MARS ION AND SPUTTERING ESCAPE NETWORK (MISEN) MISSION CONCEPT

被引：0

作者：

Parker, Jeffrey S. ^{[1
]}

Parrish, Nathan ^{[1
]}

Lillis, Rob ^{[2
]}

Curry, Shannon ^{[2
]}

Curtis, Dave ^{[2
]}

Luhmann, Janet ^{[2
]}

Puig-Suari, Jordi ^{[3
]}

Russell, Christopher ^{[4
]}

Brain, David ^{[5
]}

机构：

[1] Adv Space, 2100 Cent Ave,102, Boulder, CO 80301 USA

[2] Univ Calif Berkeley, Space Sci Lab, 7 Gauss Way, Berkeley, CA 94720 USA

[3] Tyvak Nanosatellite Syst Inc, 15330 Barranca Pkwy, Irvine, CA 92618 USA

[4] Univ Calif Los Angeles, Dept Earth & Space Sci, Geophys & Space Phys, 595 Charles Young Dr East,Box 951567, Los Angeles, CA 90095 USA

[5] Univ Colorado, Lab Atmospher & Space Phys, 3665 Discovery Dr, Boulder, CO 80303 USA

来源：

ASTRODYNAMICS 2018, PTS I-IV | 2019年 / 167卷

关键词：

SOLAR-WIND; SEASONAL VARIABILITY; MAVEN; FIELD;

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The Mars Ion and Sputtering Escape Network (MISEN) is a mission concept developed through the Planetary Science Deep Space SmallSat (PSDS3) program supported by NASA's Science Mission Directorate. MISEN includes three small satellites deployed as secondary payloads aboard a primary mission destined for Mars, the Moon, or another orbit of similar launch energy. The three satellites each use solar electric propulsion (SEP) to transfer to Mars, rendezvous with Mars, and descend to three different orbits. Once there, they conduct a joint investigation characterizing ion and sputtering escape mechanisms in the Martian atmosphere. This paper describes the mission design challenges and solutions, illustrating the viability of achieving multiple different orbits about Mars as a secondary payload aboard many viable launches using SEP.

引用

页码：1583 / 1603

页数：21

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