近地小行星交会航天器概览

A. Santo, S.C. Lee, A. Cheng
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引用次数: 5

摘要

约翰霍普金斯大学应用物理实验室根据美国宇航局的合同,设计并发射一艘宇宙飞船,该飞船将与近地小行星“爱神”433会合并绕其轨道运行。这艘宇宙飞船是美国宇航局“发现计划”下的第一艘飞船,该计划是一系列新的低成本太阳系任务。该任务计划于1996年2月发射,1997年6月飞越主带小行星253玛蒂尔德,1999年2月抵达爱神星433。在环绕爱神星的轨道上,飞船将用12个月的时间测量这颗小行星的体积、表面和内部特性。本文介绍了近地小行星交会任务,重点介绍了航天器的设计。系统级航天器架构采用了一种设计方法,利用任务几何结构,以低成本、快速周转和低技术风险实现令人兴奋的、一流的科学回报。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Near Earth asteroid rendezvous spacecraft overview
The Johns Hopkins University Applied Physics Laboratory is under contract from NASA to design and launch a spacecraft that will rendezvous and orbit the near Earth asteroid, 433 Eros. The spacecraft is the first under NASA's Discovery Program, which is a new series of low cost solar system missions. The mission plan is to launch in February 1996, fly by the main belt asteroid 253 Mathilde in June 1997, and arrive at 433 Eros in February 1999. While in orbit around Eros the spacecraft will measure the bulk, surface, and internal properties of the asteroid for a period of 12 months. This paper describes the near Earth asteroid rendezvous mission with a focus on the spacecraft design. The system level spacecraft architecture employs a design approach that takes advantage of mission geometry to enable exciting, first-rate science return with low cost, quick turnaround, and low technical risk.
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