POTENTIAL CAMPAIGN ARCHITECTURES AND MISSION DESIGN CHALLENGES FOR NEAR-TERM INTERNATIONAL MARS SAMPLE RETURN MISSION CONCEPTS

被引：0

作者：

Lock, Robert E. ^{[1
]}

Nicholas, Austin K. ^{[2
]}

Vijendran, Sanjay ^{[3
]}

Woolley, Ryan C. ^{[4
]}

Didion, Alan ^{[2
]}

Laipert, Frank ^{[5
]}

Olikara, Zubin ^{[4
]}

机构：

[1] CALTECH, Jet Prop Lab, NASA, Mars Program Formulat Off, 4800 Oak Grove Dr, Pasadena, CA 91109 USA

[2] CALTECH, Jet Prop Lab, NASA, Project Syst Engn & Formulat, Pasadena, CA USA

[3] European Space Res & Technol Ctr ESTEC, European Space Agcy, Human & Robot Explorat Directorate, Keplerlaan 1, NL-2201 AZ Noordwijk, Netherlands

[4] CALTECH, Jet Prop Lab, NASA, Inner Planets Mission Anal, Pasadena, CA USA

[5] CALTECH, Jet Prop Lab, NASA, Flight Path Control, Pasadena, CA USA

来源：

SPACEFLIGHT MECHANICS 2019, VOL 168, PTS I-IV | 2019年 / 168卷

关键词：

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Mars Sample Return (MSR) continues to be a high priority in the planetary science community and a decades-long goal of international planetary exploration programs. Options for architectures and mission concepts are currently under study by NASA and ESA to find potential partnership opportunities to achieve MSR in the 2020s. The major elements of a potential MSR campaign have significant architectural flexibility and mission launch, arrival, and return options. The decision criteria often depend on mission design and functional allocations across many elements. This paper outlines the reference architecture and key trades among the campaign elements.

引用

页码：2911 / 2926

页数：16

共 24 条

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