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_0.5617647530993415 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5617647530993415---------------------------
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: 2024-05-13T11:10:29.965
Launch V∞: [7.651724902231536, -5.896595085749392, 0.1094439769675607] km/s
Phase 1:
Planet: Saturn
V∞_in: [4.802985910585384e-7, -4.543064137273443e-6, 8.443646550601515e-7] km/s
V∞_out: [-7.181702941249281e-7, 2.612089569459924e-6, 3.7756389644826663e-6] km/s
time of flight: 1.8129845598545155e8 seconds
arrival date: 2030-02-09T19:51:24.965
thrust profile: [0.5991579720499747 -0.052604399692311156 -0.19595976799167836; 0.1481875484435777 0.04721105890895712 -0.15758911348078597; 0.02608108089184001 0.01772842967827344 -0.05704971869388517; 0.03660279787476913 0.02796535908566907 -0.1151102400700526; 0.027434792026578246 0.02425684599732448 -0.11233958292567364; 0.012230261262505147 0.01257683365962444 -0.0636349094315521; 0.011040509389544982 0.01137281952266432 -0.06446054431455034; 0.009051824454521325 0.012802071240201591 -0.06567233562172772; 0.005720384573432606 0.006497747266968859 -0.04446969006818014; 0.005109243484628099 0.005645311017502704 -0.051029177917506975; 0.0011323923254679476 0.001539745983396562 -0.00902459955670885; 0.00043161313484871137 0.0010288866642772423 -0.005502646549232824; -0.0015941449335661892 0.0030748394346380797 -0.002807139058278448; -0.0004483287128025237 -0.0004693236201583404 0.0031007341204512687; 0.0053414344104176625 -0.003163844162986633 -0.005574438870158035; 0.004126736795850974 -0.002624122119425566 0.0010307261323338813; -0.002424782952987765 0.005905127034410456 0.004336784579971534; -0.0014422868173597989 -0.005668633173195115 -0.012048974632102366; 0.0011643560816843972 0.007315800625351898 -0.004398727726038141; -0.004192434041066236 -0.0013124446041439856 0.012670479294017946] %
Mass Used: 110.96309613118183 kg
Launch C3: 93.33070556880855 km²/s²
||V∞_in||: 4.645758297917333e-6 km/s