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_0.5734495891002759 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5734495891002759---------------------------
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: 2023-04-24T16:25:15.450
Launch V∞: [5.699994879629667, -7.969468070321092, 0.05256073005760959] km/s
Phase 1:
Planet: Saturn
V∞_in: [-7.004784152822456e-10, 4.791419520213202e-10, 2.6875017183921852e-8] km/s
V∞_out: [-1.4903744473605592e-8, -2.135988315775467e-8, -1.0766843112986925e-8] km/s
time of flight: 1.576432993167883e8 seconds
arrival date: 2028-04-22T06:13:34.450
thrust profile: [0.32611930065638467 -0.1528003533206751 -0.12568321976075342; 0.15381655193529492 0.009946008591219227 -0.15004547201890608; 0.09311099856740827 0.026598548306756762 -0.14683396211665636; 0.0887387587596783 0.03605083694777926 -0.18161153617739345; 0.07895292134706372 0.04173590770644538 -0.20318773541786167; 0.042122783115859465 0.026163081113785 -0.13296432001865185; 0.027007470810882395 0.019385116974140186 -0.09862243560880796; 0.025224125881626914 0.017346563575913503 -0.09716676931691724; 0.003673835503416004 0.0030214841283288133 -0.01772900149932569; 0.030890702005124178 0.023372510490300445 -0.13505501637378547; 0.0002163001405471291 0.00019205666906649084 -0.0013140913435996944; 0.0008718714507396715 0.0005199130211514602 -0.002498164801293504; 0.0006609394162162951 0.002843800749027599 0.000915107607965745; -0.00263026308900796 -0.0009567482724550714 9.985913658401677e-5; -0.00029617121744739496 -0.001390033104447969 0.0014505265187759516; -0.003962095508977807 -0.0039559157404281675 -0.0003169019485735372; -0.00016544444945315834 0.00019266250950566958 -0.00020812022701198994; -0.002959042259179697 0.004103720764323093 0.002798675572252547; -0.0012423402851305559 0.0013943055039169956 0.00027488911304838034; 0.0035550622929601448 -0.0024628561106842836 0.0007500053086787835] %
Mass Used: 108.99462138856188 kg
Launch C3: 96.005125582016 km²/s²
||V∞_in||: 2.688841378096815e-8 km/s