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_0.5622713421176451 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5622713421176451---------------------------
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: 2023-05-02T20:09:49.494
Launch V∞: [6.381661204829912, -7.51075049993692, 0.06103607441781251] km/s
Phase 1:
Planet: Saturn
V∞_in: [-8.936033544339337e-8, -2.0165306672367802e-8, 2.4609555421155267e-8] km/s
V∞_out: [-9.5480678575095e-8, 8.869575307401635e-9, -1.1653547581322652e-8] km/s
time of flight: 1.859758761557726e8 seconds
arrival date: 2029-03-24T08:07:45.494
thrust profile: [0.30609497275908826 -0.08256498650154433 -0.11725973209206536; 0.05022726491584107 0.011062096538968174 -0.06054760283385328; 0.04945981389460413 0.02204204662244788 -0.0996458323938194; 0.048874536269117586 0.029550366629649483 -0.1369637061015384; 0.03916847654016376 0.028034334408271543 -0.13954437444411072; 0.03641117287107599 0.030724616214882983 -0.16433578167994742; 0.013942762839751984 0.012003754738606532 -0.07164857677139962; 0.013521469186366776 0.012604681506578468 -0.07875916251670254; 0.002032066697059252 0.0027709420537560974 -0.01701530552244698; 0.0014272157998423869 0.0012936802262800279 -0.00836213660389509; 0.0012685711669610921 0.0007919852104000287 -0.004753822431355758; 0.0006324041360810137 -0.0007472812843006914 -0.004715184291694766; 0.00021186747013838978 0.00012726321840469525 -4.187590260701845e-5; 0.0018827640034082735 -0.0001676802609575917 -0.0015206237092947666; 0.0005389487036115576 -0.0017962298680046554 -0.0017482858628699268; -0.00025730112031272293 0.0005981088878056989 -0.0005453541457697158; 0.000491965988777078 0.002245477307160608 -0.004520848614230201; 0.0006310598663743748 2.937078009150173e-5 -0.00269215382855769; -0.0013914086618610618 0.0020487458742145604 -0.00030516931471572884; -0.0001289636630923742 0.0007854934335287274 -0.0009540022420839415] %
Mass Used: 89.32915959108641 kg
Launch C3: 97.14069820791421 km²/s²
||V∞_in||: 9.485536021634908e-8 km/s