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_0.7445752848175967 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.7445752848175967---------------------------
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: 2023-04-25T12:58:05.042
Launch V∞: [7.349230851010424, -9.073122752782933, -2.7247516382045367] km/s
Phase 1:
Planet: Saturn
V∞_in: [-0.01627815439089098, 0.0960698989581768, -0.10029530209517624] km/s
V∞_out: [0.09529031660289092, 0.08443575683679136, 0.05782371163189639] km/s
time of flight: 8.358852471034905e7 seconds
arrival date: 2025-12-18T00:00:09.042
thrust profile: [0.2641848875444481 -0.20070489898756425 -0.09784425268974993; 0.197911973935459 -0.052691299619987565 -0.09278263233965559; 0.13226045842864786 -0.007884939473958592 -0.07938746012120451; 0.07769648032168099 0.0037348166938150616 -0.059054036569024373; 0.03752665543531245 0.0041579301232816945 -0.03472820989843579; 0.011012991804463306 0.0015213005107382977 -0.011535590799021812; 0.001307131800361793 0.00020481968286322332 -0.001535145230498401; 0.000750279671142511 8.304528101337663e-5 -0.0008497428539980856; 0.0007588739495077094 -0.0002618350041554945 -0.0009782921957597296; 0.0006746463322574797 0.0004778834586427436 -0.0006615427323143295; 0.0005957514088918199 3.2064477810664674e-5 -0.0006411139228747888; 0.0007161060632954867 0.00011233343460686281 -0.0006399413327732891; 0.0006489049502006979 0.00020983763573463116 -0.0002111716741640095; 0.0002969664154361147 -6.712198873714962e-5 -0.0005546843965028549; 0.00029286145315720756 1.9267904928838844e-5 -0.0006473781330993099; -0.00039472575528514694 0.0001154659527874489 -0.0010959935626489055; -6.780322216921829e-5 0.00028203074383132304 -0.0005946166321515191; 0.000721031844481154 -0.00046531427776177916 -0.00113421129123107; -0.00043913092121699356 8.167394744720954e-5 -0.0006852439095800284; 0.00015318798569224587 -5.3728308836256276e-5 -0.000300414663519779] %
Mass Used: 30.088536829809982 kg
Launch C3: 143.75702207840905 km²/s²
||V∞_in||: 0.1398340138112707 km/s