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_0.5619921037365282 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5619921037365282---------------------------
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: 2024-05-18T07:42:15.882
Launch V∞: [8.112513087411893, -5.903027853029376, 0.050883158263066317] km/s
Phase 1:
Planet: Saturn
V∞_in: [-1.9146638219616535e-8, 1.6011146084952182e-7, -3.00898494794659e-8] km/s
V∞_out: [2.4210141066007615e-8, -9.357662683494502e-8, -1.254597939071607e-7] km/s
time of flight: 1.867494983361286e8 seconds
arrival date: 2030-04-18T18:33:53.882
thrust profile: [0.09959374010970921 -0.005419913835889329 -0.042407723525876684; 0.026187749976520798 0.010820098064160852 -0.03828626465348115; 0.020758601934767973 0.01269997205571679 -0.05324437087346508; 0.036160053749241944 0.027367761823330918 -0.13105535070676275; 0.02973142231761697 0.02518354506613794 -0.13889997037378488; 0.015081506194653828 0.013145486483710417 -0.0860122619439027; 0.013741051587853999 0.01409115180600086 -0.09513724417968206; 0.007867830448508311 0.007046639960152152 -0.05894211625552634; 0.0075499700455120555 0.007068634285092677 -0.0628571684715568; 0.002421666405250339 0.002344486841327364 -0.02487660543460761; 0.003929965552662755 0.0031272288607500716 -0.029501526136017184; 0.00019080304426913092 0.0011233106419523391 -0.007015848948304022; -0.0005395750339156132 -3.297902242133429e-5 0.0021351978636468504; -0.00020797347954129298 -0.001255622683471408 0.0025218964157577963; -0.0031506571978146716 0.001976614415639646 0.005003448131941278; -0.007059526719999948 -0.005762608781735962 -0.0031440039963742646; -0.0011033964902585616 -0.0076774644610849985 0.004130751247618242; -0.002540473129655542 -0.007351416502608556 -0.0005112125291468434; -0.0014486143859688888 0.002194280056772434 0.001122754927285713; 0.0024016075498460867 -0.0008784555209126383 -0.011425305218815424] %
Mass Used: 68.46714714257223 kg
Launch C3: 100.66119552286467 km²/s²
||V∞_in||: 1.64035583615805e-7 km/s