Development of lightweight mirror technology for the Next Generation Space Telescope

被引:13
|
作者
Stahl, HP [1 ]
机构
[1] NASA, George C Marshall Space Flight Ctr, Space Opt Mfg Technol Ctr, Huntsville, AL 35812 USA
来源
关键词
D O I
10.1117/12.453604
中图分类号
O43 [光学];
学科分类号
070207 ; 0803 ;
摘要
In 2009, NASA plans to launch the Next Generation Space Telescope (NGST) to the L2 point, 1.5 million kilometers from Earth. With a 6-meter diameter mirror, NGST is a successor to the Hubble Space Telescope with 5 times the collecting aperture. As part of NASA's Origins Program, the ten-year observing mission will search for the "first light" of the universe. NGST will provide astronomers with unparalleled light collection, mid-infrared sensitivity, spatial resolution and field of view. Mirror technology is critical to the system's success. The hard part is solving the problem of how to launch a 6m, 600 kg, mirror into space on a 4-meter diameter rocket. Additionally, high performance is expected at operating temperatures of 50K. This paper reviews the mirror requirements and development efforts.
引用
收藏
页码:1 / 4
页数:4
相关论文
共 50 条
  • [41] The science goals of the Next Generation Space Telescope
    Gardner, JP
    ULTRAVIOLET-OPTICAL SPACE ASTRONOMY BEYOND HST, 1999, 164 : 207 - 214
  • [42] Straylight analysis of the Next generation Space Telescope
    Bely, PY
    Petro, L
    Mehalick, KI
    Perrygo, CM
    SPACE TELESCOPES AND INSTRUMENTS V, PTS 1-2, 1998, 3356 : 153 - 160
  • [43] Scientific metrics for the next generation space telescope
    Mather, JC
    Smith, EP
    Stockman, HS
    SPACE TELESCOPES AND INSTRUMENTS V, PTS 1-2, 1998, 3356 : 32 - 38
  • [44] Electrostrictive ceramic actuators to shape mirror of next space telescope
    不详
    AMERICAN CERAMIC SOCIETY BULLETIN, 2010, 89 (05): : 17 - 17
  • [45] Lightweight Design and Finite Element Analysis of Primary Mirror For The Space Telescope
    Zhang, Dandan
    Li, Weiyan
    Lv, Qunbo
    Liu, Yangyang
    Chen, Xinwen
    OPTICAL SYSTEMS DESIGN 2015: OPTICAL DESIGN AND ENGINEERING VI, 2015, 9626
  • [46] Design optimization of a 1-m lightweight mirror for a space telescope
    Kihm, Hagyong
    Yang, Ho-Soon
    OPTICAL ENGINEERING, 2013, 52 (09)
  • [47] The optical performance test of lightweight primary mirror of space Cassegrain telescope
    Lin, Wei-Cheng
    Chang, Shenq-Tsong
    Huang, Ting-Ming
    Hsu, Ming-Ying
    Lin, Yu-Chuan
    OPTICAL MANUFACTURING AND TESTING X, 2013, 8838
  • [48] Development of lightweight mirror technology for the NGST program
    Jacobson, D
    Bunton, P
    OPTICAL MANUFACTURING AND TESTING III, 1999, 3782 : 114 - 122
  • [49] Overview of mirror technology development for large lightweight space-based optical systems
    Smith, WS
    Stahl, HP
    OPTOMECHANICAL ENGINEERING 2000, 2001, 4198 : 1 - 8
  • [50] SimNGST: The Next Generation Space Telescope mission simulator
    Smith, EP
    Offenberg, J
    Bely, PY
    34TH LIEGE INTERNATIONAL ASTROPHYSICS COLLOQUIUM - THE NEXT GENERATION SPACE TELESCOPE SCIENCE DRIVERS AND TECHNOLOGICAL CHALLENGES, 1998, 429 : 301 - 305