23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5634070027207263---------------------------
|
|
|
|
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: 2023-04-30T01:50:48.172
|
|
Launch V∞: [6.370032804858611, -7.435426427374005, 0.21997036641068735] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-1.7251782833286014e-8, 2.7701797133292265e-8, 1.8727358204618386e-8] km/s
|
|
V∞_out: [-9.603442233526822e-9, 2.0172446001937892e-8, -3.174726869582695e-8] km/s
|
|
time of flight: 1.8403151077044228e8 seconds
|
|
arrival date: 2029-02-27T01:42:38.172
|
|
thrust profile: [0.3716017678789225 -0.09633859183112047 -0.12618092989643753; 0.058058765637696 0.016498453463243322 -0.06032199770220936; 0.06112282926232205 0.03351786194032604 -0.10537066045846076; 0.059552702676188285 0.04409891047131167 -0.14231017251835876; 0.04112719210262032 0.037170913839122244 -0.12668210245852854; 0.023985658613501423 0.025481995449985355 -0.09081662821928295; 0.02652105900614783 0.03043711511142605 -0.1172689379474093; 0.023596724688223013 0.03035697557815402 -0.11950531382681685; 0.004568889128204435 0.006437495141723423 -0.027978136643954522; 0.0008487410324708608 0.0015777171131553993 -0.002966659121830925; 0.0011067770638780799 0.0010022678504980815 -0.005510796317605885; 8.014941169894423e-5 0.0022710712688263435 -0.0024888381848175963; 0.0005447036964950013 0.0007283854268336787 -0.005592148313370216; 0.001319432891576962 -0.0010450206921100305 -0.002219926394375048; 0.0005224739270857919 0.0012339958492807097 -0.0019253185167919858; -0.0004417174087472856 -0.0034142261354485294 -0.0003383604319506005; -0.0006297277566321617 -0.003308808684000451 0.003132503534959771; 0.0014085088562409242 -0.0017019822428872553 -0.0005307588168698121; -0.0023612505065142156 -0.006775514422243373 -0.0010547937290687744; 0.0010252400772815574 0.0028300528097433826 -0.0019480078894427084] %
|
|
|
|
Mass Used: 97.82575535938213 kg
|
|
Launch C3: 95.91127105396546 km²/s²
|
|
||V∞_in||: 3.762615474194817e-8 km/s
|