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_0.6407473237541413 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.6407473237541413---------------------------
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: 2024-05-09T05:14:05.271
Launch V∞: [6.927559417952332, -7.569090516085685, -2.2821731052152496] km/s
Phase 1:
Planet: Saturn
V∞_in: [0.015904314007761697, -0.02836591783100673, -0.038337229661424] km/s
V∞_out: [-0.043855442956137504, -0.009183353291864794, 0.022805327900470938] km/s
time of flight: 1.057960919728773e8 seconds
arrival date: 2027-09-15T17:02:16.271
thrust profile: [0.9237064659278043 -0.4619403771759089 -0.4853047668353974; 0.28137249720630453 -0.0255921381058225 -0.32711071439035005; 0.092924833614247 0.007382162301767951 -0.1725318017719568; 0.03694890755060943 0.005361486502024985 -0.09299026054602566; 0.034768658416956755 0.008370166781338109 -0.09986375406891529; 0.030723979365410464 0.01195823407506496 -0.10819513406386749; 0.003916571878015246 0.001765948779465983 -0.027672181887341905; 0.0011352105315345679 -0.0013912245754593095 -0.01626018089782727; -0.00099208683971788 -0.0018946989164626126 -0.0006130918556220208; -0.000739826992278524 -0.0035949412221354757 -0.004377842444694566; 0.0035908741793515223 0.023616008769999305 -0.022691139587619757; 0.005645989149442397 -0.002720553598768807 -0.004470752118123034; -0.002768095226340719 0.005783000708152421 -0.00253159971431767; 0.018017589795407293 0.0012579929774273512 -0.005883103277170013; 0.010238272042121074 -0.006138186545011755 0.005510960427473659; 0.008957821026866038 0.0034771473582216874 0.008384531777654006; 0.061263552455379254 -0.005195526839896145 0.03663320445704438; -0.0012310360092760639 -0.012549708834903939 0.0374209805234175; -0.06189709266413512 0.042604584260536205 -0.025680191863109995; 0.009368065093087559 -0.01108584280196948 0.015443457167088934] %
Mass Used: 103.01048297576244 kg
Launch C3: 110.49052481212614 km²/s²
||V∞_in||: 0.0502724146681426 km/s