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_0.5566315118638512 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5566315118638512---------------------------
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: 2024-05-13T13:53:20.094
Launch V∞: [8.041924940015964, -5.758932806746821, 0.13694074362883282] km/s
Phase 1:
Planet: Saturn
V∞_in: [1.4162025723800402e-5, 9.974582223769057e-6, 0.0007107589462809278] km/s
V∞_out: [-0.0006188888055969824, -0.00023762775180590965, 0.0002557924496816423] km/s
time of flight: 1.8363980032475007e8 seconds
arrival date: 2030-03-09T00:56:40.094
thrust profile: [0.23577755687127958 -0.0071874630235881165 -0.07760623681214428; 0.051115311923208465 0.026697168524299694 -0.06074369468695647; 0.039827247082705325 0.03367302371107593 -0.08291636600406131; 0.034087758923255745 0.03703212145652103 -0.10300070007975447; 0.03629347207863677 0.04944954956705227 -0.14950741466760087; 0.028047317620275757 0.04393644358960109 -0.14262416180763152; 0.012926818532523011 0.020693717969065557 -0.07945182708103844; 0.005720610162085937 0.01185566556373241 -0.0478567256032916; 0.0060399125884840225 0.012932759031051082 -0.05372067493668958; 0.0011893583151980107 0.0021055945605056845 -0.01081166964896968; 0.00035709918053846454 0.0006242953885042862 -0.004617968565516032; 4.741652592622882e-5 0.00033765058195846806 -0.0022873744130346694; -4.999729439486968e-5 -0.00029305683868026584 0.00019101131357931783; -0.0004049802696953789 -0.0010158396956874722 -0.00012723247860394805; -0.00032236353625011917 0.0011532940768782477 0.00013449205096291265; 0.00015110315172121988 -0.00021038188423430702 -0.0008677258742379387; -0.0008270010419782249 -0.0016748546468864803 0.0026119882054554465; -0.00014382962492279975 -0.00011622591303514995 0.0003575368025516793; -0.0003820064502324071 0.0008937344837922788 -0.0006685198182215099; -0.0010161966401385097 0.0004249769492182886 0.0012122926030899072] %
Mass Used: 78.57316712016927 kg
Launch C3: 97.85661658074122 km²/s²
||V∞_in||: 0.0007109699958377394 km/s