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_0.5667150850083381 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5667150850083381---------------------------
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: 2023-04-30T22:24:56.154
Launch V∞: [6.57842068552691, -7.291246980208207, 0.21118814949843046] km/s
Phase 1:
Planet: Saturn
V∞_in: [-3.804547221020031e-6, 3.4955504772456314e-6, 4.179231032732687e-6] km/s
V∞_out: [5.684355895933197e-6, 3.442075570222526e-6, 1.0671764352225668e-7] km/s
time of flight: 1.8749577787493062e8 seconds
arrival date: 2029-04-09T00:34:33.154
thrust profile: [0.3648480794877507 -0.09639865890507972 -0.12938358299077038; 0.04000095732814677 0.010350949392176609 -0.0435708400291759; 0.043293838951095134 0.021497714830288513 -0.08053765091046282; 0.04912058723766091 0.03248550670550674 -0.1278942045367903; 0.037914454968779765 0.030091194747277252 -0.1266139948212368; 0.024909153406145766 0.02263464807255522 -0.10134134480766857; 0.01954803983953779 0.01987046166039587 -0.0925219398918508; 0.027903429584251235 0.030286904519876423 -0.15235642423875062; 0.0023805595887819594 0.0037802415543872125 -0.014183657735806616; 0.0013994861825520997 0.003281103106616083 -0.006557767322572863; 0.001546778248289239 0.002610408793531969 -0.00863787130419833; -0.00027502635842669375 0.0018759576242724097 -0.0055271229630158535; -0.003245322110124017 -0.0026620335318437607 0.0021133669226921104; -0.0018180497331716852 -0.002515764542518769 -0.005665582590534993; 0.00022855259121393559 -0.008544306421316629 0.005380167019630039; -0.008306932588723599 -0.01195690930940746 -0.008615083967627592; 0.013349549689794009 -0.008376059492618092 -0.003180621966075492; -0.01498738413255655 -0.004322443798514423 -0.008605423793847499; -0.00369462836067017 -0.0034107161019037557 0.0021581161871674776; 0.00809568165468147 0.0037700438970776676 -0.007997526161793514] %
Mass Used: 98.35300606258988 kg
Launch C3: 96.48250167665222 km²/s²
||V∞_in||: 6.645255805527679e-6 km/s