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_0.5555149418109946 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5555149418109946---------------------------
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: 2024-05-14T16:16:45.227
Launch V∞: [7.886453692881989, -5.766146669242591, 0.17731826006147883] km/s
Phase 1:
Planet: Saturn
V∞_in: [-4.836910169257413e-10, -9.375329875181162e-10, -1.1582799285250461e-9] km/s
V∞_out: [9.504450631657843e-10, -9.110896323774704e-10, 3.2446331384196525e-10] km/s
time of flight: 1.8578408420707503e8 seconds
arrival date: 2030-04-03T22:58:09.227
thrust profile: [0.42007645142641625 -0.02131548891750738 -0.14069301019438915; 0.08953349621835163 0.04150785072471936 -0.11169464971176427; 0.06786122343006948 0.04954984121876103 -0.15101372550178468; 0.03674577054207439 0.033749736956093415 -0.12061690355354283; 0.022125015413372588 0.023934154012362156 -0.09634798551306989; 0.024730692216342626 0.029776021239070798 -0.1317667777392725; 0.0074123780950023236 0.009856747845124348 -0.048619156418719646; 0.002694714312697033 0.003884994057635316 -0.02125927372055324; 0.0017148813402562892 0.002663889746125444 -0.01530517929419418; 0.0005610342798146018 0.0008897162395053332 -0.005413768922161111; -6.208974296115196e-5 1.0228331061479925e-5 -0.0003640360929690432; 0.00010073726097622381 -3.56832836566312e-5 1.644789268456803e-5; -9.148431767651544e-6 9.923576995625314e-5 -0.0004964428076852081; -2.7239255440105487e-6 1.555041927077985e-5 -4.85747570741195e-5; 2.030947003099046e-6 2.4184634377666606e-5 -8.020747864168754e-5; 7.26642570323925e-5 0.00018837509337221064 -0.00039135500520177214; -0.00015038100314065543 0.00043575027422096396 -0.0005037035493860557; 0.0004557424872628663 -0.0003999451460967983 -6.622367583560193e-5; 1.2464616354565701e-5 0.0005183325062460401 2.1627829344008482e-5; 0.0003892447055876588 0.00022211057796742216 -0.0006804821734761649] %
Mass Used: 91.1571927913401 kg
Launch C3: 95.47604102654061 km²/s²
||V∞_in||: 1.5666963634869674e-9 km/s