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_0.5667280118534229 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5667280118534229---------------------------
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: 2023-04-30T10:18:44.093
Launch V∞: [6.257826064122974, -7.654028816959386, 0.03529920638454202] km/s
Phase 1:
Planet: Saturn
V∞_in: [-1.1375147268991854e-7, 2.302727225294707e-7, 1.021744500299927e-7] km/s
V∞_out: [-8.782469437467271e-8, 1.4092586695622753e-7, -2.2134103259434204e-7] km/s
time of flight: 1.7854460413109964e8 seconds
arrival date: 2028-12-25T22:02:08.093
thrust profile: [0.22314061006559577 -0.07006959546123884 -0.0846753651143935; 0.08549526323804416 0.018016162196297123 -0.09490693907326063; 0.04031257519234377 0.018082471925146112 -0.07568347013903132; 0.041836585240247866 0.0260064949383866 -0.10768708920672497; 0.028546695449653645 0.021539162848539593 -0.09465839206271652; 0.03224778148902765 0.027609616064035038 -0.12543367866099797; 0.020335838023994822 0.018698783136941906 -0.09204676311214473; 0.010018564901383477 0.010766032516865151 -0.05482024342730423; 0.020284218656943413 0.021510373244606168 -0.10872762012995166; 0.02260461051232536 0.02359107562410601 -0.12635387292353162; 0.0041563823487434925 0.003332762606513975 -0.01927189221738655; 0.002058159733405421 0.0033913196814438396 -0.012917716367347242; 0.00044343132629328893 0.00010766242671242398 -0.002241446161979872; 0.0002316141134106228 0.00022020134245247336 -0.0017189755560152705; 0.005891635007866447 0.0010844321088795685 -0.0020832071923883337; -0.0004361631455906873 0.0008382400705034555 -0.0015376103511120047; -0.0026594928582525648 0.006242354711080126 -0.0022294258763317478; 0.0015574787824121426 -0.0023111089038675217 -0.002265396612141605; 0.003703839802724506 0.0018820202526912979 -0.0047441870092265834; -0.0035480202525579713 0.000545773454771338 0.001185482270199536] %
Mass Used: 90.99890424946807 kg
Launch C3: 97.74579021363292 km²/s²
||V∞_in||: 2.7641371622839445e-7 km/s