A design for a 1984 Mars roverA Mars rover is planned for the mid-1980's as a follow-up to the Viking program, and as a prelude to a return-to-earth mission of Martian samples in the late eighties or early nineties. An overall view of the rover's configuration is presented with a summary of basic design parameters. Six subsystems are outlined: computing, with a 10 to the 8th bit bubble memory; mobility, designed for a journey of 100 km in 2 earth years; science sample acquisition, including a soil auger and hard rock drill; power, supplied by an RTG and stored in batteries; telecommunication, with 50 K bit UHF transmission relayed through an orbiter; and visual imaging, employing two television cameras, each with an 800 x 800 pixel charge coupled device. Scientific research goals include information about Martian seismic characteristics, magnetic field, surface heat flow, chemical composition, geology along a transverse, and meteorology. Attention is given to the necessity of rover autonomy from earth commands.
Document ID
19780038657
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dobrotin, B. M. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
French, J. R. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Paine, G. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Purdy, W. I. (California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Subject Category
Ground Support Systems And Facilities (Space)
Report/Patent Number
AIAA PAPER 78-81Report Number: AIAA PAPER 78-81
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Huntsville, AL
Start Date: January 16, 1978
End Date: January 18, 1978
Sponsors: American Institute of Aeronautics and Astronautics