Ivar asteroid rendezvous mission system scenario and trajectory design

Ping Yuan Cui; Li Tao Li; Hu Tao Cui; En Jie Luan; Wei Ren Wu; Yu Long Tian

Ivar asteroid rendezvous mission system scenario and trajectory design

Ping Yuan Cui^*, Li Tao Li, Hu Tao Cui, En Jie Luan, Wei Ren Wu, Yu Long Tian

^*此作品的通讯作者

科研成果: 期刊稿件 › 文章 › 同行评审

6 引用（Scopus）

摘要

The asteroid exploration opportunities are searched and calculated with launch dates in 2006 to 2010, and with asteroid Ivar 1627 as the target, the spacecraft and its subsystems are designed and analyzed, and the transfer trajectory is designed by Δ VEGA technology for the asteroid rendezvous. The design results satisfies the energy requirements for small explorers.

源语言	英语
页（从-至）	338-342
页数	5
期刊	Journal of Harbin Institute of Technology (New Series)
卷	10
期	3
出版状态	已出版 - 9月 2003
已对外发布	是

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title = "Ivar asteroid rendezvous mission system scenario and trajectory design",

abstract = "The asteroid exploration opportunities are searched and calculated with launch dates in 2006 to 2010, and with asteroid Ivar 1627 as the target, the spacecraft and its subsystems are designed and analyzed, and the transfer trajectory is designed by Δ VEGA technology for the asteroid rendezvous. The design results satisfies the energy requirements for small explorers.",

keywords = "Asteroid exploration, Rendezvous, Spacecraft system design, Trajectory design",

author = "Cui, {Ping Yuan} and Li, {Li Tao} and Cui, {Hu Tao} and Luan, {En Jie} and Wu, {Wei Ren} and Tian, {Yu Long}",

year = "2003",

month = sep,

language = "English",

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T1 - Ivar asteroid rendezvous mission system scenario and trajectory design

AU - Cui, Ping Yuan

AU - Li, Li Tao

AU - Cui, Hu Tao

AU - Luan, En Jie

AU - Wu, Wei Ren

AU - Tian, Yu Long

PY - 2003/9

Y1 - 2003/9

N2 - The asteroid exploration opportunities are searched and calculated with launch dates in 2006 to 2010, and with asteroid Ivar 1627 as the target, the spacecraft and its subsystems are designed and analyzed, and the transfer trajectory is designed by Δ VEGA technology for the asteroid rendezvous. The design results satisfies the energy requirements for small explorers.

AB - The asteroid exploration opportunities are searched and calculated with launch dates in 2006 to 2010, and with asteroid Ivar 1627 as the target, the spacecraft and its subsystems are designed and analyzed, and the transfer trajectory is designed by Δ VEGA technology for the asteroid rendezvous. The design results satisfies the energy requirements for small explorers.

KW - Asteroid exploration

KW - Rendezvous

KW - Spacecraft system design

KW - Trajectory design

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M3 - Article

AN - SCOPUS:2342433426

SN - 1005-9113

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SP - 338

EP - 342

JO - Journal of Harbin Institute of Technology (New Series)

JF - Journal of Harbin Institute of Technology (New Series)

IS - 3

ER -

Ivar asteroid rendezvous mission system scenario and trajectory design

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