23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5575838509040627---------------------------
|
|
|
|
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: 2024-05-17T14:46:33.632
|
|
Launch V∞: [8.116567841765836, -5.8291111320239795, 0.09742443636618735] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-1.7284360330470226e-7, -1.145582946985739e-6, 2.718831389997487e-5] km/s
|
|
V∞_out: [1.1872144167045966e-6, -2.7230543462544425e-5, 1.989314046704148e-7] km/s
|
|
time of flight: 1.8749577779163253e8 seconds
|
|
arrival date: 2030-04-26T16:56:10.632
|
|
thrust profile: [0.14047988560939886 -0.005466190684182983 -0.05469990809860809; 0.00802698173817677 0.00360646390935442 -0.01113620159613063; 0.041218735067299145 0.027930327891427176 -0.09807579269373895; 0.05003503101902487 0.042938307900599736 -0.16849389493969752; 0.02838711277718321 0.02771068897969539 -0.12805221483567256; 0.02401843182301109 0.025501864625598846 -0.13332872529119247; 0.007391009988067581 0.008076477453631504 -0.05057380061339835; 0.0035604218149702287 0.004249160112682024 -0.028049665417328444; 0.0046529583886436455 0.005814868792543679 -0.04145103267747284; 0.00240556228569932 0.003076428968388568 -0.024690756992419637; 0.002158475110222142 0.0024044132648930005 -0.018302001836367036; -8.284871563267565e-5 -6.351756831896412e-5 0.00029634466551753174; -0.0002719710458462209 -9.747256050856177e-5 0.0019180738684161803; -1.1264144577532135e-5 -0.00015901718938317826 0.0037056792777323405; 0.0007762480057839912 0.001054469664245231 0.00019577224702807625; -0.00036898569790387467 0.00033366596915916516 -0.000559009471496875; 0.00015393328434705017 -0.0025613981046807574 0.0012616500935356519; -0.0003628245233359039 -0.0005071920574942802 -0.00017522547716714202; 0.00014108587584948928 0.00022908327340435812 0.00022043561098207; -0.003408622059620314 0.002730077776705411 0.0008393071647373502] %
|
|
|
|
Mass Used: 67.95873315313884 kg
|
|
Launch C3: 99.86670164027446 km²/s²
|
|
||V∞_in||: 2.7212986751240565e-5 km/s
|