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_0.5772162306674139 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5772162306674139---------------------------
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: 2024-05-07T16:12:41.204
Launch V∞: [7.126140224496407, -6.780885147701116, -0.5146094597058994] km/s
Phase 1:
Planet: Saturn
V∞_in: [-0.008778584922200341, 0.004106592559459971, 0.00032024964627310165] km/s
V∞_out: [-0.007751358124280316, -0.0038069010267254093, 0.004412975549011068] km/s
time of flight: 1.4826081528219748e8 seconds
arrival date: 2029-01-17T15:46:16.204
thrust profile: [0.36724912298758333 -0.10360937578579404 -0.15251532238104734; 0.12276435054464285 0.025513036766217224 -0.13666933691312194; 0.12261930836645976 0.05367690035251572 -0.22166574533329317; 0.1029604645062957 0.06039552188864228 -0.2555779226838804; 0.05369023030307042 0.036903495711433136 -0.16992068027428675; 0.024836258877571574 0.018905672581083777 -0.09979542826706986; 0.02655876636768434 0.0173897630952521 -0.11325617694424399; 0.02669670940826095 0.017795384208697914 -0.1224919501799886; 0.0042476749515242326 0.0042991038032866805 -0.021543193222624855; 0.008632817830444513 0.0037251029154261083 -0.031123363416962535; 0.0015962766587899993 0.00168496859412004 -0.010770482462478317; -0.000800855358917104 0.001644111325237531 -0.011573705296375521; 0.0032591458211778234 -0.0011671249216230718 0.002431704004095052; -0.001461236409682004 -0.002866032407404865 0.0016795674627904666; 0.002299414047847067 -0.003137458017263942 0.007923949927347932; 0.0010819873646423506 -0.012713497313868742 0.0029891535092272875; 0.006218365083273604 0.00907525480284782 0.005625405985010102; -0.0019562685944875847 -0.0031053585841865853 0.0030663179595712413; -0.003301297957537118 0.0008106315223686733 0.017780548912265208; 0.0006254466421147766 0.0017906494094620034 -0.008607931891837459] %
Mass Used: 107.42751455312737 kg
Launch C3: 97.02710078151809 km²/s²
||V∞_in||: 0.009696917836180381 km/s