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_0.5631385347638227 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5631385347638227---------------------------
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: 2023-04-30T04:00:17.003
Launch V∞: [6.018013745570062, -7.441962824920683, -0.028508982700458048] km/s
Phase 1:
Planet: Saturn
V∞_in: [-3.65949717103172e-9, 5.639370122855033e-9, 3.8284018801565926e-9] km/s
V∞_out: [-2.3961028459222574e-9, 5.4985506044111085e-9, -8.137543017017272e-9] km/s
time of flight: 1.8555904937173668e8 seconds
arrival date: 2029-03-16T20:11:06.003
thrust profile: [0.6351557884326726 -0.15917826167880403 -0.18862726099897262; 0.20625832245821982 0.061754980438145646 -0.1989678735212001; 0.06368405781738876 0.03773423453567815 -0.11033207638815483; 0.06727958999345864 0.054055463974631034 -0.16032720694277816; 0.03197976064065933 0.03165788980294202 -0.10216202534413066; 0.016507045845823822 0.01910908268831246 -0.06651242258569663; 0.010025559390981532 0.013206513861745211 -0.048695236363809784; 0.005372475607246087 0.007660998714260214 -0.02986053487136801; 0.006940520382456588 0.010338567162719841 -0.04652124218644896; 0.006080587384945944 0.010321803529316708 -0.043471037848912056; 0.0010723114743800667 0.0018422017186122237 -0.008312876707177074; 2.4288549600028433e-5 0.00013419012098323075 -0.0004269540628531149; 7.489015617615229e-6 7.120478106900532e-6 -8.422088077594434e-5; 2.83426658168513e-5 5.718572749572356e-5 -0.0003699913526802127; -0.00011843776685695453 0.00022288031124201565 -0.0003570207309973436; 1.5769803749870022e-6 -9.937041204911189e-5 -0.0002491244248688067; 4.5325208403649675e-6 0.00032199572373707455 0.0002892864297814556; 0.00041847579333255207 -0.00014011023614095362 -3.762299173925058e-5; 0.00019480730383130047 -0.00035077743835943093 -0.00011131415740128477; 0.00019109792004651826 -2.2963011230553614e-5 0.0002485478829796483] %
Mass Used: 122.66096535757333 kg
Launch C3: 91.60011289146625 km²/s²
||V∞_in||: 7.736347709567203e-9 km/s