Files
thesis/archive/ES_0.6412772158612863
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.6412772158612863---------------------------
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: 2024-05-07T08:09:28.270
Launch V∞: [7.417266731919179, -7.487807324262945, -1.9953294128469685] km/s
Phase 1:
Planet: Saturn
V∞_in: [0.26602253016193883, -0.17749503747745166, -0.43625704280480965] km/s
V∞_out: [-0.07878630805771869, -0.5250260729728736, -0.022513993235895] km/s
time of flight: 1.0339667063231117e8 seconds
arrival date: 2027-08-17T01:27:18.270
thrust profile: [0.3523986764969214 -0.16143619363436665 -0.18606116048123544; 0.19326275212066008 -0.004401703226283951 -0.19628233691451757; 0.11335628034799676 0.019674152845443507 -0.1706566485217129; 0.06884410172661913 0.019200366846574654 -0.13574418396282545; 0.11882293970129709 0.04547463222885117 -0.2780765516789619; 0.07834699568724236 0.03396531955868793 -0.21366623838140383; 0.04844862837540214 0.022246864266110878 -0.14644177652702242; 0.02566378577781701 0.012108589975385638 -0.08336039689614144; 0.0006702554086236263 0.0007927428764504935 -0.0024963324728058105; 0.0019441628331686466 0.0008832427549582464 -0.007349386160287739; 0.00021907383961187598 0.0004366413787805504 -0.0015720204425693765; 0.0005857347870587197 0.0003671055278816616 -0.0020576412864080577; 0.0011620296042050577 0.0013905446926966868 -0.0011189879344550642; 0.00013873082501051145 0.000731830156225527 -0.0010673113333547401; 0.0007176988336225583 3.841121458007427e-5 -0.00039264581568002917; 0.0004289660873957297 -2.5358706397508196e-5 -0.0006782731573136651; 0.00035615807863094933 0.00026257000312075507 -0.0010111605149612816; 0.0009511444451010076 -0.000887074415035246 0.0006125290138119818; -0.0003542638520601589 -0.0008078475634793914 -0.0003275726458302731; -0.0005831802271086648 -0.0014680278302318384 0.0007717018450204803] %
Mass Used: 76.94749655112446 kg
Launch C3: 115.06444376349305 km²/s²
||V∞_in||: 0.5409183693309733 km/s