23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.6430067205773874---------------------------
|
|
|
|
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: 2024-05-10T22:18:37.426
|
|
Launch V∞: [7.215286873999382, -7.777071224608427, -2.5073809789105987] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-0.005882656437163301, -0.005791325115401038, 0.0042048315753133135] km/s
|
|
V∞_out: [0.0040669557574080275, -0.008082983933288795, 0.0015460636055047755] km/s
|
|
time of flight: 1.0276523579877031e8 seconds
|
|
arrival date: 2027-08-13T08:12:32.426
|
|
thrust profile: [0.4606912252115131 -0.24893695058404697 -0.28341287181085434; 0.13896338948506165 -0.016362894675169905 -0.1713913865196975; 0.0646514591225856 0.0029819486962342134 -0.12415209890317078; 0.0401662621880639 0.004717222565306664 -0.10114073252419889; 0.026522079185872932 0.003688871057742813 -0.07861840759289083; 0.022786141555627817 0.004101878961628954 -0.07209344362133042; 0.01602393837738928 0.003200036043479594 -0.05904252663678477; 0.010049374271513868 0.002192364999364951 -0.04463665953542409; 0.004626772456017855 0.0010344851238856003 -0.023338238829403488; 0.0022974660735714664 0.0002885525049165594 -0.0007105652321091608; 0.0011872175733743525 -0.00011115447254745147 -0.0029184845912654466; -0.0001323507846118072 3.1515553547601656e-5 -0.001382013587962229; 0.001308570651044563 -0.0002511811502895751 -0.0017266918636615505; 6.274544336633975e-5 -0.00022094578211201855 -0.0008317486994245161; 0.003947866984574186 -0.0006508087562172828 -0.0007895062497984839; 0.004046244816580785 0.0010643661145251211 -0.007090715170668034; -0.00011509737531119595 0.0009488051893742184 -0.0017750548464728526; -0.001971957977208487 -0.003491000074401659 0.0016082855182696565; 0.0031658926184019508 -0.0016557970853744895 0.004101972831367652; 0.0011326284060249863 0.0007986421674143121 -0.003276243043825908] %
|
|
|
|
Mass Used: 56.9985688727852 kg
|
|
Launch C3: 118.83016088014286 km²/s²
|
|
||V∞_in||: 0.009264216206821035 km/s
|