23 lines
1.9 KiB
Plaintext
23 lines
1.9 KiB
Plaintext
archive/ES_0.7743052143442224---------------------------
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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: 2024-05-07T23:56:07.903
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Launch V∞: [7.241245091934011, -6.906985210123064, -0.6164143372376546] km/s
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Phase 1:
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Planet: Saturn
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V∞_in: [0.0007755880728621376, -0.0043715019091073535, -0.004170461993911833] km/s
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V∞_out: [-0.005341152906393544, -0.0006166836178435756, 0.002863060478918891] km/s
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time of flight: 1.462231607431396e8 seconds
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arrival date: 2028-12-25T09:28:47.903
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thrust profile: [0.1971827503426773 -0.11695238896712772 -0.044019206631471804; 0.01959670928655531 -0.02775765328889681 -0.04876788459056708; 0.057578671024243896 -0.07233909456322421 -0.028333223899165136; 0.05358560629208384 -0.0875510887394188 -0.031014454330973662; -0.0003146345701827112 -0.09934999023382536 -0.012895073281941616; 0.033382279905444394 -0.023993863557376274 -0.07147448322978738; 0.05112983799518981 -0.0007065451853939114 -0.14609002963705092; -0.014156907082229268 -0.060118624673692264 -0.05699468952354683; 0.25278096581204074 0.2256873219707113 -0.16139847774223737; -0.06645930394224449 0.1279634434894405 -0.08571621939688501; 0.0344042074517138 0.39636220993718996 -0.2038375133084272; -0.36491203086962026 0.18504663792736806 -0.275570940685372; 0.010574898073994789 0.01927268215930203 -0.12638316476881234; 0.1386503325766193 0.007999021241817748 -0.08033781575891921; -0.15930559781705678 -0.22778745945248555 -0.17377065620271137; 0.12172201712419288 0.5948990698536183 -0.013591909380693337; -0.1559329316782442 0.0714675387430356 0.17074309023327194; -0.45667461724179126 -0.40172264926720114 -0.3598550963270659; -0.15862291428778205 -0.19858064547764048 0.06393449183407363; 0.5290093715330506 0.28353928458088995 0.09471228310485809] %
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Mass Used: 316.9775061796886 kg
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Launch C3: 100.5220418094693 km²/s²
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||V∞_in||: 0.006091331467155461 km/s
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