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_0.5977677415706997 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5977677415706997---------------------------
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: 2023-04-24T05:38:09.885
Launch V∞: [5.653060278327063, -8.097547683993966, -0.5092694893144512] km/s
Phase 1:
Planet: Saturn
V∞_in: [-1.9132803143441837e-6, -0.0010344067819704635, 0.0003267047754027273] km/s
V∞_out: [0.0010265643813329893, 0.0005687066611583606, -0.0004652123360369906] km/s
time of flight: 1.5073907914630803e8 seconds
arrival date: 2028-02-01T21:36:08.885
thrust profile: [0.25374564052730103 -0.1332826455219214 -0.11745789322790351; 0.12010723802893786 0.0019821406475745264 -0.1325729071448225; 0.12188863309956832 0.027664683156499153 -0.21117248777585645; 0.11039337481735709 0.039483820854335966 -0.2554593254860309; 0.07783671758859335 0.03575276438193023 -0.2225841668911706; 0.04211123243480923 0.024174766933770887 -0.13902610618594297; 0.02054514749050947 0.015709634134541815 -0.07083595211780556; 0.03343492304449999 0.02227677000339744 -0.1394178669834246; 0.012364682470237259 0.007001995579630691 -0.03582127899044971; -0.0001978164463812054 0.010086449098529855 -0.011737187882915844; -0.01793438055135168 -0.009787567832624739 -0.005779118460067993; -0.0070532418374413324 -0.019115473940926123 -0.019114808592509015; -0.010506433075638198 0.007446837457087397 -0.018518012645822635; 0.019064343757080816 -0.034482423281060444 0.0012059137978984256; -0.020316793709405992 0.012800445577016812 -0.018239639171043553; 0.009776812110750658 -0.06682589716325403 0.044387636922934286; -0.010772547206448933 -0.014761947468033432 0.037978666603074376; -0.016583639912405784 0.0291278737479326 0.01528499140976484; 0.029965450317199775 -0.04005097327598379 0.03821463831177026; -0.050299712467098454 -0.036088337276051555 0.04402609730311666] %
Mass Used: 126.97313939588867 kg
Launch C3: 97.78672441770189 km²/s²
||V∞_in||: 0.001084775120243361 km/s