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_0.558132203222415 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.558132203222415---------------------------
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: 2024-05-14T13:54:25.090
Launch V∞: [7.969705787533854, -5.808754144964638, -0.08496338896512523] km/s
Phase 1:
Planet: Saturn
V∞_in: [0.0009219179695460417, -0.0006365929055301649, -4.006216651263405e-5] km/s
V∞_out: [0.0008136893735565351, 0.00035650083611332673, -0.0006839801479211511] km/s
time of flight: 1.8450312130861324e8 seconds
arrival date: 2030-03-20T00:46:26.090
thrust profile: [0.2886408875611252 -0.006281975985375157 -0.0971406715002358; 0.07203133424839007 0.03803007623201065 -0.08726664406459218; 0.0300423966973519 0.02527563905292478 -0.06748522692166976; 0.039203567128685904 0.04353107040479151 -0.12584523763412342; 0.018190033273089126 0.025046210833938078 -0.08240954823976636; 0.017779216980222355 0.028981809142334065 -0.10305012514598029; 0.006855642127833938 0.011727012547035892 -0.04713186237388231; 0.004985759035295423 0.009612992142444095 -0.040456190973752325; 0.011528537248149123 0.026843296139644514 -0.11387143884390163; 0.005303857907738008 0.010946784270652092 -0.05102461012975205; 0.0015147569078683045 0.0036873471509268766 -0.016421636184350934; 0.0013353090238975324 0.0017932625905832003 -0.011818527656384963; 2.7964897752932234e-5 -0.0005770844420070729 -0.00018260675134456814; 0.0001406716330166251 -0.0008803774011565883 0.0006529048564887811; -0.0006046185356003716 0.00031649181506301504 -0.0021891073067602336; 0.0007791672651984635 -0.00017007086652245815 -0.002019560847288011; -5.163794752082704e-5 -0.0011109761188584234 0.0016238882882046333; 0.00024624459594821174 -0.00020498593932669193 -0.0003281669903792959; -0.000675771092055857 0.0007589094362936248 -0.0015719603324985348; -0.0008172529739657508 -0.0013853922931761802 0.0019556234053896143] %
Mass Used: 83.77475639472368 kg
Launch C3: 97.26505383395893 km²/s²
||V∞_in||: 0.0011210656747617062 km/s