Files
thesis/archive/ES_0.5579540971762518
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5579540971762518---------------------------
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: 2024-05-12T19:55:51.054
Launch V∞: [7.9704703081790615, -5.692515305608844, 0.03974863843171797] km/s
Phase 1:
Planet: Saturn
V∞_in: [5.360023955800101e-6, -8.72471643782298e-5, -1.4888402173619585e-6] km/s
V∞_out: [-8.499786611136771e-5, 1.2270248661866803e-5, -1.7652931157606058e-5] km/s
time of flight: 1.8564795401670197e8 seconds
arrival date: 2030-03-31T12:48:25.054
thrust profile: [0.3436945299928322 -0.001572765752768555 -0.1072410494408209; 0.063439724133125 0.03680852568289646 -0.07232289512958007; 0.10916335565583934 0.10339468292977816 -0.20784367382940558; 0.05413480413256434 0.0727595234261486 -0.16643896170221673; 0.019787058808139434 0.030683134706953014 -0.08391192279350546; 0.010106846742543956 0.01889110488742394 -0.05640436196526551; 0.004090537865594636 0.008424011331313921 -0.028525118500917563; 0.005866116140757708 0.01294601289367893 -0.044996863223633304; 0.0029433255265900547 0.007771658223263708 -0.029186043105279627; 0.0006864200739433275 0.0024379755572177435 -0.011307028253656473; 0.0008365956152359479 0.002522780184516173 -0.010365254394568684; 0.000916988734851971 0.003192249154250427 -0.013438913540236368; -0.0003599549343552235 0.001471614127495342 -0.0032100505791389576; 0.0005952830995334297 -9.068582356748533e-5 -0.0028517525545913233; -0.0008995235001749058 -3.432539185501841e-5 -0.0017099268151287705; -0.0009528260467406412 -0.00030515327447579025 0.001637122405590467; -0.0025473156142316747 0.0007252850771832198 0.002010527794846036; -0.00574310792132249 0.009238740273461658 -0.0028819402296229365; -0.0026611103251928544 0.004323749511789386 -0.00010422875027888112; -0.0005025334913632915 -0.0006077628121326266 0.0001898127293173956] %
Mass Used: 91.32732024988945 kg
Launch C3: 95.93470739241215 km²/s²
||V∞_in||: 8.74243341069375e-5 km/s