connor/thesis
1
0
Fork 0
Code Issues Pull Requests Actions Packages Projects Releases Wiki Activity

Maybe nearing the final commit

Browse Source
This commit is contained in:
Connor
2022-04-18 10:59:25 -06:00
parent 0fb875c777
commit 5b6656a9a6
3598 changed files with 79349 additions and 572 deletions
Download Patch File Download Diff File Expand all files Collapse all files

22
archive/ES_0.5606359899439339 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5606359899439339---------------------------
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: 2024-05-14T12:54:15.504
Launch V∞: [7.960571840336577, -5.86037902971746, 0.3422990421812846] km/s
Phase 1:
Planet: Saturn
V∞_in: [2.778968985118717e-5, -7.304935490560097e-5, -0.00019248612798158316] km/s
V∞_out: [-0.00018977148495204094, -2.5976943231403502e-5, 8.051743587242314e-5] km/s
time of flight: 1.8516189250146922e8 seconds
arrival date: 2030-03-27T14:45:47.504
thrust profile: [0.18997646554796904 0.0026423584499857987 -0.059110128431544194; 0.09542589760245643 0.05736689629202108 -0.099176687308847; 0.06374346302317256 0.06374790809631388 -0.12104546578341321; 0.03275864612981749 0.044317419571098325 -0.09703845416592112; 0.03013836856960901 0.046327253233469194 -0.11483990094855538; 0.01515321052763947 0.029551226963753358 -0.08023529941444804; 0.009979793407884541 0.022137515148922614 -0.06297025268633616; 0.01171754483839349 0.03073874583012853 -0.08988354062516912; 0.0008765885261013454 0.004557974122678285 -0.02019117995386654; 0.0021171283786651654 0.004531112122591545 -0.022047459407784048; 0.00034330449416909974 0.005047741685768997 -0.0154708836643964; -0.0022406547607288748 0.002661542595713228 -0.004799751665873662; -0.0047100576854509435 0.00629815172119277 -0.0034728666660262496; 0.0007458858303874996 0.002295959067419079 -0.0016169435078431408; 0.010419404098202757 0.009478878698565011 -0.004783956535229678; -0.0029337756573978905 0.0005107926891517005 -0.008565260910906137; 0.0054850569158807205 0.0034074814184008803 -0.007327697664354701; -0.0005421453118149228 0.006120834680698736 -0.013448854054111448; -0.008779103162370811 0.001103913815124487 -0.0022310344858875062; -0.00047870728095311183 -0.005872304367812742 0.0057879294084041445] %
Mass Used: 83.38915058481416 kg
Launch C3: 97.83191503139007 km²/s²
||V∞_in||: 0.0002077483684159566 km/s