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_0.5692558476406293 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5692558476406293---------------------------
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: 2023-04-27T08:40:51.010
Launch V∞: [5.633880156197649, -7.943926261526477, -0.11600269365720511] km/s
Phase 1:
Planet: Saturn
V∞_in: [-1.2995677307169376e-6, -8.157365883102641e-7, 5.764260702239638e-7] km/s
V∞_out: [-9.56064507763442e-7, 1.220587386407116e-6, -7.56669605194758e-7] km/s
time of flight: 1.6555753755333397e8 seconds
arrival date: 2028-07-25T12:53:08.010
thrust profile: [0.38921145485989106 -0.15305645666008857 -0.135207523519246; 0.19989917212463118 0.028590212924660408 -0.18237140179921796; 0.07837939862403902 0.03228370837362097 -0.1258044982323413; 0.04444515990458556 0.02447686009000981 -0.09546128443052955; 0.04719658147207371 0.03464374519341371 -0.12975426787233194; 0.055611138153688386 0.045363748712064715 -0.17567689173666604; 0.020113046803293632 0.0181118521926771 -0.07581786898214816; 0.028188510084376315 0.02788900178911409 -0.12048244553063914; 0.018409873787584453 0.019923979291242965 -0.08660620941978485; 0.007441027851266033 0.008652225032496939 -0.04052526438724142; 0.002898096852217737 0.0030869193391091553 -0.016104469894403298; 0.0002838077620933684 0.0008415953603163615 -0.002233193332960731; 0.0008743202075487699 -0.0006186041520622092 -0.0017445039672553662; 0.0009009714742107674 9.170191418389007e-5 -0.0017084471041705256; 0.0006966118643361155 -0.00029412383390447247 -0.001051451765731255; 0.00012154202668845134 -0.0014053742365943284 -0.0013544628042317535; 0.00019648779740484822 -0.0002556657359921381 0.0002820846263533118; -0.0016541342828193845 0.004863221865434555 -0.0010895765706620663; 2.431500047553976e-5 -0.00010021412422921735 0.0015776215009499993; 0.0008443727432217432 0.0009302631277165287 -0.002888100581427665] %
Mass Used: 110.7816665679643 kg
Launch C3: 94.86002668790341 km²/s²
||V∞_in||: 1.6390758013779235e-6 km/s