23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5643999388773007---------------------------
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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: 2024-05-13T00:10:24.237
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Launch V∞: [8.050641560916652, -5.582536225930336, 0.09549062058273851] km/s
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Phase 1:
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Planet: Saturn
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V∞_in: [-2.6543380813727797e-9, 7.202680021841308e-9, 3.515965314503975e-9] km/s
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V∞_out: [4.284802254281796e-9, -4.020592930845045e-9, -3.382008638519899e-9] km/s
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time of flight: 1.8749577787484032e8 seconds
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arrival date: 2030-04-22T02:20:01.237
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thrust profile: [0.36633876272950316 0.007556856414636612 -0.10908177839750523; 0.08882086423886171 0.05483958267149641 -0.09736606264408099; 0.0459964203009345 0.046042439511285845 -0.0926166324647024; 0.03256754124138007 0.043624253935043725 -0.09758079328449151; 0.023042184546971465 0.03739726989951144 -0.0949935731091168; 0.019644753232814494 0.039540630054514005 -0.1060538411345155; 0.013022824074659206 0.029511103856909342 -0.08558779899468617; 0.006453653694089385 0.0160031114121656 -0.050401115205450805; 0.004445435210033899 0.012058592110943398 -0.03948210793576308; 0.011039570657627269 0.01304631133092751 -0.015967879525523847; 0.0036210016322019245 0.0070701044009361 -0.02499600616062048; 0.0002651332697528754 0.0009081892206178302 -0.004984108262783293; -0.004331818521105767 -0.0055807385402362256 -0.001544060096802379; -0.005866051395832797 -0.01299094702794404 -0.0038273924379808185; 0.007895910652783802 0.010178596605159256 0.002593038630655585; -0.0005787159658422804 -0.003135043274486912 0.00595418709826352; 0.00457184267360769 0.0028304319476784396 0.0024546166478061782; 0.014077481845683436 -0.012293772324841388 0.014588417630155521; 0.00919022555583127 -0.015156154301643378 0.015555283322868294; 0.0022784884890546878 0.0029313230617673347 0.01387435734666805] %
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Mass Used: 98.5444195205041 kg
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Launch C3: 95.9866587148023 km²/s²
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||V∞_in||: 8.443110933776286e-9 km/s
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