23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.6290938577119098---------------------------
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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: 2023-04-20T07:50:33.493
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Launch V∞: [5.3142818597630805, -8.401570407143561, -1.1587833361668403] km/s
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Phase 1:
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Planet: Saturn
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V∞_in: [-1.4323001149415608, -1.3442465247893642, -1.4539956541354755] km/s
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V∞_out: [0.793151505767186, 1.4102779982955926, -0.9951128835804696] km/s
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time of flight: 1.0967760000449966e8 seconds
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arrival date: 2026-10-10T17:50:33.493
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thrust profile: [1.0 -0.8166710532075767 -0.5038353125249835; 0.5148133388880103 -0.08906282776182026 -0.4402326702419359; 0.17728936963363898 0.0075182268512021255 -0.23367560410913205; 0.15308183571669332 0.026748394813402607 -0.25159425755905; 0.05679644805799902 0.013416077190416102 -0.11118524095993915; 0.10976779590780975 0.038327285622240054 -0.2399774397768107; 0.10162206110690675 0.03140764126366659 -0.226737345452707; 0.025488493262277867 0.009680299220854206 -0.0650425907365379; 0.0010911740617850691 0.0005623531801144358 -0.002624796727774563; 0.0011501809963381968 0.0007147647678963501 -0.001356955397911622; 0.0008257852952834393 0.0003109550240617494 -0.001971224546561709; 0.0004908649283765026 0.0019049031381954756 -0.00031562002718425394; 0.0018572554534586334 0.0006907033644521169 -0.0007078992455032464; -0.0022787574612374104 0.003041000810529779 -0.0013535172266842524; -0.0026053121768242395 -0.0093310895493239 0.0006563557459467013; -0.0036703749207311594 -0.004962991196767098 -0.0001979411014053568; -0.0047753600162294884 -0.00440605450339295 0.0005884115726305875; -0.0027099082444340165 -0.0001580632515395334 0.006567446328945507; -0.0009300291528827197 -0.0006482017569574611 -0.005039117577149453; -0.0011217109700735507 -0.0015211312967706877 0.004127857998783978] %
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Mass Used: 149.61342509753877 kg
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Launch C3: 100.17075581137533 km²/s²
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||V∞_in||: 2.443887415760951 km/s
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