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	Parts Listing   Following is a tabulation of parts* needed for the VagaLune SarL entry into the Google Lunar X Prize. Moon Rover (MR) Part Power (W) Mass (kg) Comments Ultra Triple Junction GaInP2/GaAs/Ge -300.000 1.760 Space Solar Panels RTAX -- 4.500 Radiation Hardened FPGA: Video, Image, Turbo Code 3U format RAD750 Compact PCI board 10.000 0.549 Radiation Hardened μP C-RAM -- -- Memory RA1000m -- 0.185 Image Camera RA2000m -- 0.250 HDTV Camera CMM1100-BD 5.760 0.006 Low-Noise Amplifier CMM0014-BD 2.600 -- High-Power Amplifier H264 IP Core -- -- Video Encoder S2002 DVB-RCS -- -- Turbo Encoder/Decoder ABSL 18650 -- -- Lithium-Ion Battery Dish Antenna -- -- Produced in-house Lunar Module (LM) Part Power (W) Mass (kg) Comments Ultra Triple Junction GaInP2/GaAs/Ge -1600.000 8.360 Space Solar Panels RTAX -- 3.000 Radiation Hardened FPGA: INS, Turbo Code 3U format RAD750 Compact PCI board 10.000 0.549 Radiation Hardened μP C-RAM -- -- Memory Motor(s) TBD -- -- Spacecraft Motors PPS1350 (original) PPS1350 (English) 1500.000 5.300 Stationary Plasma Thruster Ion Drive QA3000 -- -- Flex Accelerometer Airbags -- -- LM Airbags RGA-20 -- -- High Performancee Gyro Assembly ABSL 18650 -- -- Lithium-Ion Battery MLA -- -- Micrometer Laser Altimeter Launch Vehicle Part Power (W) Mass (kg) Comments Falcon 1e -- 1814.400 Launch Vehicle Falcon 1e Fairing -- 730.000 Volume for payload Usable Propellant -- 31300.000 Fuel   *Note: As final details of the design have not been completed, exact part numbers and exact values for power usage/production and weight may not be given.