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_0.5622614263793988 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5622614263793988---------------------------
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: 2023-05-01T11:30:57.204
Launch V∞: [6.444128302876954, -7.3600883915110815, 0.1307379550974187] km/s
Phase 1:
Planet: Saturn
V∞_in: [0.018730145517641808, -0.008839452233519503, 0.0222227627161653] km/s
V∞_out: [-0.019408528834239176, -0.008350287951172637, -0.02182795164365419] km/s
time of flight: 1.8749577787475932e8 seconds
arrival date: 2029-04-09T13:40:34.204
thrust profile: [0.37465983134478753 -0.09918202625352252 -0.13808811538127688; 0.11154452716527846 0.02926366235939016 -0.12978979565879573; 0.04617843001867602 0.02152498202049195 -0.09140361421520632; 0.05854581257505777 0.03899433718032522 -0.16867025740789252; 0.044163712217052314 0.03429662873667663 -0.16169372910871052; 0.019314659868577548 0.01667235218009046 -0.08547663662925291; 0.010028953331269129 0.009551417860161854 -0.05304853825210166; 0.007214520079904602 0.007547444296284147 -0.044478380813141115; 0.002267338813962904 0.0022316660335397094 -0.015492735336855665; 0.001258126877951697 0.0012594620759813387 -0.008585064159035063; 0.003076249471996449 0.003687666423672229 -0.02566540761999945; 0.0008946548267130244 -0.0003026338795072596 -0.001154327861057917; 0.0008405676197728434 0.00235653133568761 -0.0016456390938711014; 0.00019013433542250358 -0.0030648551619407187 -0.0008562805544541325; -0.00010685995249799384 0.0003306017090965456 -0.0010483238895703413; -0.0031416738665265087 0.0008360610191362022 0.0005609195087243604; -0.0013531046931225064 -0.0013936732303023837 0.0014271104160929837; -0.0005959476947694445 0.0008308777715873336 0.0003669745804996817; -0.00039072603384032815 0.005041201260846629 -0.0018984332354599106; -0.0004010328061079615 -0.0013330023709763683 0.002461832851129023] %
Mass Used: 97.6354291977209 kg
Launch C3: 95.71478312769904 km²/s²
||V∞_in||: 0.03037771304163131 km/s