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_0.5658832912892968 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5658832912892968---------------------------
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: 2023-04-28T22:16:31.089
Launch V∞: [6.3447756675560925, -7.358824180619245, 0.34362842053247533] km/s
Phase 1:
Planet: Saturn
V∞_in: [-9.89856930581946e-6, -1.419068354293409e-6, 2.7006068716201713e-8] km/s
V∞_out: [2.011720863651825e-6, -4.43308087727596e-8, -9.79219224434068e-6] km/s
time of flight: 1.8404597016001195e8 seconds
arrival date: 2029-02-26T02:09:21.089
thrust profile: [0.47386252372160037 -0.12508459783821624 -0.148141962244127; 0.07907691255770731 0.02232690976078561 -0.08040357338201333; 0.07924092785133621 0.04302735943558204 -0.13100676894207625; 0.0667845140245411 0.04913233069788861 -0.1534810643084068; 0.042507247591415144 0.03853677391491614 -0.12839802798250136; 0.027098556832575012 0.02878864848028949 -0.1014444352260999; 0.012538365233129905 0.015488634873592515 -0.057617855392462995; 0.010300993356230054 0.013908423308800648 -0.0538596147946673; 0.0049547724232446725 0.006620712787781871 -0.025934987046532028; 0.008113961674211159 0.012918752274596398 -0.05344069777704912; 0.0022908016562759484 -0.00046939875858349365 -0.008562326950629048; -0.0018922002011207487 0.0016142897826206984 -0.0025913519806487462; 0.00041686698624303353 0.004202272401834554 -0.006784540462731392; -0.0014543924493884827 -0.006490977300902346 -0.0004307278320462289; 0.003872659859962631 -0.008944092401853662 -0.0019023040556979906; -0.0037070358940953234 0.0003189072993950086 0.0021269216202324786; 0.000774975421619496 -0.0003800202298723642 -0.002778294832349628; -0.005114909850631054 0.0034280893237865428 0.0003146741300742019; 0.004332179562810054 0.003596147317798349 -0.016320723204346087; -0.0007328935413790436 0.005941794578871924 0.002622654371480284] %
Mass Used: 108.79228601256955 kg
Launch C3: 94.526552084276 km²/s²
||V∞_in||: 9.999807929356226e-6 km/s