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_0.5632283514374797 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5632283514374797---------------------------
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: 2024-05-11T23:55:52.405
Launch V∞: [7.992144971836176, -5.518744168953493, 0.33073614939278767] km/s
Phase 1:
Planet: Saturn
V∞_in: [-2.3317513044522168e-7, 1.5169122865765429e-7, -6.622513813701018e-8] km/s
V∞_out: [3.727367953063186e-8, 2.8214307024211794e-7, -1.2611192823877265e-8] km/s
time of flight: 1.8749577787403297e8 seconds
arrival date: 2030-04-21T02:05:29.405
thrust profile: [0.5366913496841028 0.002014600151962039 -0.1532190633232118; 0.05622040990469372 0.034703542166877925 -0.0613032064227422; 0.054337571452609604 0.054633637976365494 -0.10569023812688372; 0.03590363766458118 0.04836357222017913 -0.10574202182013638; 0.029785827928057253 0.050146442689670306 -0.11965122982870591; 0.01025547210674731 0.02130165946508235 -0.056054996091793687; 0.006004927890036538 0.014839370953271987 -0.04185628918569953; 0.011259841518542328 0.031225143560092695 -0.09210468234471478; 0.0036639061365749963 0.011202739031169836 -0.03486082646504425; 0.0017363779022441736 0.007533645380788737 -0.023484168018581553; 0.00044094452417152056 0.0017253166309626857 -0.008479706263264464; 0.001019797013255545 0.003825128880906405 -0.015516526353157685; -0.007912693710962055 -0.0036383621238631537 0.0006439513014137863; -0.0029548480611552314 -0.0013800956696022552 0.005277101234785975; 0.0024900021967445007 -0.00011971354361102457 -0.015063105259516246; 0.004552757915142251 0.015571832567971861 0.003796129428118; -0.001331160669647033 -0.003485353684284556 0.0054341747378815605; -0.0017865068096347859 -0.0009503119771422729 -0.00040770897061642833; -0.00699298959087584 0.011820130428122166 -0.015269731131362409; 0.0005413796333512746 0.0017576998556398512 -0.02268283467231532] %
Mass Used: 106.19796503036196 kg
Launch C3: 94.44030485371961 km²/s²
||V∞_in||: 2.8594866537733827e-7 km/s