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_0.5692256656303389 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5692256656303389---------------------------
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: 2023-04-27T06:05:31.538
Launch V∞: [6.680546812979104, -7.162772243463131, 0.2722836753500178] km/s
Phase 1:
Planet: Saturn
V∞_in: [-3.1328030579687496e-8, 4.9381663746382484e-8, 3.381411341193035e-8] km/s
V∞_out: [-2.158642822879228e-8, 4.506919525528456e-8, -4.6178746713735245e-8] km/s
time of flight: 1.8749577787484002e8 seconds
arrival date: 2029-04-05T08:15:08.538
thrust profile: [0.37517992056932625 -0.08421216066461282 -0.10325319088047422; 0.09421285260372156 0.03419449644726642 -0.08424041713423121; 0.09506457464917197 0.06371943839051811 -0.13989870300870969; 0.05430407675086123 0.05000310005760578 -0.11489738468636863; 0.026913668361163504 0.03088120925581708 -0.07601681676229424; 0.01788055897638759 0.024560353798129465 -0.06217456025379633; 0.024766846119865 0.0392082735146498 -0.10464408756779874; 0.02302478232902358 0.04028396407313864 -0.11022154400784634; 0.008773828566916175 0.017532342436077847 -0.049241392060404454; 0.0030431291160792845 0.006711117508839154 -0.019233441638897102; 0.0027054652535506486 0.007105091217335423 -0.024648592024531964; -0.0045885089913853695 -0.0019651076579180254 -0.008755090956050017; 6.087126627338159e-5 0.0008043251216070836 -0.003902531602262507; 0.00013375559968083802 -0.005519996861994213 -0.0033388444713886413; -2.4034748322698492e-5 0.0028769914255011757 0.006184837885815074; -0.003635598394741804 0.0041556029070532125 -0.002090717600090453; 0.002999758886226193 -0.0012639344204877188 0.004440351576483375; 0.0019466458775941622 0.0002448477309785155 -0.0008748274528346351; -0.0009896409326141037 -0.002962058572823561 0.008999999577279953; 0.0010989447114594455 0.005893297371961873 -0.004970364300509774] %
Mass Used: 104.04323296543498 kg
Launch C3: 96.00915033199323 km²/s²
||V∞_in||: 6.755285693586548e-8 km/s