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Additional display functions and section 6 draft done

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Connor
2022-02-20 22:10:56 -07:00
parent 472662fb60
commit 700f7e28cf
169 changed files with 810 additions and 944 deletions
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/home/connor/projects/thesis/archive/EJ_2022-02-20T15:35:42.756/mission---------------------------
Spacecraft: bepi
dry_mass: 2000.0 kg
specific impulse: 2800.0 kg/s
max_thrust: 0.0005 kN
num_thrusters: 2
duty_cycle: 0.9
Launch Mass: 4000.0 kg
Launch Date: 2027-05-07T16:42:16.204
Launch V∞: [1.7378678187417211, -2.46862158520496, -0.6330916686471314] km/s
Phase 1:
Planet: Jupiter
V∞_in: [-7.0779894637956104, -6.322884251065928, 0.08249231159415504] km/s
V∞_out: [-9.886721268095892e-5, -5.2044547868849095e-5, -1.4279616788653462e-7] km/s
time of flight: 9.753480002947423e7 seconds
arrival date: 2030-06-09T13:42:16.204
thrust profile: [0.3496133127402798 0.21627658848562392 -0.09375257020030825; 0.33049519901462543 0.4914216730807561 -0.04333085534469271; 0.015695434994927256 0.6376829912952088 -0.010776108385759698; -0.44272307995336146 0.6725191353780019 0.02401109287371488; -0.6273162232623738 0.6534499707573249 0.04855355942035699; -0.7062446552268619 0.5648886015889624 0.06359834741284556; -0.7337027908428936 0.34137315135163543 0.06893276201071429; -0.7263479369913934 -0.04280550187252788 0.06504582329795826; -0.6907323077547943 -0.29916252254363473 0.05655854617201239; -0.6304099965747246 -0.39539357580226175 0.04777470251604466; -0.546644598339376 -0.41045795909146016 0.03986867238422301; -0.4449769658797206 -0.3791551577739326 0.03302815362892815; -0.3343801111760648 -0.3170155537328812 0.027015156520834947; -0.22238014374440118 -0.2330409572673364 0.021363765089885373; -0.113202981166323 -0.1334888611558203 0.015342498857529623; -0.017481222034237697 -0.026432427062662682 0.0036199536612145674; 0.00010928351095286555 -0.0017246713395881355 -0.002344486658782495; 0.0003606569072872833 0.0017587019964605832 -0.00047445201553678664; 0.0018193454249226754 0.0015129170111366306 0.0008999344832791579; 0.08640210944237164 0.058949618519573616 0.004429993495706424] %
Mass Used: 1720.4129974933717 kg
Launch C3: 9.515082147268366 km²/s²
||V∞_in||: 9.491238332454378 km/s

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