23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5576079396588647---------------------------
|
|
|
|
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: 2024-05-13T14:00:08.509
|
|
Launch V∞: [7.919830016241076, -5.666198827471553, 0.3373488693110187] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [1.3298562812930015e-6, -1.860142853866221e-6, -1.9535941259029115e-7] km/s
|
|
V∞_out: [1.2910526521135372e-7, -6.52734330990238e-7, -2.2290091570667223e-6] km/s
|
|
time of flight: 1.8749577787647307e8 seconds
|
|
arrival date: 2030-04-22T16:09:45.509
|
|
thrust profile: [0.47804436849848353 -0.003665510280434599 -0.10480133523834283; 0.056896958566257136 0.03686877293145449 -0.05925387957427914; 0.04216062253712404 0.044149655920354906 -0.07967444180655212; 0.02936916164387737 0.040692190922008445 -0.08346150806404716; 0.02911174035254889 0.04956924583184787 -0.10759090007010984; 0.01982400761132045 0.04453030103757502 -0.10544544099976581; 0.00948193809903083 0.025762972767339867 -0.0686636826284314; 0.007041277062890843 0.022595761437264824 -0.06269351714673226; 0.003183575826687708 0.01073854878201619 -0.03229570476217034; 0.0032993361862550296 0.014151259217516527 -0.045138856379474054; 0.002914205850961293 0.010357079869108308 -0.03387434361946768; 0.0014045781048638783 0.0024248271442672215 -0.010001883970781108; -0.00030775183549393834 0.00041207767027319063 0.0006080775429369125; -0.00032181210804656246 -0.00010892018513583286 -0.0002155105505354822; 0.0009326389472003821 0.0002761898235967191 -0.000799203278525421; -0.0007118455809047396 0.0008208157537405521 -0.0001370495311541879; 0.0018553199773256395 -0.002046780512322206 -0.0005613878879793989; -0.0006735738179748526 0.0007973092321519508 -0.0011370047285352795; -0.0001708493908363617 0.000926243983455093 -0.0013285655147394983; 0.0013286577156875006 0.0011517822415736192 0.0007409422973813815] %
|
|
|
|
Mass Used: 96.70655769573386 kg
|
|
Launch C3: 94.94332089821856 km²/s²
|
|
||V∞_in||: 2.294954131518023e-6 km/s
|