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_0.5628559995596367 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5628559995596367---------------------------
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: 2023-05-01T00:03:00.045
Launch V∞: [6.459774372749673, -7.375714366566673, 0.011904333918488233] km/s
Phase 1:
Planet: Saturn
V∞_in: [-2.4114543121456023e-7, -6.624595862734421e-8, 7.65455506662136e-8] km/s
V∞_out: [-2.460401877373688e-7, 6.458633430381358e-8, -2.93686003830654e-8] km/s
time of flight: 1.8600345396396342e8 seconds
arrival date: 2029-03-22T19:40:33.045
thrust profile: [0.3583528151730406 -0.09874419434852089 -0.13321516384555668; 0.0822205800087926 0.01945875375307835 -0.0951679801370989; 0.05163088493330707 0.02442440992526033 -0.1019015440046043; 0.04659016112218277 0.02959654137680646 -0.1278464769861089; 0.04190539385408142 0.03202347032986302 -0.1469272257530047; 0.021509745087444597 0.018605696255458135 -0.09258089877677071; 0.011435679333485228 0.011186669980114073 -0.058038820270841965; 0.008556664930763274 0.008892417863867658 -0.05059685730076599; 0.005042710469599654 0.0049136301411883 -0.04009988247237647; 0.012231809299063813 0.014641521880397343 -0.08802947874554186; 0.0007934987914917551 0.001542585586668741 -0.006636616741596884; 0.0007302850268101519 0.0005565201748142507 -0.0011547728717714242; -0.00014507325887259522 -0.00036737175786763585 -7.982703749677932e-5; -0.000837238614243464 0.0001584554270667834 -0.00013399822254985645; -0.000423446507273776 0.0016407885979692405 0.0006298829748472382; -0.00046870441906031246 -0.0001954808984520667 -0.00023306612389447723; -0.0027894552920873696 0.0004974849947605095 0.001267358821864135; -0.00032133611638307096 0.000492446598764205 -5.202695235123991e-5; -0.00011900845048041986 -0.0013119609187850123 0.0023415408959731273; -0.00046910833629171207 -6.898001479518754e-5 0.002292362065498293] %
Mass Used: 95.90706320270738 kg
Launch C3: 96.1299890771775 km²/s²
||V∞_in||: 2.615317712189207e-7 km/s