Expert-level spacecraft design covering mission analysis, subsystem design, power and thermal management, attitude control, communications, and systems engineering.
한국어 요약은 준비 중입니다. 원문 설명을 표시하고 있습니다.
실행 점수 미검증
설치 방법 보기설치하기 전에 에이전트에게 전달되는 지시 내용을 확인할 수 있습니다.
Requirements flow-down: mission objectives to system to subsystem requirements. Orbit selection: driven by coverage, lighting, radiation, and launch cost. Launch vehicle compatibility: mass, volume, vibration, and acoustic environments. Mission lifetime: design life drives redundancy, radiation tolerance, consumables.
Solar arrays: BOL and EOL power, degradation from radiation and aging. Battery sizing: eclipse duration times average power determines capacity. Power budget: allocate power to each subsystem with margin. Regulation: unregulated, regulated, and hybrid bus architectures.
Sensors: star trackers, sun sensors, magnetometers, gyroscopes. Actuators: reaction wheels, magnetorquers, thrusters. Control modes: detumble, sun pointing, nadir pointing, inertial pointing. Disturbance torques: gravity gradient, solar pressure, aerodynamic, magnetic.
Passive: surface coatings, MLI blankets, radiators control temperature. Active: heaters, heat pipes, louvers for tighter temperature control. Thermal math model: lumped capacitance nodes, radiation and conduction links. Temperature limits: electronics typically -20 to +70 C operational.
Link budget: transmit power, antenna gain, path loss, receiver sensitivity. Frequency bands: UHF for CubeSats, S and X band for smallsats, Ka for high rate. Data volume: payload data rate times contact time determines link requirements. Ground station network: multiple stations for coverage, commercial options.
| Pitfall | Fix |
|---|---|
| Insufficient power margin | Maintain 20% margin on power budget at all phases |
| Wrong eclipse fraction estimate | Calculate eclipse duration accurately for orbit |
| Missing single point failures | Review FMEA and add redundancy for critical functions |
| Underestimating radiation environment | Use environment models for actual orbit and lifetime |
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Expert-level abstract algebra knowledge. Use when working with groups, rings, fields, modules, Galois theory, representation theory, or algebraic structures. Also use when the user mentions 'group', 'ring', 'field', 'homomorphism', 'isomorphism', 'normal subgroup', 'quotient group', 'Sylow theorem', 'Galois theory', 'polynomial ring', 'ideal', 'module', 'vector space', or 'representation theory'.
한국어 요약은 준비 중입니다. 원문 설명을 표시하고 있습니다.
Expert-level acoustics knowledge. Use when working with sound waves, acoustic propagation, resonance, standing waves, Doppler effect, room acoustics, ultrasound, noise control, musical acoustics, or architectural acoustics. Also use when the user mentions 'sound wave', 'decibel', 'frequency', 'resonance', 'standing wave', 'Doppler effect', 'acoustic impedance', 'reverberation', 'ultrasound', 'noise control', 'harmonics', or 'sound intensity'.
한국어 요약은 준비 중입니다. 원문 설명을 표시하고 있습니다.
Expert-level aerodynamics covering subsonic and supersonic flow, lift and drag, airfoil theory, boundary layers, compressible flow, and CFD methods.
한국어 요약은 준비 중입니다. 원문 설명을 표시하고 있습니다.
Expert-level air quality engineering covering pollutant sources, atmospheric dispersion, air quality standards, emission controls, and air quality modeling.
한국어 요약은 준비 중입니다. 원문 설명을 표시하고 있습니다.
Expert-level aircraft structures covering structural design philosophy, wing and fuselage analysis, fatigue and damage tolerance, composite structures, and certification.
한국어 요약은 준비 중입니다. 원문 설명을 표시하고 있습니다.
Expert-level algorithms and complexity theory covering sorting, searching, graph algorithms, dynamic programming, greedy algorithms, NP-completeness, and algorithm design paradigms.
한국어 요약은 준비 중입니다. 원문 설명을 표시하고 있습니다.