23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5567787762422494---------------------------
|
|
|
|
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: 2024-05-14T00:23:45.626
|
|
Launch V∞: [8.068477400617782, -5.628047046406362, 0.13230448107260975] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-1.916290968547276e-6, -1.89776113020791e-5, 0.0003739244427296238] km/s
|
|
V∞_out: [1.480035873759156e-5, -0.00037410876453076303, 4.124138384995763e-6] km/s
|
|
time of flight: 1.8749577787493765e8 seconds
|
|
arrival date: 2030-04-23T02:33:22.626
|
|
thrust profile: [0.32183193820169675 0.0012489805229971204 -0.10326640778771759; 0.061447563315034856 0.03587448214105782 -0.07170952408996066; 0.03690047968440975 0.03455496902432887 -0.07865179755466528; 0.04122913435769527 0.05145700659566763 -0.1280746785140881; 0.03001019967472108 0.04595531584435085 -0.1270471625029271; 0.022311000035355175 0.04051005017926068 -0.12204863940418383; 0.004659672730315286 0.008804132825920952 -0.032181137057565964; 0.003240880637287823 0.009135584794601956 -0.030408156951373222; 0.0031065898970564065 0.006115330310306011 -0.023356713335467565; 0.005430154514205593 0.016499335965308896 -0.06482799593045727; 0.00317061429136903 0.003791708629833139 -0.013198181109082982; 8.362870931459163e-5 0.001616347372918023 -0.006036948660823107; -3.9760797194675736e-5 0.0007689000788583899 -0.0031017523398088904; -0.00022172072204143124 0.0001640861612826618 0.0009777988546344973; -0.0003827712981388137 -4.315048533330636e-5 0.0013687196048565893; -0.0004489255139070807 -0.00037926003847571477 0.0007371783230220592; -0.0010012817766053789 -0.001729148766420185 0.0004892345532422665; 5.942854158965999e-5 -0.0002678766611274644 0.0001572261982835518; -0.0027181474060325142 -0.0021123517206462204 0.002155688347466322; 0.0006577536251311702 -0.0018351591137721083 -0.00016852865466505517] %
|
|
|
|
Mass Used: 84.95088963605258 kg
|
|
Launch C3: 96.79274559655514 km²/s²
|
|
||V∞_in||: 0.0003744106178682285 km/s
|