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_0.5606415604367481 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5606415604367481---------------------------
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: 2024-05-13T00:43:38.934
Launch V∞: [7.754929172135357, -6.084689621468404, 0.30510776390118677] km/s
Phase 1:
Planet: Saturn
V∞_in: [-6.615353595454984e-6, 1.758144961982311e-5, 4.30266145031949e-5] km/s
V∞_out: [3.989357030641408e-5, 6.694525180779326e-6, -2.406577103219387e-5] km/s
time of flight: 1.7635150570637712e8 seconds
arrival date: 2029-12-14T03:15:23.934
thrust profile: [0.27496555713525717 -0.025304636674319682 -0.09956751031224323; 0.06845222318765247 0.028078319849676996 -0.08153028444001328; 0.06298930195322987 0.04202159289458482 -0.12897195154250135; 0.05089177139276519 0.0427633159257794 -0.14856035082898994; 0.032941908988573514 0.03198194830196141 -0.12826998911245496; 0.02850040361894859 0.03397275412990294 -0.1367813040566968; 0.015852415207725977 0.018347405446324683 -0.09138105159804659; 0.006427615419029497 0.008958239345983167 -0.046180260273142745; 0.002272303642932582 0.005560584307973425 -0.026391769583483812; 0.0018141741963347395 0.0030871345996612634 -0.016864247355228363; 0.001005514540111178 0.0009210441047667801 -0.0030550389799378097; 0.001631547756106779 -0.0003546721178249659 -0.0067685558863372144; 0.0029721099064621997 0.001455300733272206 -0.010588907691991984; 0.001053237009133936 -0.00039514356350233543 -0.000979893394454582; 0.002746222056038513 0.002880590771527264 0.0009898248095278387; 0.002777902108984867 -0.006238477163958758 0.0015229369877837414; 0.0007119660290836647 0.004315810530984631 0.003388600657835204; 0.004077623555325966 0.00030902555067296544 -0.0019756581313889513; -0.00437794688898076 -0.00022232469745011682 0.0033881495876056642; 0.001051800874826109 0.0031566719506708777 -0.0013286686855279411] %
Mass Used: 86.75827466434066 kg
Launch C3: 97.25546500203407 km²/s²
||V∞_in||: 4.694848058812787e-5 km/s