Files
thesis/archive/ES_0.5977085400531784
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5977085400531784---------------------------
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: 2024-05-04T01:27:53.106
Launch V∞: [6.768873158870772, -7.016247537835063, -0.947516536868481] km/s
Phase 1:
Planet: Saturn
V∞_in: [0.000495813423119562, -0.002462972075637481, -0.002475891987126096] km/s
V∞_out: [-0.00347298830652278, -0.0004203670901944956, 0.0004357007239428386] km/s
time of flight: 1.2509324701842394e8 seconds
arrival date: 2028-04-20T21:35:20.106
thrust profile: [0.9364663387031461 -0.3904301826141752 -0.4144398718071081; 0.27066949102823545 0.02333812117307297 -0.27435295439580654; 0.14897742874416361 0.048149709639948184 -0.23895473332559058; 0.14111592181308247 0.06533150831016077 -0.2987068368520294; 0.05534926877365657 0.03174329029754172 -0.15124562594790356; 0.012215223912645469 0.007711231780052445 -0.04073830362329088; 0.036808290511135676 0.02515627346743983 -0.12321274686214508; 0.06833853277596527 0.043273295113134554 -0.22319144812797123; 0.012386042769948896 0.010267451966091516 -0.05677556679812984; 0.0027860668827288044 0.002049087576394262 -0.012509955555174942; 0.0013982828054144112 0.0013314710613007476 -0.007018664541666103; 7.354509580363057e-5 3.6956657697112256e-5 -4.732646550128876e-5; -6.732097231693684e-5 -0.0001087045491710195 0.00013466585567261811; -0.00019519658186092166 0.0005974083825763209 -0.0002539801790777447; -0.0005901205793563787 -3.926272749518092e-5 -0.00030072547130283113; 2.7301549958476852e-5 0.00014745840678965182 0.0001239214404028143; -8.251744507247895e-5 -2.4707946451009476e-5 0.00010367983877245197; 7.729759976981786e-5 4.451600627072307e-5 -0.0004751104586185491; 7.397821581728352e-5 0.00013012568449713945 -0.0008883983152210377; -0.00018271539384291007 -0.0006573081978852378 3.449542787942498e-5] %
Mass Used: 137.65819124130894 kg
Launch C3: 95.943160940697 km²/s²
||V∞_in||: 0.0035273366054050966 km/s