23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.7645629890886761---------------------------
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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: 2024-05-01T00:47:23.075
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Launch V∞: [8.73880313785822, -6.841212344639952, -1.8714028039678943] km/s
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Phase 1:
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Planet: Saturn
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V∞_in: [-1.6732581120473174e-9, 6.860446957325391e-10, -9.282500736995751e-11] km/s
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V∞_out: [1.2520373296398024e-9, -1.1243756593593086e-9, -9.092199948036654e-10] km/s
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time of flight: 8.368410638254885e7 seconds
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arrival date: 2026-12-25T14:22:29.075
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thrust profile: [1.0 -0.7260816798125624 -0.5221109407270118; 1.0 -0.011316931989143303 -0.6866952050866189; 0.9881935702549839 0.19934038452552066 -0.6215555008566784; 0.3154718834284725 0.10216017394212862 -0.2433416646112872; 0.14711707090448456 0.060152940139807806 -0.12978235440846822; 0.007534520616440096 0.0041399447006685835 -0.011082377659710332; 0.01618670696724964 0.008306995296487547 -0.01714388189930545; 0.005254795968722959 0.002963788672743729 -0.005035034798062426; -0.0021515063363921976 0.004072224887162544 -0.002485463433734908; -0.003296859904492316 0.0011741654130089205 -0.002945407282860111; -0.000208967023188552 -0.010540017109930525 -0.001537380032761984; -0.008729610567923995 -0.004845759595065413 -0.010186553260316788; -0.005236179967622607 0.008126924716473123 0.007111589685472231; 0.01307268677621358 0.0077191986542122434 0.021391258095320578; -0.028019378449284222 -0.0003135368818428497 -0.0064059762529873835; -0.006864001827634412 0.01545260736826886 0.01304743063275955; -0.007420376723956295 -0.016135511013320458 0.005146723136338686; 0.0016214657768161105 0.004192070350132664 0.005732359502383033; -0.010097369113253684 -0.004882929238768678 -0.012899852661201902; -0.014087513138118318 -0.011511030060457393 0.017853991739108767] %
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Mass Used: 153.07589929532605 kg
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Launch C3: 126.67101508139362 km²/s²
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||V∞_in||: 1.8108192941506168e-9 km/s
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