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_0.5691634930656995 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5691634930656995---------------------------
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: 2024-05-09T22:09:47.233
Launch V∞: [7.258176623512393, -6.707522017129237, -0.33739590199862163] km/s
Phase 1:
Planet: Saturn
V∞_in: [-2.177482604156834e-6, 6.814486547129813e-6, 3.4844656560954634e-6] km/s
V∞_out: [5.389228469950306e-6, -5.016361298441931e-6, -3.0170107586759246e-6] km/s
time of flight: 1.5419716701601714e8 seconds
arrival date: 2029-03-29T14:42:34.233
thrust profile: [0.32646672448336284 -0.09193289670320408 -0.14690469473055603; 0.051909429176406695 0.008921076164389362 -0.06708341490561522; 0.09474005087150209 0.03436408583546494 -0.200215596597357; 0.055116725673533276 0.025718274953350054 -0.1622237085383326; 0.05507635618618761 0.029551888628533016 -0.2034598852148481; 0.0361414954191697 0.020950940683137707 -0.1596130369422236; 0.025800549764934434 0.01570187375549111 -0.13117449750239485; 0.016424672873717322 0.01016892113021867 -0.09404624408264078; 0.007426868319811046 0.004599655569299987 -0.048507661101073615; 0.0007172059205739071 0.0005650121662733799 -0.005044157872881189; 0.0005132728080993004 0.00027623279724658495 -0.0035530527845568233; -5.2252414321295616e-5 -1.892002937517974e-5 -9.757881389125736e-5; 3.148380701912521e-5 4.7358770244629e-5 -0.0002608927346116742; -0.00021164223215124555 0.000613199468690146 -0.0003978284663663759; -5.191795801383478e-5 -0.0006732477410523749 -0.000834835952518109; 0.00019345687696705293 -2.4859400662562278e-5 -0.0006110925924232293; 0.00026483203751054545 0.00028722009261764395 -0.00038540548052798515; 0.0002530947345479563 -0.0007244877519597352 8.582570332965069e-5; -0.0001974884063600511 -0.00014215702899206777 -0.0011237643967613384; -0.0002325342980819575 -0.0001437771593008028 -0.0003592926058369828] %
Mass Used: 93.60681814212876 kg
Launch C3: 97.78581550306068 km²/s²
||V∞_in||: 7.957396452416306e-6 km/s