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_0.6251526202443105 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.6251526202443105---------------------------
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: 2023-04-23T19:21:36.746
Launch V∞: [5.368159093763517, -8.670806508076442, -2.0080330833216316] km/s
Phase 1:
Planet: Saturn
V∞_in: [2.6509202684784094e-5, -1.775409569597736e-5, 3.6508526265577296e-5] km/s
V∞_out: [3.350904170200645e-5, 3.154602026031152e-5, 1.5257780277894097e-5] km/s
time of flight: 1.0968872731275883e8 seconds
arrival date: 2026-10-14T08:27:03.746
thrust profile: [0.6274204070957015 -0.48545131584660767 -0.3840484235888666; 0.3014680368159275 -0.06922724637160707 -0.3347715036442002; 0.14630738615888786 -0.003559619538300777 -0.2404000954823709; 0.07995693659907234 0.00696969858086167 -0.17080779350200262; 0.06262906295764063 0.009556078672423923 -0.15822474752858337; 0.02148678504107497 0.0047178743337211015 -0.0635476690239041; 0.032868669782795186 0.006978625928366613 -0.10947504783913439; 0.005258587945789746 0.0017027486288632716 -0.021093813320137683; 0.0010411521669247458 0.0005289676792634628 -0.007449108720857103; 0.0017629534627441128 -0.00042366323980381083 -0.0013125006277025044; 0.008409086355585195 0.0034903012421790493 -0.03116801611873444; -0.0008704481562714025 0.00045905311424341655 -0.0010110060948948073; 0.00030039412581933265 0.0018979180806332158 0.0013894152303222077; -3.998387570972126e-5 -0.0003267335891423886 -0.0036243385122305396; -0.0019317062537527576 -0.007099166706157395 0.002658796164972407; -0.0015634984056495742 0.0010614267981880155 0.0050939966018624825; 0.0012383896029939387 -0.0011035912228380446 -0.008418544770753674; 0.0022846286221386764 0.0013305329238082074 0.007092002955004221; -0.005429614497249022 -0.0029570443189834727 -0.00043513911057045445; -5.041958481532909e-5 0.003245502830680121 -0.001595115016911812] %
Mass Used: 99.15680616736518 kg
Launch C3: 108.03221442017092 km²/s²
||V∞_in||: 4.848523724856086e-5 km/s