23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5719735862530898---------------------------
|
|
|
|
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: 2024-05-22T14:04:46.208
|
|
Launch V∞: [7.731998000682213, -6.276788345092118, -0.06976830801095361] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [1.0249624822505934e-5, -2.6288534435739583e-5, -7.84711670334987e-5] km/s
|
|
V∞_out: [-7.633157277751861e-5, -9.57395620485602e-6, 3.239551908232681e-5] km/s
|
|
time of flight: 1.874957778382454e8 seconds
|
|
arrival date: 2030-05-01T16:14:23.208
|
|
thrust profile: [0.47924466430888524 -0.07373672446802078 -0.1705868943998767; 0.017002104179322502 0.0023847532657508587 -0.028535446429999292; 0.031690486461979375 0.0050685072003106586 -0.09041715327576678; 0.025430487598636805 0.0024785644172975155 -0.09938021740724771; 0.02886502821938008 0.000645137045506361 -0.13356885505260757; 0.010277503375170492 -0.0005054806566715809 -0.05473860709591187; 0.014782506452346534 -0.0016871936816196386 -0.08538803473226886; 0.011162115518040791 -0.002192092530092172 -0.0745807490562611; 0.00583570453802806 -0.0017344605761247438 -0.03961164491392596; 0.0055316826637993805 -0.0014318083526092592 -0.0374341461159252; 0.000817877968025533 -0.0002737286002090715 -0.005361191800981361; 0.00010348305732642819 -5.1856734981119355e-5 -0.0005964039178113866; 0.0001567704511143718 -0.00018390275143325847 -0.0002931547440491571; -0.00029920102023330616 0.00012113678128180207 -0.0003424350430361449; -0.0003045919124951551 0.00022682167579174888 -0.00032178123285087697; 0.00017512893172931125 8.782172174634539e-5 -0.00011354442110392214; -0.0005486204326795897 0.00030075804094095796 -0.0006511559710270638; 0.0002545997003922979 1.8437350712000483e-5 0.0002662783754564887; 6.813440719028172e-5 -0.0003839474545196102 0.00033731043910635887; 0.00041669982217978116 7.587602671146936e-5 -0.00036207339131432] %
|
|
|
|
Mass Used: 88.7132436293673 kg
|
|
Launch C3: 99.18673262844071 km²/s²
|
|
||V∞_in||: 8.338984295092808e-5 km/s
|