Flight abort.

CFR · 2024-01-01 · US · Title 14

(a) (b) (1) Meets the requirements of § 450.145 if the consequence of any reasonably foreseeable failure mode in any significant period of flight is greater than 1 × 10 (2) Meets the requirements of § 450.143 if the consequence of any reasonably foreseeable failure mode in any significant period of flight is between 1 × 10 (c) (1) To ensure compliance with the safety criteria of § 450.101(a) and (b); (2) To prevent continued flight from increasing risk in uncontrolled areas if the vehicle is unable to achieve a useful mission; (3) To prevent the vehicle from entering a period of materially increased public exposure in uncontrolled areas, including before orbital insertion, if a critical vehicle parameter is outside its pre-established expected range or indicates an inability to complete flight within the limits of a useful mission; (4) To prevent conditional expected casualties greater than 1 × 10 (5) To prevent the vehicle state from reaching identified conditions that are anticipated to compromise the capability of the flight safety system if further flight has the potential to violate a flight safety limit. (6) In lieu of paragraphs (c)(2) and (4) of this section, to prevent debris capable of causing a casualty due to any hazard from affecting uncontrolled areas using a flight safety system that complies with § 450.145. (d) (1) Account for temporal and geometric extents on the Earth's surface of any reasonably foreseeable vehicle hazards under all reasonably foreseeable co

official document · source cfr-2024 · id 14:§ 450.108