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_0.5746128528938002 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5746128528938002---------------------------
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: 2024-05-06T02:17:59.998
Launch V∞: [7.116476207502739, -6.614686183078417, -0.4433243337543846] km/s
Phase 1:
Planet: Saturn
V∞_in: [-1.3024409326172732e-8, -8.486398449767864e-9, 6.929069566538978e-9] km/s
V∞_out: [-5.983779221600116e-9, -1.139470699306042e-8, -3.7492665160703123e-10] km/s
time of flight: 1.502549398196025e8 seconds
arrival date: 2029-02-08T03:46:58.998
thrust profile: [0.5961995518255412 -0.1492390205752341 -0.20882383242272937; 0.1271186371443471 0.03422531770692585 -0.13310472826922531; 0.0998567529606582 0.0522922211226219 -0.1695054300198962; 0.06669416796841587 0.048735613864870325 -0.16007767999210343; 0.04740988409381709 0.04197488867158904 -0.14754174059622113; 0.04171463511517462 0.04225724317382311 -0.15537549815980867; 0.011790500855549474 0.012567054309717317 -0.05143720002270058; 0.049246396968812216 0.05997246538514711 -0.22458736325591458; 0.007424355433295871 0.009033566435444472 -0.039112175271640154; 0.010212264543311306 0.013008472468566411 -0.0589645494356823; 0.0008835089951066451 3.93396475890013e-5 -0.005445781142088199; -0.0028934181113190074 2.8386746662629222e-5 -0.003381309410737748; -0.000670680292531215 -0.0005547597215124927 -0.0014587530685895669; 0.0026012793955107836 -0.0007397742450684765 0.00044105559713185664; 0.0011622504501989156 0.005589812868169513 -0.0012583604863933488; -0.0010305424167004196 -0.0016794051088184297 0.0025752026233511966; -0.0013089571111058972 0.00011561330199363743 -0.0007497915573693386; -0.0003333905788261162 -0.0024777571796342113 -0.002935131092139531; 0.0034225212198047833 -0.004121974637699265 0.001702761917529248; 0.0014769941181765334 0.00012927183107580326 -0.006439994195988086] %
Mass Used: 118.57840867425102 kg
Launch C3: 94.59484337745985 km²/s²
||V∞_in||: 1.7019582897411273e-8 km/s