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_0.567367660415866 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.567367660415866---------------------------
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: 2023-04-27T23:25:14.314
Launch V∞: [6.212353893062356, -7.625792388428856, 0.22997001301476463] km/s
Phase 1:
Planet: Saturn
V∞_in: [1.17770586991781e-7, 8.058336087631978e-7, -4.770094207087845e-8] km/s
V∞_out: [2.529730360651024e-7, -5.870142666552158e-7, 3.365292889282369e-7] km/s
time of flight: 1.7562593328444865e8 seconds
arrival date: 2028-11-19T16:24:07.314
thrust profile: [0.24071113042367578 -0.07936290839765439 -0.08488263949595222; 0.1091372099738696 0.0215828440067603 -0.11353358137631471; 0.13554203524256508 0.06011696336455055 -0.22066191305323876; 0.03755985091827349 0.02294116141875109 -0.09496179386253996; 0.03713130040164549 0.02835803541261544 -0.11794896587952877; 0.03953126787634107 0.0346663157524989 -0.1462118463555023; 0.026698021506004248 0.02832095403163545 -0.12170036316480815; 0.010596019209099531 0.010005465320776227 -0.05020553666145993; 0.008454212411456453 0.010049141195898162 -0.04972464043030901; 0.00023849201501380908 0.000575664808216666 -0.0029732852425141073; -0.0005154946100031745 0.0007771253640403205 -0.0042855886460845954; 0.00014022860086968392 0.00045037302542396134 -0.005478923394626244; -0.000996533837936589 0.0024358587101234773 -0.0009792592310063995; -0.0012797083120769123 -0.003096324936803957 -0.00418169483253769; -0.00016675103902706584 0.0012129848108144354 -0.003708903849290305; 0.0021067983617661604 -0.0018599396076427663 0.004590967268668944; 0.005374881751617927 0.005300570954310109 -0.005026849209492156; -0.007635689287305555 0.008466700252421012 -0.0015920413145680437; 0.002164415572150364 0.004982964810663032 -0.021996638016633006; -0.0025281100756669363 0.0006901085857185447 0.006256777445817368] %
Mass Used: 97.26847335462071 kg
Launch C3: 96.7989366509525 km²/s²
||V∞_in||: 8.157898602257548e-7 km/s