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_0.5689232415181253 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5689232415181253---------------------------
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: 2023-04-29T19:47:43.509
Launch V∞: [6.139989752845699, -7.756470595755766, 0.8982460180992401] km/s
Phase 1:
Planet: Saturn
V∞_in: [1.839046311624002e-10, -4.004111745419425e-9, -1.6511254905613418e-8] km/s
V∞_out: [5.871088435998627e-9, 8.309734468775895e-9, 4.0695306357692264e-9] km/s
time of flight: 1.7440448725943795e8 seconds
arrival date: 2028-11-07T09:29:10.509
thrust profile: [0.17271841045040728 -0.062150073866923186 -0.06606555014177165; 0.07926504717891047 0.010529385766815818 -0.08954263249497144; 0.06566977161712605 0.021215316633998626 -0.12207041605231997; 0.11353524707562175 0.051635501833263216 -0.2726876288929356; 0.04282929212396326 0.022185035496092374 -0.1363027387667022; 0.028795619296629795 0.017022530375422958 -0.10688121598791794; 0.020133842223588324 0.013240361217990418 -0.08931067084235549; 0.012135967501174244 0.008200632909761566 -0.05961114494254005; 0.007694249915701059 0.006113930474513418 -0.04389236822097041; -9.630549279050752e-5 0.0009276229513686864 -0.0031654850016100645; 0.0018714199836659278 0.0014961393647442598 -0.01116665955263791; -0.0004325910426692515 -8.925671686933951e-6 -0.00047057509304716273; -0.0023810250366923485 4.7854144692627406e-5 -0.002947892305270475; 0.0009519287836862896 0.001203003899662275 -0.006627483499534031; -0.0003379695576999979 0.0021397984754595867 -0.007889381374706862; 0.0018526182750906236 -0.0008398838594298359 -0.007098153471190913; 0.000982511656564293 0.00042728194833736724 -0.005108134717144937; 0.0011399004330542454 -0.00281128138769559 9.854296576216389e-6; 0.0023863161615499343 -0.0015367264302646917 -0.00818092195722848; -0.00019037693883326167 -0.0002503941653926727 0.00047563381079359594] %
Mass Used: 88.17370407253293 kg
Launch C3: 98.66915617690513 km²/s²
||V∞_in||: 1.6990829006888156e-8 km/s