23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5623343987519294---------------------------
|
|
|
|
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: 2023-05-02T11:23:55.631
|
|
Launch V∞: [6.575082158600776, -7.441373166601024, 0.13170793533044872] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [5.4320474078144336e-6, -4.606850354676026e-6, -5.50326576107122e-6] km/s
|
|
V∞_out: [-7.715819319061386e-6, -4.62036566077096e-6, -1.502882447215361e-7] km/s
|
|
time of flight: 1.874957778711174e8 seconds
|
|
arrival date: 2029-04-10T13:33:32.631
|
|
thrust profile: [0.12107505761404985 -0.03397597855299791 -0.045114721576389454; 0.11760376478201594 0.02764614662643727 -0.12024476342920817; 0.05616158834621218 0.023466376195372986 -0.10928994840133305; 0.08950388738224556 0.05598411118630426 -0.20434345942433071; 0.013775734754826496 0.009825399151979067 -0.050956242484493694; 0.02347370855767211 0.018251308564190643 -0.10127108057922417; 0.015135548046822938 0.012702260231685084 -0.07240238871192707; 0.014329888571580842 0.012705016733453539 -0.08606811149440115; 0.003952543628849183 0.00397068097055912 -0.02576371720234214; 0.004782985855860263 0.0068313309802375925 -0.03730284292657064; 0.0013267247416013494 0.0015953814331027578 -0.010453871525319482; 0.0015307067926673141 0.001299481520446112 -0.013964856821485573; -0.0006358802552809963 8.563320999533476e-5 0.00032850081113332177; 0.00025031615464571224 -0.00031388879614948793 8.750023986165627e-5; 2.8801319768905485e-5 0.0001815199432816167 0.00017247868893229077; 0.0010656716790245165 -0.0006122596940306847 0.0004350599497944315; -0.00042032321644297987 -0.0009766379600610444 0.0012959053811098075; 0.0005707827368364646 -0.0004706591039776186 0.0006110199039546402; 0.0007312384655965634 -0.0006697515414178358 0.0009051607661186825; -0.002825241402811987 -0.0006450013193147825 -0.0027899949752091856] %
|
|
|
|
Mass Used: 80.7554578436484 kg
|
|
Launch C3: 98.623086977189 km²/s²
|
|
||V∞_in||: 9.000896803546907e-6 km/s
|