18065015960900016 0.08740742446155071 -0.30403025066127853; 0.10248875965132118 0.06063796192970542 -0.21497968792565086; 0.08338045120220135 0.056688096391749335 -0.20215894735742795; 0.07887004887583762 0.05941979023466609 -0.21235731456802007; 0.0229843245681633 0.018505422430265896 -0.06785506490478066; 0.01823578179497519 0.01548440305634518 -0.06101618314749655; 0.0002901538197337305 -0.0016223591992106942 3.205407219406334e-5; 0.002873873687006971 -0.004662918383876911 -0.0004510593494124414; 0.00430470582405602 -0.003009020159280036 8.728342550493647e-5; -0.0022794285403208527 -0.0009648491939429927 -0.006293626488579706; 0.0011637101927252833 0.001071312493633596 -0.004770915783360482; -0.00107065156804025 -0.002699694621590011 -0.004509154573100797; -0.0020216781866428837 -0.0024564512238648174 -0.006095482963089488; 0.012471230063607982 0.00011388168858744913 0.0076364691595693784; 0.0009647357382865877 0.0008229274087098732 -0.0024345158387460123; -0.010410373178908307 -0.0063652727719950425 0.011194511483434939; -0.000643184932303301 0.002595909436010302 0.003527348481835557] %
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Mass Used: 131.50448265472824 kg
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Launch C3: 100.77739711976703 km²/s²
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||V∞_in||: 0.2459864887242357 km/s
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