23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5747974566123688---------------------------
|
|
|
|
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: 2023-04-27T13:20:18.137
|
|
Launch V∞: [6.726065704697215, -7.2806613974106495, 0.24678751859547646] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-4.155711012637257e-8, 7.868317691182023e-8, 4.399828373352752e-8] km/s
|
|
V∞_out: [-2.53047084965871e-8, 5.1885842955658075e-8, -8.098027926524746e-8] km/s
|
|
time of flight: 1.8384908389744487e8 seconds
|
|
arrival date: 2029-02-22T10:31:41.137
|
|
thrust profile: [0.17544515367293706 -0.05068485680290517 -0.058092977662581154; 0.07235071064265487 0.01752148593874962 -0.07168459288052483; 0.12302479687825986 0.06198933069054483 -0.2023337400547829; 0.05602553914258306 0.03795576570302335 -0.13030187230820595; 0.06663728151799063 0.05417295223785613 -0.194238109782815; 0.023381079051557705 0.022464200776354772 -0.08604109056838537; 0.018368396357870825 0.019021542852586865 -0.07891884541512352; 0.005942343202044479 0.005612364963450975 -0.024841530637805004; 0.0009929338842170257 0.0008321136161707765 -0.005128461007263279; -0.006009552525847613 0.004725157967082579 -0.0002699150022949788; 0.007297666296752773 -0.0012154037012878788 -0.01049875979232836; 0.003942039205271818 -0.001654490058638498 -0.011987967492943025; -0.0015604202006814366 0.005185627817737612 -0.004217307053425043; 0.0015240502239413506 3.425246227315923e-6 -0.004135846883117827; -0.04014203805599443 0.018836541795359908 -0.02857464980402404; 0.00655191772157444 0.0038763520639076288 0.00017098219932930466; 0.04664581064472817 0.01408295570215195 -0.017172343323352605; 0.010344803160428413 -0.003939215211099715 -0.006166196550976834; 0.007725216689610167 -0.004097023795363857 0.025995125519770235; -0.008554449452701701 0.0035220698696255427 -0.02275366788694135] %
|
|
|
|
Mass Used: 97.12848247368947 kg
|
|
Launch C3: 98.30889432698415 km²/s²
|
|
||V∞_in||: 9.926673512556083e-8 km/s
|