1. Transmission Opitimization
January 22, 2009
[John Dixon]
[Group Lead]
[Communications]

2. Lander to Earth Transmission
Distance from 200 km Parking Orbit to 440,000 km of Moon at Apogee
Minimum Power: 33 W
Frequency: 2.2 GHz
(S-Band Range)
Transmit Satellite: m
Receiver Satellite: DSN 26 m
Data Rate: 51.2 kbps
[John Dixon]
[Group Lead]
[Communications]

3. Rover to Lander Transmission
Distance from 0 m Lander to 500 m Maximum Travel
Minimum Power: Open Condition
Frequency: 2.2 GHz
(S-Band)
Transmit Satellite: m
Receiver Satellite: Lander 0.2 m
Data Rate: 51.2 kbps
[John Dixon]
[Group Lead]
[Communications]

4. Beamwidth Optimization (Backup)
[John Dixon]
[Group Lead]
[Communications]

5. Optimization Coding (Backup)
MATLAB Scripts For:
Lander Beamwidth
Lander Power Reqs
Lander Distance Reqs
Rover Beamwidth
Rover Power Reqs
Rover Distance Reqs
[John Dixon]
[Group Lead]
[Communications]

6. Resources (Backup) [John Dixon] [Group Lead] [Communications]
"Deep Space Network Home Page." Interplanetary Network Directorate (IND). Ed. Shannon McConnell. 03 Dec NASA. 21 Jan <
Duncan, John. "TELECOMMUNICATIONS." Telecommunications. Aug Jan <
[John Dixon]
[Group Lead]
[Communications]