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_0.6706246448529066 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.6706246448529066---------------------------
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: 2024-05-10T01:13:49.537
Launch V∞: [7.561531303351862, -7.613574285697982, -2.398681059546541] km/s
Phase 1:
Planet: Saturn
V∞_in: [-0.11960413110451108, 0.23650055982860718, -0.2956935826831073] km/s
V∞_out: [-0.20690600388974878, 0.245756936101976, -0.2334577823396604] km/s
time of flight: 9.343062915989152e7 seconds
arrival date: 2027-04-26T10:10:58.537
thrust profile: [0.9999932785025054 -0.522544602208734 -0.4928859756961482; 0.3304890931795283 -0.03482108074069687 -0.30594744848773203; 0.05813222858227802 0.005272286268952939 -0.08537290543380771; 0.04322881528430029 0.008341997491255937 -0.08015234406151656; 0.034050501769421336 0.008642670815693483 -0.0743541479955501; 0.008916880884420698 0.00282528073090198 -0.02384294557766033; 0.01240305422944762 0.004144765241825118 -0.036019546449681444; 0.007238144641812918 0.0024719819183083988 -0.021703069162770424; -1.3803583802318774e-5 -0.0001764787892558395 0.00027680108600745335; 0.004146243589336356 0.001107675517536273 -0.015054322237407635; -0.0008970337663192306 -0.0004056843715532151 0.0008333458119365215; 0.00028064833706788845 -0.0006138590118953062 -0.0004406784615683302; -3.769109239444373e-5 0.00013727898693082028 -2.4959914837721165e-5; -0.0006822716978209143 0.00015878181249450772 -0.0003607549474406275; -0.00022672409971464757 -0.0002364659764000662 -0.00016625557981838536; 0.0005695139597086195 0.0016247370005985477 0.0018935362066237079; 0.00032856822888539133 -0.0010205166684849193 0.0006229607298386059; 0.00013568782056773513 0.00044338728257200226 0.0005614717348211715; -0.0012743169505750912 3.92069888509388e-5 -0.0005197703027493366; 0.0013413064135947789 -0.0010533275587836883 0.0006257257686541023] %
Mass Used: 77.16326969016382 kg
Launch C3: 120.89693988083897 km²/s²
||V∞_in||: 0.39707978772090796 km/s