Developed by: Jan A. King . To Be Determined. Orbit Type: Near Circular; Polar; 800 km Altitude. Omni-directional Antenna on S/C; Medium Gain Antenna at E.S. Model/Case No./Rev No.: Date Data Last …
List each major flight system element separately. Breakout non-standard cost, e.g., coordinating ground stations. Breakout separable services, e.g., DSN, etc. Passes per day and duration . Assumed …
C: ATTENUATION Tx Antenna Feeder Loss Tx Earth Station Contour Loss Tx Antenna Pointing Loss Uplink Atmospheric Loss Uplink Rain Margin Rx Earth Station Contour Loss
Lowest eyepiece position - pointing @ horizon N or S - NEWTONIAN.
Down-beam frequency re-use pattern (e.g. hexagonal, 1-in-7) Up-beam pointing method (tracking or fixed relative to sub-satellite point) Up-beam frequency re-use pattern (e.g. hexagonal, 1-in-7, etc.) …
General spacecraft maneuver requirements and frequency. Special maneuvers requirements. Rationale for maneuvers . Ephemeris requirements. Changes in viewing modes and directions per orbit, per …
Changed "Downlink" to "Uplink" at D22 in "Antenna Gain" W/S. Changed hard coded cells in "Ant. Pointing Losses" W/S for referenced cells. Fixed errors in downlink portion of worksheet.
Number of antenna elements per TRxP. Up to 256 Tx/Rx. Number of UE antenna elements. Up to 8 Tx/Rx. Device deployment. UE mobility model. Fixed and identical speed |v| of all UEs, randomly and …
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NASA
Deep-imaging particle calorimetry tech CALET (CALorimetric Electron Telescope) ATIC (Advanced Thin Ionization Calorimeter) Remote operations, precision mirror figured, optical quality and accurate …
Element Templates Modified cells that the element templates were pointing to for guardrail left and right: Modified Element Template: Modeling > Crossing Point Features > Guardrail > GUARDRAIL – LT …