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_0.562270572632635 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.562270572632635---------------------------
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: 2023-04-30T19:26:35.754
Launch V∞: [6.646173610948886, -7.313773895417789, 0.18909041422395753] km/s
Phase 1:
Planet: Saturn
V∞_in: [0.017357982175743955, -0.007277971771624313, 0.017602578268243844] km/s
V∞_out: [-0.017147592643447937, -0.0064693886386645695, -0.018115441266262265] km/s
time of flight: 1.8749577787468052e8 seconds
arrival date: 2029-04-08T21:36:12.754
thrust profile: [0.25150400330839795 -0.06403920035464924 -0.09027087552716258; 0.03011864472613215 0.008386376084574688 -0.033300132510374385; 0.03905807154415958 0.021100569782435873 -0.07291559338064385; 0.10989965800030027 0.0779730488170774 -0.26361968218340687; 0.02492003120122827 0.021425600869332203 -0.08404365491732817; 0.017073911683889192 0.017149322921347993 -0.07013312838698052; 0.009919128345320152 0.010466016586090098 -0.047738908394414165; 0.017294443477466507 0.023613556684107067 -0.10681707105159824; 0.01363337879288473 0.018482275575205348 -0.08812133498291273; 0.0010000052067033398 0.0014156653745113009 -0.007393651053284935; -0.0004913910764195902 0.0003137390506436778 -0.0023944947810925427; 0.0009736698477189529 -0.0002406348145768528 -0.0022754745682996955; 0.0005870168396829526 0.000580787942005432 -0.002222746886437432; 0.0014531304643678167 0.001514257573651817 -0.0012343239804361952; -0.00019244420581504204 0.0001671127061414124 -0.0006914289283447227; 0.004614360482252338 0.0017244552260759923 -0.0026614507673345445; 0.0005188685552967062 0.0003608687250409931 -0.0025843412921572; -0.0010711898627103122 0.0031975193430625144 -0.004120877733496985; 0.000937110069624261 -0.0012218105156616794 0.0005828624127811859; -0.00028123043907478607 -0.0011321222841865093 -0.0010380928255453031] %
Mass Used: 86.07344130937736 kg
Launch C3: 97.69866744491945 km²/s²
||V∞_in||: 0.025770509890408758 km/s