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_0.5633301254291854 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5633301254291854---------------------------
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: 2023-04-30T02:17:22.581
Launch V∞: [6.381593891391033, -7.489120448469649, 0.10666415700893167] km/s
Phase 1:
Planet: Saturn
V∞_in: [-3.351302227358847e-6, 3.08610594272355e-6, 2.538368382422998e-6] km/s
V∞_out: [4.385461128951578e-6, 2.823930314577965e-6, 9.126375164370433e-8] km/s
time of flight: 1.8326815406494915e8 seconds
arrival date: 2029-02-18T06:06:36.581
thrust profile: [0.2794207220195891 -0.06969067408558476 -0.09292788945059277; 0.07102502609412444 0.019278997725702005 -0.06967962698470848; 0.060681318602667914 0.03372887996207727 -0.10391885227522908; 0.0499991838465702 0.03782790838917552 -0.11721728819539923; 0.052733955799823304 0.05022294285218747 -0.1591069846887082; 0.035862764981822344 0.03879568549434063 -0.13046844939542385; 0.027090303123938068 0.03234874619767098 -0.1165996376723433; 0.011159587049352136 0.015509291825915643 -0.05863902077327212; 0.012036675517037252 0.01705942165697659 -0.06852160532977579; 0.0007538050452726625 0.0016678246215010792 -0.0012799665013322416; 0.0005159762191383542 0.00013646893589291183 -0.0029453069157419146; -0.00016770550145726854 0.0027098455251967804 -0.000697008848270403; 0.0006716526801971367 -0.0020473699442268224 0.0010701396215819184; -0.003295892543143541 -0.0016936571465607053 -0.0021697956717049234; -6.748917076131942e-5 0.0005104975527294891 -0.0012143955432499447; 0.00033931642219015663 0.00042841703013164886 -0.00010157115058693502; -0.004173330049637587 0.0011607751879444254 -0.0018210591795514222; -0.0010677586622255138 -0.0009848721938903711 5.2690533112338114e-5; -0.001546770464194045 0.0007294711783131865 0.0010333170992908045; -0.006207912356938863 0.0018397304530983522 -0.0019279414228789682] %
Mass Used: 92.41739591653959 kg
Launch C3: 96.82304292871599 km²/s²
||V∞_in||: 5.215226797915766e-6 km/s