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_0.5638644011827746 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5638644011827746---------------------------
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: 2023-05-03T05:13:17.332
Launch V∞: [6.604176224375799, -7.456822444428203, 0.13403813009696364] km/s
Phase 1:
Planet: Saturn
V∞_in: [-2.9986007071319625e-8, 5.7874978144742856e-8, 3.08730436020303e-8] km/s
V∞_out: [-1.8725730076095615e-8, 3.723141483641799e-8, -5.970446589210912e-8] km/s
time of flight: 1.8749577787479165e8 seconds
arrival date: 2029-04-11T07:22:54.332
thrust profile: [0.13252453140520581 -0.03550390585033915 -0.054052080939185586; 0.061626657559503945 0.012970099825325168 -0.07522553153470089; 0.047266406353267565 0.020070228177598688 -0.0994031937343705; 0.042729137522014966 0.025585753199833142 -0.12562699348648984; 0.032919451999338795 0.02330342539235615 -0.12391349222353838; 0.0269989054927121 0.021123669307639197 -0.12110553291326809; 0.020334046236930418 0.015960136386489535 -0.10184394572659393; 0.009875994558921096 0.008798793058137735 -0.059136099448188185; 0.013398149378463618 0.011959943571156397 -0.09029137943597323; 0.00035912374006928454 0.00072504963360866 -0.008706220543393862; -0.0006868288450664569 0.0011328640063202975 -0.002128496344193574; 0.001776912661759146 0.0015461637573311545 -0.00024621920714314725; -0.004013623277636089 -0.0024641550778923263 -0.002153417520059833; -0.0017285179270593763 0.0035049984309919527 0.0008674784923272763; -0.004729122745655406 -0.004862288538844815 -0.003087320487264604; -0.0032018165472996016 -0.0006608124448496215 0.0008146490318873912; 0.000983627541141239 0.002307845305396208 0.0011512407088704153; 0.0020248095646193433 0.004288452096283036 0.003633150994365581; 0.0029508956432854677 -0.0024011104171479166 0.007119373955254842; -0.00017590882923803643 0.0001090364651493489 -0.0006132756930185166] %
Mass Used: 78.95748843439469 kg
Launch C3: 99.23731079065868 km²/s²
||V∞_in||: 7.212363368957889e-8 km/s