23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5683529377467695---------------------------
|
|
|
|
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: 2024-05-21T22:57:36.336
|
|
Launch V∞: [7.938998558754267, -6.223077409877822, -0.1355308208492254] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-2.4941290856720713e-9, -2.036445167186257e-9, -5.479822802770969e-9] km/s
|
|
V∞_out: [-5.752221217404784e-10, 1.992140423680985e-9, -2.9948217891741763e-10] km/s
|
|
time of flight: 1.8749577778627205e8 seconds
|
|
arrival date: 2030-05-01T01:07:13.336
|
|
thrust profile: [0.18119902212927455 -0.012342616055067526 -0.07961945454149796; 0.02402736946969952 0.007349584056738114 -0.03784108245134327; 0.020991648867162226 0.009087163182063712 -0.05707295836801263; 0.019511714941195878 0.00936437831847948 -0.07381653444038964; 0.016747713879516304 0.008216572423571529 -0.07941054049876099; 0.02006971041983906 0.009368652832491347 -0.11304837381391479; 0.022551994279494683 0.0134976294218203 -0.15852884294536085; 0.007321720690216808 0.002811013557430216 -0.051702627692150435; 0.007737598048799822 0.004427353938312158 -0.05730291448998908; 0.003858054356319117 0.002331324350074476 -0.041132673441330425; 0.0009209329334033629 0.0005463626454009185 -0.00879980694679669; 0.0007388420493041367 0.00011948573932932547 -0.006741426881651037; 0.0006885358842578472 0.00022178095723725488 -0.006045088136569424; 1.2809433203546567e-5 -0.00037675462526476735 -0.0016398439418283143; 0.002576348333677499 0.00072363375489734 0.0016759582022668799; -0.0019799710011973366 -0.0004258908289247558 -0.0006760094237108986; 0.001159248485482952 0.0007578512629660349 0.0008694234518505232; 0.0003469290065369242 0.0003365455751179388 -0.0023076627945924563; 0.0001188674381735612 0.00023670235373201274 0.0005893872720158012; -0.001544574544574846 -0.004746004145711425 0.00023502395755208103] %
|
|
|
|
Mass Used: 69.40399888753245 kg
|
|
Launch C3: 101.77275916863405 km²/s²
|
|
||V∞_in||: 6.355804179230221e-9 km/s
|