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_0.5863064938299247 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5863064938299247---------------------------
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: 2023-05-10T18:13:05.853
Launch V∞: [6.125413616183972, -8.252970721147008, -1.0301419493951354] km/s
Phase 1:
Planet: Saturn
V∞_in: [3.069311318793241e-8, -5.789740142868467e-8, -3.130483747974621e-8] km/s
V∞_out: [1.7686136115736376e-8, -3.706450608507827e-8, 5.574922057854532e-8] km/s
time of flight: 1.8132926198024985e8 seconds
arrival date: 2029-02-06T11:27:26.853
thrust profile: [0.004637960694363234 -0.0016284977834921158 -0.0048408406879539585; 0.0042013390813392315 -0.0011835280026481372 -0.008376821277351712; 0.021356486645750055 -0.007707935333594569 -0.07115917182389314; 0.030254731449033852 -0.015676082757405996 -0.1394951024643831; 0.030226630473940877 -0.020442860164320533 -0.1721941515489541; 0.024838394594230477 -0.02037055335174785 -0.16378880380477878; 0.01575261655304219 -0.014877632020203828 -0.11538316641001416; 0.008602288582913072 -0.009013075222821765 -0.06834194363348918; 0.0023317200383223147 -0.00208905547728088 -0.01733981966051602; 0.0011389183679453318 -0.0014617721466067264 -0.006529601874786409; 0.001418508315748298 -0.0017324869612105696 -0.00909664753340993; -9.979271570508853e-5 -0.0011787145331738067 -0.006242945033347111; 0.0005203444163735014 -6.908967202324574e-5 -0.0044426772089326706; 0.0002808943531492879 -0.0002762427463111382 -0.0071193034697342415; -4.3963789449865016e-5 0.0005929486965603288 -0.004016493346689728; 0.0006457328109164274 -0.0005383023270201473 -0.0018054841393939291; 0.003139974602606478 -0.002790464028097846 -0.00045077338294739235; 0.0002681570627769132 -0.0009927099562293575 -0.0027522235670212475; -0.004831170708497218 0.004120873035236537 -0.004676358904114665; 0.016425895528097752 -7.339227055437191e-5 -0.0017121819613615781] %
Mass Used: 61.646017047064106 kg
Launch C3: 106.69341012934538 km²/s²
||V∞_in||: 7.262347512337048e-8 km/s