Using the Shuttle for future advanced planetary missionsAdvantages of using the STS for advanced planetary missions are considered. Several factors are analyzed with relation to a proposed exploration of the Jupiter System. Information relating to a Martian expedition for retrieving surface samples and also calculations pertaining to a landing on Titan are presented. The components of the suggested Jupiter System exploration facility include an orbiter, subsatellite, deep probes, Callisto lander, Io lander, and rough landers. Data concerning the STS injection mass possibilities and Ganymede orbiter mass potential are provided.
Document ID
19770053702
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Friedman, L. D. (California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Scofield, W. (Martin Marietta Aerospace Bethesda, Md., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1977
Subject Category
Astronautics (General)
Report/Patent Number
AAS 75-275Report Number: AAS 75-275
Meeting Information
Meeting: Annual Meeting on Space shuttle missions of the 80''s