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_0.6822394363533053 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.6822394363533053---------------------------
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: 2024-06-06T18:08:37.059
Launch V∞: [8.330593216100656, -7.373188211464181, -0.792015035216008] km/s
Phase 1:
Planet: Saturn
V∞_in: [-1.183897192928887e-5, -9.639238620608787e-6, -7.64444099643253e-6] km/s
V∞_out: [-1.4656413992252486e-6, 1.0960505287374608e-5, -1.2997710123785488e-5] km/s
time of flight: 1.874957778751348e8 seconds
arrival date: 2030-05-16T20:18:14.059
thrust profile: [0.0015711959672841612 -0.0013559658990181247 -0.001236504498562517; 0.014232717230222547 -0.033027670714973666 -0.028637734735745945; 0.018522010635571788 -0.05686145821846088 -0.0499349055006167; 0.04353390581791822 -0.13179998433140014 -0.11173063338870293; 0.03448989609590799 -0.09172219273292151 -0.08143909749248873; 0.056355953746159176 -0.14295823598437266 -0.12811423060559146; 0.03667048887537307 -0.08619895638012974 -0.07948629183171609; 0.023883622764208867 -0.05216972729762638 -0.0492379746833267; 0.01351866617716842 -0.02752436993441589 -0.026852595726665093; 0.009829132079396875 -0.018513359441684977 -0.018389520734572885; 0.0020403388533876206 -0.004224348189974316 -0.0061050750230524226; 0.004900860653955615 -0.004155713888710896 -0.0034480565456519903; 0.0015658865296962522 -0.0025713072772885477 -0.0031003784296287163; -0.00018687359061966358 -0.0030612866286395834 -0.0013546065089139134; -0.0007642047735673938 -0.0009526849657002503 -0.0038294733338663; -0.00044430553331317735 -0.006072260530905209 -0.001945276530345394; -0.0014714990441768716 0.0009653465817501029 0.003772818154904503; -0.0015960469545140722 -0.0033958634087623485 -0.0018276481756078857; -5.91411390321768e-5 -0.0010147364410716632 -0.00017132261299868893; 0.00041320778142633127 0.0003494895649835787 -0.0002692550761187952] %
Mass Used: 70.33781837154447 kg
Launch C3: 124.38997554982487 km²/s²
||V∞_in||: 1.7073770985797605e-5 km/s