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_0.6191535652127245 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.6191535652127245---------------------------
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: 2023-05-02T21:29:16.718
Launch V∞: [6.391373033024575, -7.592661856037789, 0.016776871105339444] km/s
Phase 1:
Planet: Saturn
V∞_in: [1.8582078404865137e-7, 4.771853382365994e-8, -6.050637074266155e-8] km/s
V∞_out: [1.9373788652576166e-7, -4.86981150486479e-8, 2.426705491908171e-8] km/s
time of flight: 1.8393882525605264e8 seconds
arrival date: 2029-02-28T19:36:21.718
thrust profile: [0.1943793682912686 -0.07165834817253139 -0.06566090915334023; 0.09047049384753277 0.09050781000674532 -0.014568347073951039; 0.009155149658652863 -0.010438136550214507 -0.0454775278757411; 0.03085956560500499 -0.005659974100338611 -0.0792293743671805; 0.01746862680361731 -0.010235266198677494 -0.06675891753458289; -0.016566235872967662 -0.012976832412670558 -0.029510443239439254; 0.018613545928896094 0.09443033199544254 -0.04291213051103289; 0.01626878657591351 -0.01815668808466127 -0.12676480429510442; 0.08755921267457334 0.06090239318749957 -0.07737312322110973; 0.0035833214133381627 -0.014071289884522161 -0.05516592256339695; 0.024310948486015088 -0.023284759413780595 -0.07906206414242525; 0.022784713896892246 0.007197624325757373 -0.09724830083327111; 0.014653820681754 0.0018313212626211075 -0.10922530804976091; 0.02780955094951383 0.05518204193354144 -0.07520252771697132; 0.05917240146368348 -0.08051075088464868 -0.048835678961762434; -0.09202116666908824 0.05924482123158176 0.02049091020555114; -0.05228445457423975 0.02959557250742745 -0.06375392402544772; -0.017659901982860403 -0.04241609148742411 -0.022355613053700204; 0.024494692324692452 -0.01622294885938727 -0.0016651886595341059; -0.061499333793469044 0.20632657581804087 -0.06564171805862631] %
Mass Used: 147.77156491845926 kg
Launch C3: 98.49844477080903 km²/s²
||V∞_in||: 2.0116521358123456e-7 km/s