23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5560023625989194---------------------------
|
|
|
|
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: 2024-05-15T06:34:46.393
|
|
Launch V∞: [8.019768550322814, -5.762585550766168, 0.15592824132622102] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [2.5397457769996804e-7, 1.79859652476901e-6, -3.795133629857484e-5] km/s
|
|
V∞_out: [-1.6182366639426836e-6, 3.79366641569337e-5, -4.587397153004402e-7] km/s
|
|
time of flight: 1.8575911038327533e8 seconds
|
|
arrival date: 2030-04-04T06:19:56.393
|
|
thrust profile: [0.2932666836496181 -0.01127882232179828 -0.10388398643169922; 0.04120691869588206 0.01967251708117255 -0.05154606938094552; 0.033674926163999086 0.025014252895920883 -0.0767826687184777; 0.037689131354553894 0.03614401336451646 -0.12315711774590254; 0.031051299498785052 0.034434984424217906 -0.13258811839182447; 0.01655970843213068 0.021474705746660414 -0.09222980426779685; 0.01049487537677418 0.013874083890883876 -0.06693379488480816; 0.011094537508937123 0.01967682073210263 -0.09382542533317158; 0.005952188684591435 0.011493125496033695 -0.054673176780492945; 0.000660621520467849 0.0009910740975231736 -0.0059534464524647205; 0.000232208780465853 0.000398464208772207 -0.002206355718936093; 0.0003943354523319499 3.16418906137669e-5 -0.0021414276319304693; 2.093281856220758e-5 2.6129636005569296e-5 -8.078960795866518e-6; 0.0003693299385592538 7.414781677347502e-5 -0.0010191500192014773; 0.00023664881841307196 6.253126493881319e-5 -0.0005935132984557998; 0.0007073775979540668 4.0786655041411506e-5 -0.0003182305673431377; 0.00011229044146784778 0.00029861110859407867 -5.189931865070917e-5; -0.00021907177799839787 0.0001355462961031466 0.00015916691965242613; -0.0003131245683582538 0.0016190785013516507 -0.0005917641706069743; -0.00043890199740328687 -8.119840112083315e-5 -0.0012534850045604429] %
|
|
|
|
Mass Used: 79.6371279240534 kg
|
|
Launch C3: 97.54839344708901 km²/s²
|
|
||V∞_in||: 3.799478094939558e-5 km/s
|