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_0.6375806472704638 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.6375806472704638---------------------------
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: 2024-05-08T19:05:35.635
Launch V∞: [7.161752291831886, -7.594696187286239, -2.0153386513712306] km/s
Phase 1:
Planet: Saturn
V∞_in: [0.006582937344947125, -0.004189565548191936, -0.016296016749258596] km/s
V∞_out: [-0.0027286023071583327, -0.017835700964171662, -0.0007652137809617] km/s
time of flight: 1.0408485333393845e8 seconds
arrival date: 2027-08-26T11:33:08.635
thrust profile: [0.5502352311613862 -0.2792171166156014 -0.3089813777754755; 0.2940297518377967 -0.02236816129752549 -0.31923329060804473; 0.1608818234589802 0.01685322874658531 -0.2619188521355404; 0.07965217177059011 0.01637604306316858 -0.17012934798878693; 0.03145109049931313 0.008409352355677581 -0.08367517022055017; 0.04368052011364387 0.015056105751750992 -0.13807240530125633; 0.00860376016508424 0.004396864817347266 -0.031240294785579496; 0.01743664692828919 0.006383240124638949 -0.0653617121088275; 0.007485709706039308 0.001952590749296353 -0.030701968525511103; 0.005026006323881407 9.203467946022968e-5 -0.013982271611405797; 0.0006775677506997035 0.001454893031671482 -0.0037091809332017995; -0.0005349892176301414 0.0025175416841089066 -0.005091779787778902; -0.0007982302708328315 -0.00011631033365559502 -0.0027065106898485607; 0.00017872980745711124 -0.00061642369259572 -0.0027423469163897207; 0.001005606193868493 2.4535049214285433e-5 -0.005025062016168802; 0.0019456917238976114 -0.0018429700581824903 -0.003774115492682222; 0.0027357225341884898 -0.001162807751023484 -0.002349146539949253; -0.0009195361470908927 -0.00015827473434077463 -0.00011461489035826267; 0.0007678878925949097 0.0020961110464616526 0.001544734130220605; -0.0016373088845630444 0.0015111539320724317 -0.000995892163492349] %
Mass Used: 84.49252879458163 kg
Launch C3: 113.0316959464502 km²/s²
||V∞_in||: 0.018067863334169123 km/s