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Maybe nearing the final commit

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Connor
2022-04-18 10:59:25 -06:00
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/home/connor/projects/thesis/archive/EMS_2022-03-31T02:42:47.529/mission---------------------------
Spacecraft: mySat
dry_mass: 200.0 kg
specific impulse: 3200.0 kg/s
max_thrust: 0.00025 kN
num_thrusters: 1
duty_cycle: 1.0
Launch Mass: 3500.0 kg
Launch Date: 2024-05-23T06:02:13.164
Launch V∞: [4.790675190538004, -2.7827628147301513, 2.3322515350749833] km/s
Phase 1:
Planet: Mars
V∞_in: [-1.4810007913292704, -3.291455435720552, 2.9831687001217015] km/s
V∞_out: [-0.5916884460359885, -2.770372854415817, 3.728441598440503] km/s
time of flight: 1.463399999793926e8 seconds
arrival date: 2029-01-11T00:02:12.164
thrust profile: [0.3803411573668084 -0.24699359911364535 -0.48327553487098146; -0.45637919416245415 0.20259655112804134 -0.4183214076160344; -0.43367448998695834 0.4136614397548196 -0.27973436226784304; -0.5190285617571937 0.29456217917248934 0.127585421435257; -0.5523405717458744 0.26680149330655734 0.3932431972939049; -0.5996656678338447 0.2522039800955279 0.4621499788811929; -0.6304800501642223 0.0890041612002452 0.5223357259424798; -0.6361153588831391 -0.24667340158896864 0.5373571355951733; -0.5825139178259425 -0.389919029978712 0.5093601462685652; -0.5454531372852401 -0.44623500436201025 0.3645214794294788; -0.4801024497934835 0.2102254586306563 0.2565776222052905; -0.579136948771309 -0.13710895068534665 -0.20134408320607608; -0.5188982220935089 -0.42618154892831445 -0.3564433259684089; -0.5230878988602696 -0.4827987429089918 -0.33730666065169657; -0.4547076944063366 -0.17486449212182634 -0.32509286969961976; -0.5648002138742563 0.1946720610839311 0.06983061891210761; -0.620774801689964 0.3715690637443947 0.19453195354416444; -0.634451658470199 0.34548391469755085 0.34375519703180396; -0.6916942031325952 0.12255205006355444 0.4731318096261815; -0.6556954878586314 0.06192414594617366 0.475764756523579] %
Phase 2:
Planet: Saturn
V∞_in: [0.6126357305264523, 0.036628352063377154, -0.44998341351260274] km/s
V∞_out: [-0.40771540308617077, 0.5213716669014113, 0.1788657968644158] km/s
time of flight: 1.7526600019051787e8 seconds
arrival date: 2034-08-01T13:02:12.164
thrust profile: [-0.4584109571736202 0.1135715923073197 0.3475236165861346; 0.28933933320539057 -0.16213518851926365 0.3689204283653291; 0.7767123213868962 -0.30606989550403363 0.2968304361134133; 0.8171230455941187 -0.177050989819005 0.13516760011367504; 0.792566162402287 0.7145286520800527 -0.4309109115263434; 0.7426473957923972 0.8547076140253718 -0.4619343157035517; 0.6131385822232893 0.8703485610178433 -0.37934354880999643; 0.05835968610825082 0.8697084452811487 -0.20558789532136582; -0.013918439576788977 0.8562307293716963 -0.016866144920425347; 0.14989145996688175 0.8391019899698795 0.09255224234844622; 0.18019735809471005 0.8224708378791422 0.16995741266663397; 0.14139412971775753 0.8023864633039065 0.20129093897625455; 0.17968164104668602 0.7805428866365428 0.2139526044756662; 0.08498935350820547 0.7527751665441202 0.19421753791674876; 0.03954352379181277 0.7151788408627606 0.18168198769090368; 0.03303845971086855 0.6728825558974967 0.14690981920697405; 0.02940785938392452 0.6148823095722372 0.10110999555278848; 0.017750178567555636 0.5324957838020801 0.08462070573863552; 0.014357313865460512 0.37335705098385324 0.058909504167600976; 0.00697353943058537 0.10646619320896161 0.016159717939472934] %
Mass Used: 1920.8181793791025 kg
Launch C3: 36.13373488714083 km²/s²
||V∞_in||: 0.7610185588597774 km/s