A design for a Venus orbital imaging radar missionA planetary exploration mission to map the surface of Venus is discussed. A review of the Venus exploration program provides a basis for determining the probable scientific requirements for resolution, planetary coverage, etc., for such a mission. From these requirements, the range of possible mission, radar, and spacecraft functional requirements is determined and a single 'point' design is investigated in some detail. This point design, which provides full planet mapping at resolutions better than 200 meters, is based on Mariner-class spacecraft technology, including a conventional bipropellant propulsion system, currently under development, capable of delivering the required payload into a 500-km circular Venus orbit.
Document ID
19740038033
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rose, J. R.
Friedman, L. D. (California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1974
Subject Category
Space Sciences
Report/Patent Number
AIAA PAPER 74-222Report Number: AIAA PAPER 74-222
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Washington, DC
Start Date: January 30, 1974
End Date: February 1, 1974
Sponsors: American Institute of Aeronautics and Astronautics