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_0.5630386954889394 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5630386954889394---------------------------
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: 2023-05-02T10:11:28.809
Launch V∞: [6.500232724700241, -7.395313395981474, 0.199511313804635] km/s
Phase 1:
Planet: Saturn
V∞_in: [1.0399039392290008e-5, 1.6334187095274346e-6, 1.2370817483022961e-9] km/s
V∞_out: [-2.094010755377158e-6, 5.0216477557380635e-8, 1.0303797688055901e-5] km/s
time of flight: 1.8749577787473392e8 seconds
arrival date: 2029-04-10T12:21:05.809
thrust profile: [0.3165083211353569 -0.08845642569223303 -0.11903030328939805; 0.04976186255982653 0.010571442781769363 -0.05710818242402541; 0.043706057372160434 0.018549833031963194 -0.08458727685060038; 0.05222900262034041 0.02927225006833746 -0.1413311419013506; 0.04138108314983397 0.02735330058961902 -0.1429067910099878; 0.04005865275307787 0.02979621448570292 -0.1676318525354996; 0.017839834246242765 0.014429778369485786 -0.08713455700713976; 0.007315052794216699 0.006504494492471358 -0.04156852281235469; 0.0010160630854502452 -3.389886011779717e-5 -0.01709328300629686; 0.0011183482461770487 0.0020618366189701196 -0.012121363731939321; 0.0005709947033412154 0.0005233558475938567 -0.005451831903991694; 5.16476149830656e-5 0.0012719897498518575 -0.007460969438317179; -0.0004979337214442254 -0.002860532754933367 -0.0023096062782640603; -0.00041205909544455373 -0.00014164521636606084 -0.0011855897832203886; 0.00040565424624179917 0.0003359662354269989 -0.003030220997604806; 0.0022689211745583965 -0.0006184100069430968 0.00037188204204757617; 0.0008305039012278777 -3.642569241943752e-5 -0.005001493630325806; 0.00446272115012729 0.005064494973942322 7.832300940402242e-5; 0.004016392307752461 -0.0014976336478987478 -0.0026313664341255883; 0.006725632761672101 0.01349389663770502 -0.003382787742193063] %
Mass Used: 91.14145036152831 kg
Launch C3: 96.98349046438301 km²/s²
||V∞_in||: 1.0526541620751084e-5 km/s