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The small reconnaissance of atmospheres mission platform concept, part 1: motivations and outline for a swarm of scientific microprobes to the clouds of Jupiter in 2030

Authors :
Kartheephan Sathiyanathan
Isaac DeSouza
Regina Lee
Barry Stoute
John E. Moores
Ben Quine
Jinjun Shan
K. A. Carroll
Source :
International Journal of Space Science and Engineering. 2:327
Publication Year :
2014
Publisher :
Inderscience Publishers, 2014.

Abstract

A mission concept is presented for several small atmospheric entry vehicles at Jupiter. By relaxing the requirement for substantial penetration into the Jovian atmosphere, the size of the atmospheric entry probes shrinks dramatically. Such atmospheric entry probes would experience much less heating than previous concepts of much larger (~300kg) spacecraft presented as minimum concepts and no parachutes are necessary. This reduces complexity while still permitting over 15 minutes of useable science under free-fall from above the 0.41 bar level to near the 10 bar level of the Jovian Atmosphere during which up to 20 Mbits of data could be returned per probe. By dividing the payload, the risk to the mission is substantially mitigated and ground truth may be obtained from a large part of the entire planetary atmosphere using a single launch.

Details

ISSN :
20488467 and 20488459
Volume :
2
Database :
OpenAIRE
Journal :
International Journal of Space Science and Engineering
Accession number :
edsair.doi...........a48974de1f36ef06b28f6d031446169a