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_0.6114786097013363 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.6114786097013363---------------------------
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: 2024-05-07T18:00:40.778
Launch V∞: [6.953424136513991, -7.4390977364673185, -1.6727374781545443] km/s
Phase 1:
Planet: Saturn
V∞_in: [0.0004589872116713477, -0.0002429276598402826, -0.0011274066812662356] km/s
V∞_out: [-0.0005998737406470219, -0.001086150622292008, -3.4994938130208056e-5] km/s
time of flight: 1.1553077999044529e8 seconds
arrival date: 2028-01-04T21:53:39.778
thrust profile: [0.4508485793598639 -0.2176127512103883 -0.24944461062735074; 0.18012303341479144 -0.006055747990662437 -0.21263659794931117; 0.16511906967252551 0.025536661400275367 -0.3009761231742261; 0.12575871732609473 0.032648987918155264 -0.305735265299572; 0.0655952951903353 0.020567285644187108 -0.1953293757911294; 0.04877812397687888 0.018381335202039658 -0.17505547416382555; 0.006453175597608125 0.0025080638429275885 -0.0262833643197896; 0.003226071541833782 0.001275575883190813 -0.014376037005499373; 0.002489380082572425 0.0010196405345356905 -0.01197456055567128; 0.0008845993542564295 0.00030387790938639223 -0.0045015398250993046; 0.005459781983879778 0.0025242869191955987 -0.02840853802992789; 0.0005020864692912417 5.788807743954867e-5 -0.0025145895531604855; 0.00023101963969061667 -0.0008560876082369906 -0.0014178591198170903; 0.00013300288897843742 0.00010234819292520873 -0.0006559873362999457; 0.0011151188103203458 -0.0002214112925572105 -0.0016941648042166709; 0.0003624984230108854 9.197337464656352e-5 -0.0012063533414792722; 2.7386231671402573e-5 0.001296964586287346 -2.047914485765875e-5; -0.000150887871707942 -8.169045963890936e-5 0.0006935718908139021; -0.0010050506158637944 0.0015415741324672108 -0.0003670274601037237; 7.89255724815269e-6 4.1138657879940654e-5 0.0002025857034041507] %
Mass Used: 92.20976866777619 kg
Launch C3: 106.48833302579135 km²/s²
||V∞_in||: 0.0012412610254725078 km/s