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_0.5575668726874371 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5575668726874371---------------------------
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: 2024-05-14T13:55:10.325
Launch V∞: [7.940142160743537, -5.940969083765449, 0.32568773265147727] km/s
Phase 1:
Planet: Saturn
V∞_in: [-6.193151239343893e-10, -9.050904902047788e-10, -1.18723169736659e-9] km/s
V∞_out: [9.91327551642007e-10, -8.818493792747185e-10, 3.3605024241746995e-10] km/s
time of flight: 1.829663599404393e8 seconds
arrival date: 2030-03-02T05:54:29.325
thrust profile: [0.12742732210605393 -0.00299007743320023 -0.04427149556920487; 0.10590389079363782 0.05571963340139605 -0.11687029836048686; 0.07387593875460575 0.06251505267662176 -0.14491407322324257; 0.046844868500088815 0.05137120919158366 -0.1354005854889806; 0.030341362751020742 0.040187901171836085 -0.11846370030150861; 0.019563184435411107 0.029963477006421498 -0.09696530146310789; 0.015256630246326107 0.025892171570614627 -0.09007926658168779; 0.007805604461315446 0.014323823332449347 -0.05402674548114576; 0.0008506360583472101 0.0017872124605037727 -0.007342591764642361; 0.00051624631804151 0.0006248181390563745 -0.003269181494140175; 0.00010587385929907204 0.0004967658692396654 -0.0026035942670340822; 0.0004007714798528703 -0.00018280227789348337 -6.6092058578956e-5; -0.00011873346545432863 0.00019520266512545878 -0.00034281059668307993; 0.0004742259902278813 0.0006840526026885846 -0.0005276425756009807; 0.0010616990467198935 -0.0010310769330490529 0.0017248401639186157; 0.0009621525658740101 -0.0021476382612995244 -0.0015179814136507721; 0.00038250453922162404 0.0007499218242820746 0.0010281470000498795; -0.0024023186436899894 0.0029703460711347873 -0.00045256138670733383; -0.0011099385221844003 0.0011360986109954802 -0.0050698547227961185; -0.0006250083454657199 -0.0020517211555856384 0.0021163425824125325] %
Mass Used: 76.22026329874734 kg
Launch C3: 98.44704368627359 km²/s²
||V∞_in||: 1.6162484714377765e-9 km/s