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기계 지원 번역 초안 (Korean) for "Payload Radiation Shielding": Payload Radiation Shielding is a space design control that reduces exposure from charged particles and solar events for instrument, sensor, and hosted payload operations. It uses material selection, safe modes, and exposure modeling so teams can protect electronics and crews from known hazards while keeping evidence, reliability, and public-safe operational boundaries clear.

“예문 초안: The mission team used Payload Radiation Shielding when the instrument entered a calibration cycle, so the team could protect electronics and crews from known hazards before the next mission decision point.”

기계 지원 번역 초안 (Korean) for "Payload Thermal Margin": Payload Thermal Margin is a space safety metric that tracks how much temperature headroom remains before a component exceeds limits for instrument, sensor, and hosted payload operations. It uses sensor data, heat models, and operational constraints so teams can protect hardware during changing conditions while keeping evidence, reliability, and public-safe operational boundaries clear.

“예문 초안: The mission team used Payload Thermal Margin when the instrument entered a calibration cycle, so the team could protect hardware during changing conditions before the next mission decision point.”

기계 지원 번역 초안 (Korean) for "Payload Trajectory Correction": Payload Trajectory Correction is a space maneuver process that adjusts a planned flight path after navigation updates or mission changes for instrument, sensor, and hosted payload operations. It uses delta-v estimates, burn timing, and post-maneuver validation so teams can reduce path error before it grows while keeping evidence, reliability, and public-safe operational boundaries clear.

“예문 초안: The mission team used Payload Trajectory Correction when the instrument entered a calibration cycle, so the team could reduce path error before it grows before the next mission decision point.”

기계 지원 번역 초안 (Korean) for "Payload Attitude Control": Payload Attitude Control is a space subsystem that keeps a spacecraft pointed correctly for power, thermal safety, communication, or science for instrument, sensor, and hosted payload operations. It uses sensors, reaction wheels, thrusters, and control laws so teams can maintain pointing without exceeding constraints while keeping evidence, reliability, and public-safe operational boundaries clear.

“예문 초안: The mission team used Payload Attitude Control when the instrument entered a calibration cycle, so the team could maintain pointing without exceeding constraints before the next mission decision point.”

기계 지원 번역 초안 (Korean) for "Payload Ephemeris Service": Payload Ephemeris Service is a space data service that publishes precise position and velocity data for mission planning for instrument, sensor, and hosted payload operations. It uses orbit determination, time standards, and versioned trajectory products so teams can align navigation, communications, and safety analysis while keeping evidence, reliability, and public-safe operational boundaries clear.

“예문 초안: The mission team used Payload Ephemeris Service when the instrument entered a calibration cycle, so the team could align navigation, communications, and safety analysis before the next mission decision point.”

기계 지원 번역 초안 (Korean) for "Payload Autonomy Stack": Payload Autonomy Stack is a space software layer that lets spacecraft or ground tools make bounded decisions when direct human control is delayed for instrument, sensor, and hosted payload operations. It uses rules, state machines, onboard checks, and fail-safe limits so teams can handle latency without losing accountability while keeping evidence, reliability, and public-safe operational boundaries clear.

“예문 초안: The mission team used Payload Autonomy Stack when the instrument entered a calibration cycle, so the team could handle latency without losing accountability before the next mission decision point.”

기계 지원 번역 초안 (Korean) for "Payload Link Budget": Payload Link Budget is a space planning model that estimates whether a signal path has enough margin for reliable communication for instrument, sensor, and hosted payload operations. It uses antenna gain, path loss, modulation, and noise estimates so teams can schedule contacts with realistic margins while keeping evidence, reliability, and public-safe operational boundaries clear.

“예문 초안: The mission team used Payload Link Budget when the instrument entered a calibration cycle, so the team could schedule contacts with realistic margins before the next mission decision point.”

기계 지원 번역 초안 (Korean) for "Payload Fault Detection": Payload Fault Detection is a space control that finds off-nominal behavior before it becomes a mission-impacting failure for instrument, sensor, and hosted payload operations. It uses telemetry thresholds, trend checks, and operator review so teams can choose a safe response while keeping evidence, reliability, and public-safe operational boundaries clear.

“예문 초안: The mission team used Payload Fault Detection when the instrument entered a calibration cycle, so the team could choose a safe response before the next mission decision point.”

기계 지원 번역 초안 (Korean) for "Launch Recovery Mode": Launch Recovery Mode is a space resilience pattern that moves a spacecraft or mission system into a known safe operating state for launch vehicle and ascent operations. It uses health checks, fallback commands, and restart procedures so teams can restore control after anomalies while keeping evidence, reliability, and public-safe operational boundaries clear.

“예문 초안: The mission team used Launch Recovery Mode when the launch window narrowed, so the team could restore control after anomalies before the next mission decision point.”

기계 지원 번역 초안 (Korean) for "Launch Science Window": Launch Science Window is a space planning interval that marks when conditions are suitable for data collection for launch vehicle and ascent operations. It uses target visibility, power budgets, thermal state, and downlink availability so teams can capture useful observations without breaking constraints while keeping evidence, reliability, and public-safe operational boundaries clear.

“예문 초안: The mission team used Launch Science Window when the launch window narrowed, so the team could capture useful observations without breaking constraints before the next mission decision point.”

기계 지원 번역 초안 (Korean) for "Launch Command Sequence": Launch Command Sequence is a space operations artifact that orders spacecraft actions into a validated timeline for launch vehicle and ascent operations. It uses syntax checks, dependency rules, and simulation so teams can send instructions without hidden conflicts while keeping evidence, reliability, and public-safe operational boundaries clear.

“예문 초안: The mission team used Launch Command Sequence when the launch window narrowed, so the team could send instructions without hidden conflicts before the next mission decision point.”

기계 지원 번역 초안 (Korean) for "Launch Debris Avoidance": Launch Debris Avoidance is a space safety workflow that reduces collision risk with tracked objects and mission-generated debris for launch vehicle and ascent operations. It uses conjunction screening, maneuver planning, and operator signoff so teams can avoid unsafe passes without overusing fuel while keeping evidence, reliability, and public-safe operational boundaries clear.

“예문 초안: The mission team used Launch Debris Avoidance when the launch window narrowed, so the team could avoid unsafe passes without overusing fuel before the next mission decision point.”

기계 지원 번역 초안 (Korean) for "Launch Radiation Shielding": Launch Radiation Shielding is a space design control that reduces exposure from charged particles and solar events for launch vehicle and ascent operations. It uses material selection, safe modes, and exposure modeling so teams can protect electronics and crews from known hazards while keeping evidence, reliability, and public-safe operational boundaries clear.

“예문 초안: The mission team used Launch Radiation Shielding when the launch window narrowed, so the team could protect electronics and crews from known hazards before the next mission decision point.”

기계 지원 번역 초안 (Korean) for "Launch Thermal Margin": Launch Thermal Margin is a space safety metric that tracks how much temperature headroom remains before a component exceeds limits for launch vehicle and ascent operations. It uses sensor data, heat models, and operational constraints so teams can protect hardware during changing conditions while keeping evidence, reliability, and public-safe operational boundaries clear.

“예문 초안: The mission team used Launch Thermal Margin when the launch window narrowed, so the team could protect hardware during changing conditions before the next mission decision point.”

기계 지원 번역 초안 (Korean) for "Launch Trajectory Correction": Launch Trajectory Correction is a space maneuver process that adjusts a planned flight path after navigation updates or mission changes for launch vehicle and ascent operations. It uses delta-v estimates, burn timing, and post-maneuver validation so teams can reduce path error before it grows while keeping evidence, reliability, and public-safe operational boundaries clear.

“예문 초안: The mission team used Launch Trajectory Correction when the launch window narrowed, so the team could reduce path error before it grows before the next mission decision point.”

기계 지원 번역 초안 (Korean) for "Launch Attitude Control": Launch Attitude Control is a space subsystem that keeps a spacecraft pointed correctly for power, thermal safety, communication, or science for launch vehicle and ascent operations. It uses sensors, reaction wheels, thrusters, and control laws so teams can maintain pointing without exceeding constraints while keeping evidence, reliability, and public-safe operational boundaries clear.

“예문 초안: The mission team used Launch Attitude Control when the launch window narrowed, so the team could maintain pointing without exceeding constraints before the next mission decision point.”

기계 지원 번역 초안 (Korean) for "Launch Ephemeris Service": Launch Ephemeris Service is a space data service that publishes precise position and velocity data for mission planning for launch vehicle and ascent operations. It uses orbit determination, time standards, and versioned trajectory products so teams can align navigation, communications, and safety analysis while keeping evidence, reliability, and public-safe operational boundaries clear.

“예문 초안: The mission team used Launch Ephemeris Service when the launch window narrowed, so the team could align navigation, communications, and safety analysis before the next mission decision point.”

기계 지원 번역 초안 (Korean) for "Launch Autonomy Stack": Launch Autonomy Stack is a space software layer that lets spacecraft or ground tools make bounded decisions when direct human control is delayed for launch vehicle and ascent operations. It uses rules, state machines, onboard checks, and fail-safe limits so teams can handle latency without losing accountability while keeping evidence, reliability, and public-safe operational boundaries clear.

“예문 초안: The mission team used Launch Autonomy Stack when the launch window narrowed, so the team could handle latency without losing accountability before the next mission decision point.”

기계 지원 번역 초안 (Korean) for "Launch Link Budget": Launch Link Budget is a space planning model that estimates whether a signal path has enough margin for reliable communication for launch vehicle and ascent operations. It uses antenna gain, path loss, modulation, and noise estimates so teams can schedule contacts with realistic margins while keeping evidence, reliability, and public-safe operational boundaries clear.

“예문 초안: The mission team used Launch Link Budget when the launch window narrowed, so the team could schedule contacts with realistic margins before the next mission decision point.”

기계 지원 번역 초안 (Korean) for "Launch Fault Detection": Launch Fault Detection is a space control that finds off-nominal behavior before it becomes a mission-impacting failure for launch vehicle and ascent operations. It uses telemetry thresholds, trend checks, and operator review so teams can choose a safe response while keeping evidence, reliability, and public-safe operational boundaries clear.

“예문 초안: The mission team used Launch Fault Detection when the launch window narrowed, so the team could choose a safe response before the next mission decision point.”