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_0.5800689299700075 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5800689299700075---------------------------
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: 2023-05-10T08:43:38.608
Launch V∞: [6.516851255442644, -7.768626277924343, 0.5462996874630618] km/s
Phase 1:
Planet: Saturn
V∞_in: [-0.0008571305533013674, 0.005320846625293723, -0.007556551688696792] km/s
V∞_out: [0.00577136191081862, 0.005366366842853193, 0.004914270238047049] km/s
time of flight: 1.8749577781413805e8 seconds
arrival date: 2029-04-18T10:53:15.608
thrust profile: [0.09784939225356239 -0.06102727772189372 -0.055484779483834075; 0.04013696381913552 -0.0268784067108107 -0.08574823513436163; 0.023361284690516577 -0.02371741128404393 -0.0861354485707763; 0.028763700289821195 -0.04136326923693718 -0.13882129000599708; 0.0244842974695379 -0.04016975722253468 -0.13579186690465098; 0.018822072962608676 -0.03242850527184326 -0.1147288717687876; 0.015659741301544614 -0.027742780337934182 -0.09909571347158709; 0.011726602885025595 -0.021344964202021345 -0.07703283550136508; 0.007777022965218061 -0.014575535473196356 -0.05255345736303811; 0.0036387027175494788 -0.007037640064390109 -0.025154372922089753; 0.0008992781580597526 -0.0017464892320586845 -0.006081540545865193; 0.00033833268084422334 -0.000585997178125846 -0.00231248765094427; 1.4048059391730952e-5 -2.344956034780622e-5 -0.000165510225560116; 1.294057627956112e-5 -1.9051956021501944e-5 -0.0001232916850977887; 7.601313410162961e-5 -0.0002264752508691726 -0.00026276404781561135; -1.835088176483679e-5 8.607562214386292e-5 -4.177461096007142e-5; 8.559359596742609e-5 -1.3776348420616589e-5 -4.8427108073110386e-5; 5.1244546191142566e-5 -0.00018596017508587577 -0.00025494260177678257; 4.546056881122861e-5 -0.00016870456406735136 -0.00011390062008707528; 0.0001117006095468363 -1.7933513718237247e-5 7.420555611819038e-5] %
Mass Used: 75.21755566417323 kg
Launch C3: 103.11934788014324 km²/s²
||V∞_in||: 0.009281570719401359 km/s