23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5727895791564782---------------------------
|
|
|
|
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: 2024-05-07T22:44:09.476
|
|
Launch V∞: [7.229159222937927, -6.70671381726863, -0.40020011824693713] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-5.291055646039621e-6, 1.4303486235962972e-5, 7.548955758115113e-6] km/s
|
|
V∞_out: [1.1514412123240558e-5, -1.0756605336333825e-5, -6.419863802823845e-6] km/s
|
|
time of flight: 1.504794237954207e8 seconds
|
|
arrival date: 2029-02-12T14:34:32.476
|
|
thrust profile: [0.3293536428938134 -0.09222736072972149 -0.14041127564818376; 0.10215126592785018 0.020103316140315557 -0.1209001290611527; 0.10402804754311769 0.04355955441390767 -0.20326462956473662; 0.08522123833448486 0.04705830023546483 -0.22941134503686758; 0.054337724248739734 0.035220011656006835 -0.18589098832515646; 0.04693063676299524 0.034379100582282995 -0.19238338965604082; 0.022273734161053823 0.017649388509493817 -0.10523974189033763; 0.008997399667732584 0.005534570771010108 -0.046746658002431545; 0.006440412075196534 0.005278437677451233 -0.041269392256310614; 0.001272133752726732 0.0011925741166845909 -0.007843957471118495; 0.00021609154217664545 0.001243740605132279 -0.007612745530141891; 0.0045934556763167315 0.0013464844770784022 -0.0031863416195798814; 0.0020867924692537006 0.001379781888627031 -0.0039020961574995957; -0.0025379097256465286 -0.0013586387221262855 -4.3206757847046246e-5; -0.0026142396461749334 -0.0021136369679821583 0.0034231601698462904; 0.002340452436636139 -0.0026994087235915677 -0.005786593910522136; -0.0001962238760062132 -5.589436610090243e-5 0.0011114435210839114; -0.0025555139454990737 -0.005039558418520756 -0.008826917996562331; -0.006886212329660196 -0.0002618611604068479 0.0030329566136681253; -0.0013513017649467117 0.002337706439359434 -0.00031997062321075843] %
|
|
|
|
Mass Used: 100.08251399603523 kg
|
|
Launch C3: 97.40091343197533 km²/s²
|
|
||V∞_in||: 1.701680702687344e-5 km/s
|