Flight safety limits analysis.

CFR · 2024-01-01 · US · Title 14

(a) (b) (1) All time delays, as established by the time delay analysis of § 417.221; (2) Residual thrust remaining after flight termination implementation or vehicle breakup due to aerodynamic and inertial loads; (3) All wind effects; (4) Velocity imparted to vehicle fragments by breakup; (5) All lift and drag forces on the malfunctioning vehicle and falling debris; (6) All launch vehicle guidance and performance errors; (7) All launch vehicle malfunction turn capabilities; and (8) Any uncertainty due to map errors and launch vehicle tracking errors. (c) (d)

official document · source cfr-2024 · id 14:§ 417.213