Table 3 Simulated object flight parameters at the given θ and γ
θ | γ | Landing Lat. | Landing Lon. | Flight duration | Impact speed |
|---|---|---|---|---|---|
(°) | (°) | (°) | (°) | (s) | (m/s) |
135 | −3.5 | −9.7140 | 12.5568 | 772.8858 | 486.9969 |
−3.4 | −10.8610 | 13.7908 | 797.9283 | 484.9199 | |
−3.3 | −12.7992 | 15.9083 | 839.8996 | 480.8955 | |
−3.2 | −17.9284 | 21.7818 | 951.0035 | 467.1791 | |
−3.1 | 5.8825 | −3.5119 | 6318.6523 | 492.2742 | |
315 | −3.5 | 9.1975 | −6.5992 | 759.3582 | 487.8578 |
−3.4 | 10.1045 | −7.5206 | 778.7893 | 486.3153 | |
−3.3 | 11.4627 | −8.9171 | 807.6132 | 483.7396 | |
−3.2 | 13.9916 | −11.5786 | 860.8729 | 478.1008 | |
−3.1 | 24.7709 | −24.3056 | 1093.2232 | 442.2178 | |
−3.0 | 2.2062 | 0.3725 | 7194.1372 | 494.9099 |
