Files
thesis/archive/ES_0.5565546677766434
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5565546677766434---------------------------
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: 2024-05-14T23:17:10.697
Launch V∞: [7.960558859839496, -5.81218132824179, 0.2031639471288138] km/s
Phase 1:
Planet: Saturn
V∞_in: [-6.364532870114473e-10, -9.237926294289154e-10, -1.1899607377445182e-9] km/s
V∞_out: [9.829864467162396e-10, -8.978278474016799e-10, 3.349943735037466e-10] km/s
time of flight: 1.8584873955044118e8 seconds
arrival date: 2030-04-04T23:56:09.697
thrust profile: [0.281796317730554 0.0035578944011281245 -0.0981309288631762; 0.07197850316398101 0.04154159705130649 -0.09028817205100675; 0.041019215054681174 0.03766101717755272 -0.0922406388961462; 0.041398433721470326 0.05141467204442501 -0.13938613282870546; 0.033599251556794954 0.05063189616646789 -0.15002498738078643; 0.019140803205260126 0.03383835490102266 -0.1158184859001496; 0.005753944392123871 0.010629123441298544 -0.039642155779810784; 0.004517010462613611 0.008976956943823888 -0.03449435509876245; 0.0017942465801876585 0.00346822656017307 -0.014709303158498829; 0.0021937080871339614 0.005397794015081407 -0.02262140561801366; 0.0005970458981319754 0.0016592488576758445 -0.002774300863391975; 1.4131224728213595e-5 0.00032150338480031553 -0.002411560402493508; -1.3068930883800142e-5 0.0010642427278510268 -0.002709602836558975; -0.00033600587264888404 0.001794483604602102 -0.0028350342560888985; -0.0003289662261814681 0.0014992429661934978 -0.004753973790767484; 1.60471548665993e-5 0.0006512845119996866 -0.001192238536598981; 0.00025451410040416167 0.00019147089246690675 -0.0027138611580069688; 0.00033945422265559545 -0.003292849662324633 0.0011592734896702238; 0.0001420113758888907 0.0023167155981203315 -0.0016052420944680696; -0.0009807991317648862 -0.0019440836875478603 -0.0008269429290343332] %
Mass Used: 82.35330140674068 kg
Launch C3: 97.19322474274456 km²/s²
||V∞_in||: 1.6353813518896267e-9 km/s