23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5876701828801765---------------------------
|
|
|
|
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: 2023-04-22T14:09:34.221
|
|
Launch V∞: [5.287684590798862, -8.29599785580204, -0.31798764889378445] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-1.3445681142936726e-9, 4.6542757744533606e-10, 5.636503296126571e-9] km/s
|
|
V∞_out: [-3.6623787438099427e-9, -4.939098896184667e-9, -2.656500679888658e-9] km/s
|
|
time of flight: 1.361701660676542e8 seconds
|
|
arrival date: 2027-08-15T15:12:20.221
|
|
thrust profile: [0.4574616530084792 -0.28566825230118814 -0.21708028406506016; 0.18893667164774372 -0.017040395217775305 -0.20277057461685014; 0.12084637610010353 0.013714478869992023 -0.1990135406981672; 0.19551669549432096 0.047023196693100934 -0.4102185107483236; 0.06404890768685452 0.01980348837048263 -0.16927298456378012; 0.04314068415497713 0.015947256485400203 -0.13382962419565328; 0.053467237291627945 0.022392442592082725 -0.1834465083857183; 0.014719759864253527 0.007070729438027969 -0.0598333474220876; 0.0041827537362000445 0.0018967374460835177 -0.017102900651095945; 0.008233339265880574 0.0037733786794650094 -0.037571841571258535; 0.0011472108322006444 0.0007904229121012175 -0.005992153990644185; 0.00020834558810818414 0.0001891591560427856 -0.0020537336362127226; 0.0008556136145383923 -5.675234998340318e-5 -0.004117978642326993; 0.00021274184447811592 0.0003165225661183533 -0.0021393750359353543; -0.0035906739460122685 -0.0001961175864057627 -0.0009023602581768081; 0.0014945771931277971 0.00015800581667458965 -0.0007863150630316095; 0.0037805418205688387 -0.0024725853138127377 -0.0009013208711390104; 0.004099006289828198 0.0006617087030847355 -0.005521999297868666; -0.0009959919363125183 -0.0012434717897445388 0.0031271564506127197; -0.0018876454647498223 -0.0013681864981480792 0.001951813818385103] %
|
|
|
|
Mass Used: 120.45676810966461 kg
|
|
Launch C3: 96.88430490009277 km²/s²
|
|
||V∞_in||: 5.813317095348195e-9 km/s
|