23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.6786510691264909---------------------------
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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: 2023-04-24T13:48:06.612
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Launch V∞: [5.541813596297596, -8.800404908882074, -2.3539114165918735] km/s
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Phase 1:
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Planet: Saturn
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V∞_in: [0.00011875776195185788, -6.582745817436946e-5, -0.00011806946338181835] km/s
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V∞_out: [5.218027879652468e-5, -0.00011875151479647383, 0.0001247130031818499] km/s
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time of flight: 1.0477817216233343e8 seconds
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arrival date: 2026-08-19T06:50:58.612
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thrust profile: [0.5166168294034894 -0.42159355006765886 -0.29838585693023645; 0.2613694539774006 -0.07583112457673323 -0.24362198860493578; 0.14267185487947917 -0.01680974045361836 -0.1851968964542207; 0.05963690949253759 -0.006639172258966266 -0.09211009168105118; -0.0005913934399714785 -0.03296499244175606 -0.04924779424611121; 0.07447849004547287 -0.003935838614050122 -0.07024061122497827; 0.05706673623851734 -0.013484273477286078 -0.08651065732337279; 0.013222323271434286 0.00490552245522012 -0.029553696309997737; 0.008195719336596352 0.009801823200051962 -0.026710979660392275; 0.0075113543756136145 0.015144210850312366 -0.0434361738027845; 0.01282922634716346 -0.01916886725576724 -0.003381748545668639; 0.004592515124317955 0.008785930312560204 0.012186717891221877; 0.03812806122214163 0.05718459315868231 -0.06277704738333836; 0.06616997786241434 0.05316694581842777 -0.014132455875622467; -0.04133506176594507 0.02993236336782946 0.02781284510061073; -0.05980846987555781 0.07271416559110527 -0.21331715488252903; 0.07331309311480232 -0.10167870068271054 0.1228231758343177; -0.08896636452447687 0.22348712372712087 -0.15012700832249765; 0.06558515758498433 0.0916181658857709 -0.15685072038092496; -0.0011756140859066463 -0.07260650614284078 0.07344818387970319] %
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Mass Used: 128.51119383522018 kg
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Launch C3: 113.69972345354616 km²/s²
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||V∞_in||: 0.00017993626220632418 km/s
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