Table 1: Key Terrestrial Environment Parameters Needed Versus Engineering Systems (X) and Mission Phase (P).
X | Terrestrial Environment Parameters | P | ||||||||||
Launch Vehicle Systems (Sub-) | Winds & Gusts | Atmosph. Thermo-dynamics | Atmosph. Constit. | Sola/Thermal Radiation | Atmosph. Electricity | Clouds & Fog | Humidity | Precip.or Hail | Sea State | Severe Weather | Geologic Hazards | Mission Phase |
System | X P | X P | X P | X P | X P | X P | X P | X P | X P | X P | X | Mission Analysis |
Propulsion Engine Sizing | X | X P | P | X | X P | X | Manufacturing | |||||
Structures/Airframe | X P | X P | X | X P | P | X P | X | X P | P | Testing | ||
Performance/Trajectory/G & N | X P | X P | P | P | X P | P | P | P | P | P | P | Transportation/Ground Handling |
Aerodynamics | X P | X P | P | P | P | P | P | P | P | Roll Out/On Pad | ||
Thermal Loads/Aerodynamic Heat | X P | X P | P | X P | P | P | P | P | P | P | Pre-Launch/DOL Count | |
Control | X P | X P | P | P | X P | P | P | P | X P | Liftoff/Ascent | ||
Loads | X P | X P | P | P | P | X P | X P | Stages Recovery | ||||
Avionics | P | P | X | X | X P | P | X | P | X P | Flight | ||
Materials | X | X P | X P | X P | X | X | X | X | X | Orbital | ||
Electric Power | P | P | X | X P | X | X P | P | Descent | ||||
Optics | P | X P | X P | X | P | X P | P | X P | P | P | Landing | |
Thermal Control | P | X P | P | X P | P | P | X P | P | P | Post Landing | ||
Telemetry/Tracking/Comms | P | X P | X P | P | X P | X P | P | X P | P | X P | P | Ferry/Transport |
P | P | P | P | P | P | Facility/Special Eq | ||||||
P | P | P | P | P | P | P | Refurbishment | |||||
Mission Operations | X P | X P | X P | X P | X P | X | X P | X P | X | X P | X P | Storage |