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_0.5644152901617425 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5644152901617425---------------------------
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: 2023-04-30T14:23:27.604
Launch V∞: [6.448172548937218, -7.4242345383264094, 0.1318043799194211] km/s
Phase 1:
Planet: Saturn
V∞_in: [0.024920054299754153, -0.011016190554208176, 0.026299217863841092] km/s
V∞_out: [-0.023191936974389107, -0.00965120503839515, -0.028333397637971828] km/s
time of flight: 1.8437413063244766e8 seconds
arrival date: 2029-03-03T13:25:37.604
thrust profile: [0.2983279150024791 -0.08461109287926542 -0.10604742951586407; 0.0909311170393989 0.026540062463185684 -0.10634582502435129; 0.05305405747449945 0.025926416936319096 -0.10310816956898226; 0.05653288211073051 0.03733079971329946 -0.14300155385768243; 0.03317380288945887 0.02578232915727097 -0.11608674346585274; 0.027912649657182265 0.02335163295332015 -0.11035602162976564; 0.012902125538153276 0.011061268140071728 -0.06477756838018668; 0.008808705299813806 0.008627782656028317 -0.04866223747749356; 0.012605107299374294 0.010826438852098332 -0.06535122068739425; 0.007070961522033776 0.005817440355904211 -0.04241690874400454; -0.0011330511453110964 -0.0008867921646815078 -0.00292705462161961; 0.0012887890637121742 0.0014920667443190324 -0.009160151275949666; 0.003808365851630042 0.0035321414323252224 -0.02323521370627795; -0.0010516333062952985 0.0010690138544889357 -0.0016299732789763631; 0.005822715476745646 0.0002276447650251191 -0.004413100712001165; 0.002455836762875164 0.0004314406837546672 0.001889008938672054; -0.0036431254517742618 -0.0024886212572141934 -0.006570161613998961; -0.0008163134858224173 9.258510161602069e-5 -0.0012252381721221811; 0.002611387578108677 -0.0026809358728716 0.0006128493858117876; 0.006392618211457236 -0.0030967812056829965 -0.002330534571983612] %
Mass Used: 94.31040463154523 kg
Launch C3: 96.71556009551219 km²/s²
||V∞_in||: 0.037868382865909385 km/s