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_0.5862076686912056 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5862076686912056---------------------------
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: 2024-05-06T13:43:29.668
Launch V∞: [7.038382581019894, -6.993009020669396, -0.8219080995468192] km/s
Phase 1:
Planet: Saturn
V∞_in: [-1.288991158237453e-6, 1.3467876614832761e-6, -1.9892851460939926e-7] km/s
V∞_out: [-1.388387187343557e-6, 9.717151603883223e-7, 8.054744677700702e-7] km/s
time of flight: 1.3635335521815756e8 seconds
arrival date: 2028-08-31T17:39:24.668
thrust profile: [0.4065119761047128 -0.14378662515329066 -0.18713019899095573; 0.09301905353412525 0.012075018442969928 -0.10987519084562404; 0.10252537871356054 0.033495858372471383 -0.18888748008703599; 0.09741042867489035 0.04438881836579867 -0.24381318064786198; 0.089019459266825 0.04915850043330689 -0.2723911790657849; 0.03693626437646569 0.024805812648303418 -0.13521324598973203; 0.04641403452700974 0.030531838987936065 -0.19426240870530992; 0.011575663719215961 0.013156417968677059 -0.06894470488396955; 0.007332139771742151 0.004246401123449867 -0.04105201025124171; 0.001217310136205978 0.0017284204057084012 -0.011587730622516586; 0.005699594797104952 0.004359190996061731 -0.03414734469630009; 0.0014280646755045869 -7.733323245689007e-5 -0.005352502130074124; 0.0004931400990516157 -0.0027076841551218265 -8.79638631468599e-5; 0.0009468255753089603 -5.714352196120034e-5 -0.0004645793744481046; -0.005573846180309676 0.0017780275608375218 0.005034649133794763; 0.0008727021455579537 -0.00567084333002129 0.008368542493696993; 0.0008152479866979687 -0.0014689700014824372 0.0032571412248926807; 0.005364696100413162 -0.003054618688241126 0.00395882741747742; 0.0003858068367062474 -0.004650533755728113 -0.0030067290678364514; -0.0033118479390958425 0.003833130627438143 -0.009054369319802837] %
Mass Used: 105.72914504934033 kg
Launch C3: 99.11653744406847 km²/s²
||V∞_in||: 1.8748087275939976e-6 km/s