Ivar asteroid rendezvous mission system scenario and trajectory design

Pingyuan Cui; Hutao Cui; Hehua Ju; Enjie Luan; Wuiren Wu; Yulong Tian

Ivar asteroid rendezvous mission system scenario and trajectory design

Pingyuan Cui
, Hutao Cui
, Hehua Ju
, Enjie Luan
, Wuiren Wu
, Yulong Tian

空天科学与技术学院

科研成果: 期刊稿件 › 会议文章 › 同行评审

摘要

Based on the principle of faster, better, cheaper, this paper has searched and calculated asteroid exploration opportunities whose launch dates are in the interval of 2006 to 2010, Taking 1627 Ivar asteroid as the exploration target, the whole spacecraft and its subsystems project have been designed and analyzed, simultaneously, the transfer trajectory for asteroid rendezvous has been designed using ΔVEGA technology, the result acquired satisfied energy requirement of minitype spacecraft.

源语言	英语
期刊论文编号	AAS 03-758
页（从-至）	453-460
页数	8
期刊	Science and Technology Series
卷	108
出版状态	已出版 - 2004
活动	International Lunar Conference 2003/International Lunar Exploration Working Group 5 - ILC2003/ILEWG 5 - Hawaii Island, HI, 美国期限: 16 11月 2003 → 22 11月 2003

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abstract = "Based on the principle of faster, better, cheaper, this paper has searched and calculated asteroid exploration opportunities whose launch dates are in the interval of 2006 to 2010, Taking 1627 Ivar asteroid as the exploration target, the whole spacecraft and its subsystems project have been designed and analyzed, simultaneously, the transfer trajectory for asteroid rendezvous has been designed using ΔVEGA technology, the result acquired satisfied energy requirement of minitype spacecraft.",

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T1 - Ivar asteroid rendezvous mission system scenario and trajectory design

AU - Cui, Pingyuan

AU - Cui, Hutao

AU - Ju, Hehua

AU - Luan, Enjie

AU - Wu, Wuiren

AU - Tian, Yulong

PY - 2004

Y1 - 2004

N2 - Based on the principle of faster, better, cheaper, this paper has searched and calculated asteroid exploration opportunities whose launch dates are in the interval of 2006 to 2010, Taking 1627 Ivar asteroid as the exploration target, the whole spacecraft and its subsystems project have been designed and analyzed, simultaneously, the transfer trajectory for asteroid rendezvous has been designed using ΔVEGA technology, the result acquired satisfied energy requirement of minitype spacecraft.

AB - Based on the principle of faster, better, cheaper, this paper has searched and calculated asteroid exploration opportunities whose launch dates are in the interval of 2006 to 2010, Taking 1627 Ivar asteroid as the exploration target, the whole spacecraft and its subsystems project have been designed and analyzed, simultaneously, the transfer trajectory for asteroid rendezvous has been designed using ΔVEGA technology, the result acquired satisfied energy requirement of minitype spacecraft.

UR - https://www.scopus.com/pages/publications/27844494618

M3 - Conference article

AN - SCOPUS:27844494618

SN - 0278-4017

VL - 108

SP - 453

EP - 460

JO - Science and Technology Series

JF - Science and Technology Series

M1 - AAS 03-758

T2 - International Lunar Conference 2003/International Lunar Exploration Working Group 5 - ILC2003/ILEWG 5

Y2 - 16 November 2003 through 22 November 2003

ER -

Ivar asteroid rendezvous mission system scenario and trajectory design

摘要

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