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_0.5680876336378602 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5680876336378602---------------------------
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: 2024-05-05T04:39:35.211
Launch V∞: [7.269784191325434, -6.034411314582767, 0.22004222752497724] km/s
Phase 1:
Planet: Saturn
V∞_in: [2.7823233471474997e-9, 1.547219906015437e-9, -3.259492032744859e-9] km/s
V∞_out: [2.553966031582303e-9, 4.863540660676852e-9, 1.5984539333567653e-10] km/s
time of flight: 1.6939920310592338e8 seconds
arrival date: 2029-09-16T19:59:38.211
thrust profile: [0.8481636080049151 -0.09741454959914819 -0.2091891118149942; 0.3199440312569588 0.15226085085292096 -0.2550295933396138; 0.08566860296486684 0.0715182449667792 -0.1261894765477567; 0.041425219758167944 0.04627924324457467 -0.08826869272766591; 0.03449078392758199 0.0479236108149764 -0.09735696642414012; 0.033355321671861865 0.054048582925067104 -0.11645689283974457; 0.017559695310984152 0.03285345719865211 -0.0753142670037185; 0.019750212699697473 0.04265335408413094 -0.10075479339031866; 0.00243916476265026 0.00604118542506306 -0.013811112474655949; 0.0024414766459414554 0.005866111704495598 -0.014192936406633275; 0.0008109759337137259 0.0021434989380200607 -0.005606104211599531; 0.0006711157492778003 0.0025053615342965343 -0.006290306930009168; 9.298253538298718e-5 0.0020688105528175473 -0.0020311899812187786; 0.0017431422089088996 0.00160869149688359 -0.003440227537905236; 0.0011563407382964843 -0.0007726067227806048 -0.0020335569451364398; 0.0012915924592648816 -0.00035376380866024727 -0.004266703690780369; -0.002398832628759692 0.0007541174157296658 -0.0008011484612007926; 0.00039440161357856595 -0.00012469977059379432 0.00015120478546951782; -0.0007712544538846366 -0.003248460370024617 -0.0010731814139319593; 0.003044483376534994 -0.0016664852159019529 -0.0019171670280380398] %
Mass Used: 141.78048525473105 kg
Launch C3: 89.31230068390387 km²/s²
||V∞_in||: 4.556259535757341e-9 km/s