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_0.5657972782299101 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5657972782299101---------------------------
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: 2024-05-10T01:16:56.401
Launch V∞: [7.3075110377914, -6.43829454475096, 0.254387362353164] km/s
Phase 1:
Planet: Saturn
V∞_in: [2.6868910767354994e-5, -4.705241428426204e-5, -3.6433030330673347e-6] km/s
V∞_out: [3.162935202177813e-6, -1.617304549379666e-5, -5.171200321326409e-5] km/s
time of flight: 1.6309532882747093e8 seconds
arrival date: 2029-07-10T17:32:24.401
thrust profile: [0.4848769226191405 -0.09738123084639863 -0.17668208814102368; 0.10064110038545454 0.02750584214460962 -0.11287480283074815; 0.0823403158514641 0.03998519921679431 -0.15586403830826645; 0.07405285247871439 0.04739568226878764 -0.1996733613515048; 0.0618222351292469 0.04572180528030232 -0.2134909648175021; 0.029160852071327795 0.02329513994774094 -0.11639424220433182; 0.011319972692331471 0.010380027399080975 -0.05621377303047424; 0.012375983403733462 0.011398496700887998 -0.06352626249870011; 0.004809059664576253 0.00458827933232713 -0.02974797725639961; 0.0008782813984866398 0.0008252822387747647 -0.004743619058510852; -0.001208480572837451 0.0009999591116286028 -0.003322875966338385; 0.0011311032345026808 0.0012474698939579265 -0.008011308135575488; -4.787197605404933e-6 7.958289247861957e-5 -0.0039958074830011864; 0.0002678943501570766 0.0002496289390456362 -0.0032028708564104513; -0.0018008106220136477 0.00020336267234885355 -0.003943881160976689; 0.0002161499446954924 -0.005191022432700686 -0.004553586450013697; 0.0010242201675348377 0.0010005996159885965 0.003754638015558802; -0.003479384555623013 0.002515136882436601 -0.001245220093763131; -0.0053216308926234916 -0.0019042175004608986 -0.005087066248765592; -0.004454300657447449 -0.0008771847515132742 -0.003797523794092078] %
Mass Used: 106.41976627008944 kg
Launch C3: 94.91606714253811 km²/s²
||V∞_in||: 5.430600070703669e-5 km/s