Near-earth asteroid rendezvous: Mission overview

被引:38
|
作者
Cheng, AF
Santo, AG
Heeres, KJ
Landshof, JA
Farquhar, RW
Gold, RE
Lee, SC
机构
关键词
D O I
10.1029/97JE03364
中图分类号
P3 [地球物理学]; P59 [地球化学];
学科分类号
0708 ; 070902 ;
摘要
The Near-Earth Asteroid Rendezvous (NEAR) mission, the first launch of NASA's Discovery Program, will be the first mission to orbit an asteroid. NEAR will make the first comprehensive scientific measurements of an asteroid's surface composition, geology, physical properties, and internal structure. NEAR launched successfully on February 17, 1996, aboard a Delta II-7925. It will orbit the 20-km-diameter near-Earth asteroid 433 Eros for about 1 year, at a minimum orbit radius of about 35 km from the center of the asteroid. The NEAR is a solar-powered, three-axis stabilized spacecraft with a launch mass including propellant of 805 kg. NEAR uses X band telemetry to the NASA Deep Space Network, with the data rates at Eros up to 8.8 kbits/s using a 34-m High Efficiency (HEF) dish, and up to 26.5 kbits/s using a 70-m dish. A solid-state recorder is accommodated with a memory capacity of 1.8 Gbytes. Attitude control is to 1.7 mrad, line-of-sight pointing stability is within 50 mu rad over 1 s, and post processing attitude knowledge is within 50 mu rad. NEAR accommodates 56 kg of instruments and provides them with 84 W. The instruments are a multispectral imager (MSI), a near-infrared spectrograph (NIS), an X ray/gamma ray spectrometer (XRS/GRS), a magnetometer (MAG), and a laser rangefinder (NLR), while a radio science (RS) investigation uses the coherent X band transponder. NEAR will make a flyby of the C-type asteroid 253 Mathilde in June 1997 and will rendezvous with 433 Eros in February 1999. It will execute an initial slow flyby of Eros, with a flyby speed of 5 m/s and a closest approach distance of 500 km. Subsequently, its orbit will be lowered to 35 km. The NEAR Mission Operations Center and the Science Data Center are at the Johns Hopkins Applied Physics Laboratory. The Science Data Center will maintain the entire NEAR data set on-line, and data from all instruments can be accessed by every member of the NEAR Science Team. Data, including images, are released over the Internet as soon as they are validated.
引用
下载
收藏
页码:23695 / 23708
页数:14
相关论文
共 50 条
  • [1] Near-Earth Asteroid Rendezvous (NEAR) mission overview and trajectory design
    Farquhar, RW
    Dunham, DW
    McAdams, JV
    ASTRODYNAMICS 1995, 1996, 90 : 1331 - 1351
  • [2] The Near-Earth Asteroid Rendezvous (NEAR) mission
    Farquhar, RW
    JOURNAL OF THE ASTRONAUTICAL SCIENCES, 1995, 43 (04): : 349 - 351
  • [3] Near Earth Asteroid Rendezvous: Mission overview
    Cheng, AF
    SPACE SCIENCE REVIEWS, 1997, 82 (1-2) : 3 - 29
  • [4] Near Earth Asteroid Rendezvous: Mission Overview
    Andrew F. Cheng
    Space Science Reviews, 1997, 82 : 3 - 29
  • [5] Postlaunch contingency trajectories for the near-earth asteroid rendezvous mission
    McAdams, JV
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1997, 20 (04) : 819 - 823
  • [6] Laser radar instrument for the near-earth asteroid rendezvous (NEAR) mission
    Cole, TD
    Boies, M
    ElDinary, A
    LASER RADAR TECHNOLOGY AND APPLICATIONS, 1996, 2748 : 122 - 139
  • [7] Target selection and accessibility for rendezvous with a Near-Earth asteroid mission
    Dong Qiao
    Pingyuan Cui
    Hutao Cui
    Earth, Moon, and Planets, 2007, 100 : 137 - 156
  • [8] Target selection and accessibility for rendezvous with a Near-Earth asteroid mission
    Qiao, Dong
    Cui, Pingyuan
    Cui, Hutao
    EARTH MOON AND PLANETS, 2007, 100 (3-4): : 137 - 156
  • [9] Multiple near-earth asteroid rendezvous mission: Solar-sailing options
    Peloni, Alessandro
    Dachwald, Bernd
    Ceriotti, Matteo
    ADVANCES IN SPACE RESEARCH, 2018, 62 (08) : 2084 - 2098
  • [10] The Near-Earth Asteroid Rendezvous Laser Altimeter
    T. D. Cole
    M. T. Boies
    A. S. El-Dinary
    A. Cheng
    M. T. Zuber
    D. E. Smith
    Space Science Reviews, 1997, 82 : 217 - 253