Title :
RTGs for space exploration at the end of the 20th century
Author :
Chmielewski, Art
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
Abstract :
The use of radioisotope thermoelectric generators (RTGs) as energy conversion devices for spacecraft designed for weak-sunlight environments is discussed. The two upcoming missions Galileo and Ulysses will both use general-purpose heat source (GPHS) RTGs. Two other missions that are planned for the mid-nineties and will carry RTGs onboard are the comet rendezvous asteroid flyby (CRAF) and Cassini. Another mission that might become a program start in the last decade of the 20th century is Solarprobe, which is most likely to use modular RTGs. Several other missions that are in different planning stages that are in need of RTGs to meet their power requirements are the Mars rover sample return, planetary (Mars) penetrators, microspacecraft, and the Mars Egg. All of these missions are discussed, stressing their RTG requirements
Keywords :
space vehicle power plants; thermoelectric conversion; CRAF; Cassini; GPHS; Galileo; Mars Egg; Mars rover sample return; RTGs; Solarprobe; Ulysses; comet rendezvous asteroid flyby; energy conversion devices; general-purpose heat source; microspacecraft; planetary penetrators; radioisotope thermoelectric generators; spacecraft; Bills of materials; Earth; Gravity; Jupiter; Magnetic field measurement; Mars; Probes; Space exploration; Space vehicles; Venus;
Conference_Titel :
Energy Conversion Engineering Conference, 1989. IECEC-89., Proceedings of the 24th Intersociety
Conference_Location :
Washington, DC
DOI :
10.1109/IECEC.1989.74546