VagaLune SarL

Overview
About Google Lunar X Prize
About VagaLune SarL
Launch/Orbit
Rocket Specifications
Rocket Launch
Orbit Specifications
Rover/Lander
Moon Rover
Lunar Module
Landing Specifications
Communications
Link Budget
  >>   Antennae
Comm Systems
Project Execution
Pre-Launch Schedule
Launch Day Schedule
Post-Launch Schedule
Project Management
Parts Listing
Budget
Cash Flow
References
Link Budget
 
Both the Lunar Module (LM) and Moon Rover (MR) will communicate back to Earth at the Allen Telescope Array (ATA) at the Hat Creek Radio Observatory in northern California. The ATA is a SETI institute center that is allowing use of its facilities to the competition.
General Link Parameter Value Unit Power Loss/Gain (dB)
Transmit bandwidth 50 MHz --
ATA to LM/MR uplink freq 2119 MHz -38.97
LM/MR to ATA downlink freq 2278.5 MHz -39.60
Earth to Moon path length 378x106 m -171.5
Moon Parameter Value Unit Power Loss/Gain (dB)
Moon Blackbody Temp 274.5 K -127.2
MR antenna (on uplink) 0.3 (diameter) m 6.47
MR antenna (on downlink) 0.3 (diameter) m 7.10
ATA Parameter Value Unit Power Loss/Gain (dB)
ATA antenna Temp 45 K -135.1
ATA antenna (on uplink) 6.1 (diameter) m 41.21
ATA antenna (on downlink) 6.1 (diameter) m 41.84
 
Using the values above, equations and the diagram below, we estimate that to receive -80dBm of power at the ATA, our assumed 30cm dish antenna must transmit (Ptrans,dBm) -6.99 dBm or 200 μW of power.
 
Earth to Moon Picture of Link
The above diagram shows the link between the Earth and the Moon and the relative parameters used in the link budget calculations (for the Matlab file linked below). The uplink and downlink frequencies were chosen (S-band) because they were successfully used in information transmissions on the Apollo missions. Below is a listing of the various equations used to help in calculating the link budget for this system.
Link Equations used for the above system
Equation 1 is a restatement of the Shannon Channel Capacity. Equations 2 and 3 are variations of the Friis Link Equation (in decibel format). Equation 4 gives the gain for an antenna dependent on the physical area and efficieny. Equation 5 calculates the noise power dependent on object temperature. Equation 6 gives the signal-to-noise ratio (SNR) used for equation 1. Notice that it is a ratio of powers in Watts and not a decibel value. Equations 7 and 8 are the constants used for free-space speed of light and the Stefan-Boltzman constant, respectively.
M-File to determine various link budget parameters