23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5646553599198615---------------------------
|
|
|
|
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: 2023-04-28T07:48:10.540
|
|
Launch V∞: [6.177470081011915, -7.51506051807631, 0.0400378032791625] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-1.8640207658881653e-7, -3.921319135339572e-8, 4.8229565029929856e-8] km/s
|
|
V∞_out: [-1.9444852739964979e-7, 2.0274187107112458e-8, -2.3100375941109627e-8] km/s
|
|
time of flight: 1.8164628817808202e8 seconds
|
|
arrival date: 2029-01-28T17:06:18.540
|
|
thrust profile: [0.33291932524540946 -0.08585512869178441 -0.09276314488393302; 0.22153262079133715 0.06520621072737125 -0.17956956888023923; 0.08534982708412978 0.052130345298204595 -0.13574285831735472; 0.07601991604081536 0.06226553264640176 -0.14581150738720466; 0.04506442242162266 0.04481413471672929 -0.11388163374173424; 0.021521569015036015 0.02353746216752405 -0.07000860977003767; 0.035256274413831924 0.03590161183606798 -0.11807585575186112; 0.009185177916803886 0.013908953842595311 -0.04375407809671005; 0.005509180332445682 0.010703007482442635 -0.03371500230617058; 0.0011547743229099142 0.004481845543807996 -0.018664148563609644; 0.003623775772158129 0.007089378947165078 -0.022913550286888518; -0.00018073663307752256 0.00014176558201247144 0.0015332874003733735; 0.0007834414339167697 0.0009657143414211495 -0.0062411867516548565; -0.0012075420934947985 0.00024035205687992665 -0.0020650895929638455; 0.001514488007548731 -0.00046218547750180236 -0.0006599406215888593; 8.85899195030795e-5 0.00043955804662039954 6.477618826838461e-5; 0.0006760734791259706 -0.00014912840388218193 0.0021133331280365876; 0.000390350394829195 -0.00015558349061663176 0.00048712680007147397; 0.0027088219784397287 -0.0012114439429714015 -5.369389915200134e-5; -0.0018425699445290768 0.0008906363108824756 2.365541772358199e-6] %
|
|
|
|
Mass Used: 106.7044869691158 kg
|
|
Launch C3: 94.63887421783815 km²/s²
|
|
||V∞_in||: 1.9649300108583328e-7 km/s
|