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_0.58724946614164 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.58724946614164---------------------------
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: 2023-04-23T05:20:01.620
Launch V∞: [5.381568149174851, -8.301527803146614, -0.6220385158876829] km/s
Phase 1:
Planet: Saturn
V∞_in: [-0.0004760371522594299, 0.00022181553971162602, -0.0003866479279687488] km/s
V∞_out: [-0.00020490189288705556, 0.00047011526444789886, 0.000402879770151921] km/s
time of flight: 1.3923103546111512e8 seconds
arrival date: 2027-09-20T16:37:16.620
thrust profile: [0.3614509294605178 -0.20975072923487723 -0.16225106166692668; 0.10733791067898005 -0.004032163658307875 -0.11357273688926146; 0.13905272779349928 0.02652058072598768 -0.21641627930585952; 0.060602498343172356 0.01886443656596032 -0.12863658104068806; 0.09851324420339179 0.04086881597209262 -0.24102407401949624; 0.06361585381320023 0.03137698928067069 -0.1852710714357286; 0.04113023797451792 0.022549509623507567 -0.13792567720082696; 0.037986899770937804 0.022500124383622602 -0.1387228194393616; 0.011864846690634404 0.007140365806880642 -0.048307054861153824; 0.005346604030272115 0.0035106575403509553 -0.02314754835263354; 0.03183101377608104 0.016153462927532617 -0.1339719094787327; 0.0010621473876780882 0.00026467190267676576 -0.004821636572403318; 0.0006479487481009035 0.0004935835133503467 -0.004131653549167258; -0.0006996271070900702 0.00023236705064370855 0.0007609912003690351; -0.002100429188202211 -6.408558198607855e-5 -0.002862853701941437; -0.00040824311052360326 0.0007418167385275762 0.0033016828773880453; -0.0020371474374236464 -0.0003351761646556774 -0.004750533727767753; 0.007826882298640928 -0.006181985854725657 -0.002019967658236592; -0.005326196883693883 -0.004289382234669235 -0.00424092722491771; 0.0020297782542239196 0.003938315937414761 0.0030474129587132904] %
Mass Used: 111.92020993096276 kg
Launch C3: 98.26357152587724 km²/s²
||V∞_in||: 0.0006521580515422272 km/s