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_0.5806562413044064 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5806562413044064---------------------------
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: 2024-05-08T07:29:55.558
Launch V∞: [7.092357170929488, -7.0177353304381915, -0.7025343558047723] km/s
Phase 1:
Planet: Saturn
V∞_in: [0.0010476981680330635, -0.0015435167776550662, -0.00013724922112442355] km/s
V∞_out: [0.00010491826031998272, -0.0004839317076663024, -0.0018036612860090101] km/s
time of flight: 1.409281524162762e8 seconds
arrival date: 2028-10-25T10:12:27.558
thrust profile: [0.24616319708527098 -0.08102703766942997 -0.12100928087402452; 0.10536822551807558 0.013163989009602644 -0.13122920628986856; 0.09944885008839878 0.03382025872717212 -0.20350910338577546; 0.058473160141917134 0.02533830890019724 -0.1614615814074809; 0.05946616949240581 0.030310047444090896 -0.1998830666501313; 0.04440977582303558 0.026916915948403175 -0.1846063867743281; 0.03433243112944403 0.02279476354843604 -0.16660155634445023; 0.007794647638439383 0.004658930208415123 -0.042576057181853894; 0.01490255542504055 0.012201844792635948 -0.09625809846368107; 0.015642080620032216 0.008606355363458683 -0.07881882049811405; 0.00020244505747209 3.825900966474958e-5 -0.0008009967748996184; 0.0007550783519238717 3.649487495822139e-5 -0.0004411924591547704; 0.0007648486480407435 0.0008603812953791311 -0.010703133293257523; -0.000296657334697242 -0.0005527975078362209 -0.0010484717352855298; 0.00031513066610081703 -0.0007037754688926396 -4.014143751272624e-5; 0.00045563639231923346 1.1069596225063934e-5 -0.00035790945702984214; -7.052060227544631e-5 9.820731059993927e-5 0.0002356988011989439; 0.0001353798605851725 -9.75425877011947e-5 -0.001169984150669473; -0.0003711169867945379 0.00013768471018892818 0.00035448343707264603; 0.0008091215410499771 0.0009058641861818022 -0.00016760994476903028] %
Mass Used: 93.84406693479923 kg
Launch C3: 100.0436939292014 km²/s²
||V∞_in||: 0.0018705488079442827 km/s