SatLife v1.0 for Satellite Tool
Kit SatLife Stand-Alone Module v1.0 |
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Environment |
Increased User Productivity Reduction in
Post-simulation data analysis activities and time Ease of administration
for large, complex scenarios Straightforward mission-specific additions to
simulation environment* Quickly cost justifies by saving weeks of work
compared to other methods |
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Description |
SatLife is a tool for predicting the orbital lifetime
of a satellite, from initial orbit through atmospheric reentry. SatLife takes
into account the satellite's initial orbit conditions, area and mass. It also
uses historical or projected solar cycle information to predict atmospheric
drag.
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| The stand alone version of SatLife can run lifetime
analyses for a family of circular orbits, with varying start dates, initial
altitudes or ballistic coefficients or for a single elliptical orbit. It
outputs the predicted lifetime to the screen and a time history of the altitude
to a file in a format compatible with most spreadsheet programs for plotting.
For circular orbits, the history consists of the altitude as a function of the
number of days on orbit. For elliptical orbits it consists of the apogee,
perigee and eccentricity as a function of the number days on orbit.
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| The STK/SatLife Module takes the initial orbit
conditions of any STK satellite and a user input ballistic coefficient. It
displays the calculated lifetime in a standard STK utility window. The time
history of the satellite's apogee, perigee and eccentricity can be displayed in
an STK Data Window, with options to save, export or print the
results. |
| SatLife uses a variable step size Euler integrator to
combine high fidelity with good performance even on high altitude orbits with
very slow decay rates. |