Foresail-2 Orbital Lifetime Analysis
<p>The dataset has been created with the following inputs for DRAMAs CROC.</p> <table> <tbody> <tr> <td>Inputs for DRAMA</td> <td> </td> <td>Outputs for DRAMA</td> </tr> <tr> <td>Orbital elements</td> <td> </td> <td>CROC</td> </tr> <tr> <td>Inclination</td> <td>15</td> <td>°</td> <td> </td> <td>F3. Randomly tumbling satellite</td> </tr> <tr> <td>RAAN</td> <td>0</td> <td>°</td> <td> </td> <td>Average cross section for 6U</td> <td>0.170</td> <td>m^2</td> </tr> <tr> <td>Argument of perigee</td> <td>0</td> <td>°</td> <td> </td> <td>Minimum Cross Section</td> <td>0.028</td> <td>m^2</td> </tr> <tr> <td>Drag coefficient</td> <td>2.2</td> <td>N/A</td> <td> </td> <td>Maximum Cross Section</td> <td>0.268</td> <td>m^2</td> </tr> <tr> <td>SRP coefficient</td> <td>1.3</td> <td>N/A</td> <td> </td> <td> </td> <td> </td> <td> </td> </tr> <tr> <td>Orbit Predigtion Update</td> <td>08.02.2023</td> <td> </td> <td> </td> <td> </td> <td> </td> <td> </td> </tr> <tr> <td> </td> <td> </td> <td> </td> <td> </td> <td> </td> <td> </td> <td> </td> </tr> <tr> <td>6U CubeSat with 2 folding panel + boom</td> <td> </td> <td> </td> <td> </td> <td> </td> </tr> <tr> <td>Dry mass</td> <td>14</td> <td>kg</td> <td> </td> <td> </td> <td> </td> <td> </td> </tr> <tr> <td>Main body dimensions</td> <td>0.11x0.34x0.25</td> <td>m^3</td> <td> </td> <td> </td> <td> </td> <td> </td> </tr> <tr> <td>Solar Panel X+</td> <td>0.007x0.34x0.25</td> <td>m^3</td> <td> </td> <td> </td> <td> </td> <td> </td> </tr> <tr> <td>Solar Panel X-</td> <td>0.007x0.34x0.25</td> <td>m^3</td> <td> </td> <td> </td> <td> </td> <td> </td> </tr> <tr> <td>Extended boom dimensions</td> <td>0.07x0.68x0.01</td> <td>m^3</td> <td> </td> <td> </td> <td> </td> <td> </td> </tr> <tr> <td>Magnetometer dimensions</td> <td>0.05x0.05x0.05</td> <td>m^3</td> <td> </td> <td> </td> <td> </td> <td> </td> </tr> </tbody> </table> <p> </p> <p>OSCAR simulations have been conducted with orbits with apogee varying from 15000 km to 65000 km in 5000 km steps.<br> The perigee has been varied for every apogee height from 250 km to 400 km in 50 km steps.<br> Every simulation has been done for 4 different launch dates:</p> <table> <tbody> <tr> <td>21.03.2025 12:00:00</td> <td>Spring</td> </tr> <tr> <td>21.06.2025 12:00:00</td> <td>Summer</td> </tr> <tr> <td>21.09.2025 12:00:00</td> <td>Autumn</td> </tr> <tr> <td>21.12.2025 12:00:00</td> <td>Winter</td> </tr> </tbody> </table> <p>If not specified otherwise all settings in DRAMA have been kept to the default values.</p> <p> </p>
ShareScore
44/100
Overall dataset sharing score